• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    SYSTEMS AND METHODS FOR PLASMA COMPRESSION WITH PROJECTILE RECYCLING. Modalities of systems and methods for plasma compression are disclosed in which plasma can be compressed through the impact of a projectile on a magnetized plasma in a liquid metal cavity. The projectile can fuse in the liquid metal cavity and liquid metal can be recycled to form new projectiles.
    公开号:BR112012002147B1
    申请号:R112012002147-8
    申请日:2010-07-28
    公开日:2020-12-22
    发明作者:Stephen James Howard
    申请人:General Fusion, Inc；
    IPC主号:
    专利说明:

    CROSS REFERENCE TO RELATED ORDERS
    [0001] This application claims benefit under 35 USC § 119 (e) of United States Provisional Patent Application No. 61 / 229,355, filed on July 29, 2009, entitled "SYSTEMS AND METHODS FOR PLASMA COMPRESSION AND HEATING WITH RECYCLING OF PROJECTILES ", which is incorporated herein by reference in its entirety. BACKGROUND Field
    [0002] The present description refers to the embodiments of systems and methods for plasma compression. Related Technique Description
    [0003] Some systems for plasma compression at high temperatures and densities are typically large, expensive and are limited in repetition rate and operational durability. The addition of a magnetic field within the plasma is a promising method for improving the effectiveness of any given heating scheme due to the rates of energy loss and decreased particles in the plasma volume.
    [0004] Plasma compression methods include the following six schemes. (1) Direct compression of a plasma using an external magnetic field that increases with time. (2) Compression by a rocket ablative effect of an external surface of an implosion capsule, with compression triggered by intense electromagnetic radiation or high energy particle beams (such as certain Inertial Confinement Fusion (ICF) devices). See, for example, R. W. Moir et al. "HYLIFE-II: An approach to a long-lived, first-wall component for inertial fusion power plants", Report Numbers UCRL-JC-117115; CONF-940933-46, Lawrence Livermore National Lab, August 1994, which is incorporated herein by reference in its entirety. (3) Compression by means of electromagnetic implosion of a conductive coating, typically metal, driven by large pulsed electrical currents that circulate in the implosion coating. (4) Compression by spherical or cylindrical focusing of an acoustic pulse of great amplitude in a conduction medium. See, for example, the systems and methods revealed in United States Patent Application Publication Nos. 2006/0198483 and 2006/0198486, each of which is incorporated herein by reference in its entirety. In some implementations, compression of a conductive medium can be accomplished using an external pressurized gas. See, for example, the LINUS system described in R. L. Miller and R. A. Krakowski, "Assessment of the slowly-imploding liner (LINUS) fusion reactor concept", Rept. No. LA-UR-80-3071, Los Alamos Scientific Laboratory, Los Alamos, NM 1980, which is hereby incorporated by reference in its entirety. (5) Passive compression by injecting a mobile plasma into a static void, but conically converging within a conductive medium so that the kinetic energy of the plasma triggers the compression determined by the wall boundary restrictions. See, for example, C. W. Hartman, '' A Compact Torus Fusion Reactor Utilizing a Continuously Generated String of CT's. The CT String Reactor ', CTSR Journal of Fusion Energy, vol. 27, pages. 44-48 (2008); and "Acceleration of Spheromak Toruses: Experimental results and fusion applications”, UCRL-102074, in Proceedings of 11th US / Japan workshop on field- reversed configurations and compact toroids; 7-9 Nov 1989; Los Alamos, NM, each of which it is incorporated by reference in its entirety. (6) Compression of a plasma triggered by the impact of high kinetic energy macroscopic projectiles, for example, by a pair of collision projectiles or by a single projectile impacting a stationary target medium. for example, U.S. Patent No. 4,328,070, which is incorporated herein by reference in its entirety. See also the document incorporated above by CW Hartmann and colleagues, "Acceleration of Spheromak Toruses: Experimental results and fusion applications." SUMMARY
    [0005] An embodiment of a system for compressing plasma is revealed. The system may include a plasma injector comprising a plasma forming system configured to generate a magnetized plasma and a plasma accelerator having a first portion, a second portion and a longitudinal axis between the first portion and the second portion. The plasma accelerator can be configured to receive the magnetized plasma in the first portion and to accelerate the magnetized plasma along the longitudinal axis in the direction of the second portion. The plasma compression system may also include a liquid metal circulation system configured to supply liquid metal that forms at least a portion of a chamber configured to receive the magnetized plasma from the second portion of the plasma accelerator. Magnetized plasma can have a first pressure when received in the chamber. The system may also include a projectile accelerator configured to accelerate a pointer along at least a portion of the longitudinal axis toward the chamber. The system can be configured so that the projectile compresses the magnetized plasma in the chamber so that the compressed magnetized plasma can have a second pressure that is greater than the first pressure.
    [0006] An embodiment of a plasma compression method is revealed. The method comprises the generation of a toroidal plasma, accelerating the toroidal plasma towards a cavity in a liquid metal, accelerating a projectile towards the cavity in the liquid metal and compressing the toroidal plasma with the projectile while the toroidal plasma is in the cavity in the liquid metal. In some embodiments, the method may also include circulating a liquid metal to form the cavity. In some embodiments, the method may also include recycling a portion of the liquid metal to form at least one new projectile.
    [0007] An embodiment of an apparatus for plasma compression is revealed. The apparatus may comprise a plasma injector configured to accelerate a compact plasma toroid towards a cavity in a liquid metal. The cavity can be concave in shape. The apparatus may also include a projectile accelerator configured to accelerate a projectile towards the cavity, and a timing system configured to coordinate the acceleration of the compact toroid and the acceleration of the projectile, so that the projectile confines the compact toroid in the cavity in the liquid metal. BRIEF DESCRIPTION OF THE DRAWINGS
    [0008] Through drawings, reference numbers can be reused to indicate correspondence between referenced elements. The drawings are provided to illustrate example embodiments described here and are not intended to limit the scope of the description.
    [0009] Figure 1 is a schematic cross-sectional diagram showing an example embodiment of a plasma compression system with liquid metal wall limitation, where the system comprises a projectile acceleration device, a plasma injector, a liquid metal recirculation vessel and a projectile-forming subsystem.
    [00010] Figure 2 is a schematic cross-sectional diagram showing a portion of an example embodiment of a plasma injector located coaxially around the barrel of a projectile accelerator. In the illustrated embodiment, the plasma injector is symmetrical rotationally about the geometric axis of projectile accelerator 40a.
    [00011] Figure 3 includes simplified cross-sectional schematic diagrams (AI) that illustrate an example, in a time sequence, of how the projectile and plasma can behave from impact with a liquid metal to the point of maximum pressure and then subsequent fracture of the projectile and mixing with the liquid metal used for recycling projectile material. Density values in kg / m3 are illustrated as gray scale levels according to the values in the status bar to the right of the figure.
    [00012] Figures 4A-4F are schematic cross-sectional diagrams illustrating various example embodiments of projectiles.
    [00013] Figure 5 shows, schematically, an example of timing of gas ventilation valves in an example embodiment of a projectile accelerator.
    [00014] Figure 6 is a flow chart that schematically illustrates an example embodiment of a plasma compression method in a liquid metal chamber, using a projectile's impact on the magnetized plasma. DETAILED DESCRIPTION Overview
    [00015] The plasma compression schemes described above have several advantages and disadvantages. However, a significant obstacle in the effective implementation of any plasma compression scheme is, typically, the monetary cost of building such a device on the necessary physical scale. For some of the above schemes, construction costs prevent or even prohibit full-scale testing and development of prototypes. Thus, it may be beneficial to consider technologies that can be economically built on a prototype and full scale, using some conventional methods and materials and that have a relatively simple global model and relatively small physical scale.
    [00016] Embodiments of the compression schemes described above, in general, are of a pulsed nature. Two possible factors to consider are the cost per pulse and the pulse repetition rate. Schemes that use high-precision parts that are destroyed with each pulse cycle (for example, schemes 2, 3 and some versions of scheme 6) can typically have a significantly higher cost per pulse than schemes that are both non-destructive (for example, scheme 1) when employing passive material recycling (for example, schemes 4, 5 and some versions of scheme 6). Non-destructive pulse schemes tend to have the highest repetition rate (which can be limited by magnetic effects) which can be as high as in a kHz range in certain implementations. Passive recycling can be the second fastest with repetition rates (which can be limited by coating fluid flow speeds) that can be as high as several Hz in certain implementations. Schemes where the central set for pulsed compression is destroyed each pulse tends to have the slowest intrinsic repetition rate, determined by the time taken to clean up destroyed elements and insert a new set. This is not likely to be more than once every few seconds, at best, in some implementations.
    [00017] Due to the potential for emission of energetic particles and intense X-rays from plasmas at high density and temperature, it may be advantageous to consider schemes that incorporate a large volume of replaceable absorbent material to reduce the extent to which the radiation products of the plasma to reach the permanent structural elements of the compression device. Devices that do not incorporate this material or absorbing mat may tend to suffer from radiation damage to their structural components and have correspondingly shorter operating durations. Although some embodiments of schemes 1, 2 and 3 can be adapted to accommodate a quantity of absorbent material, this can complicate the model (see, for example, the HYLIFE-II reactor model, described in the incorporated article above, by Moir and colleagues ). In contrast, diagrams 4, 5 and 6 incorporate an absorbent material, by choosing the material used for the compression coating fluid and / or by adding material in large unused volumes surrounding the device. Systems with a recirculating absorber fluid can also provide a low-cost method of extracting heat produced during compression. The recirculation of an absorbing fluid can also allow radiation products from the compressed plasma to be used to transmit isotopes included in the absorbing fluid. This approach can be used to process waste material or to provide a cost-effective method of producing rare isotopes.
    [00018] Compression schemes driven by impact, typically, have involved methods to accelerate small but macroscopic projectiles, to the ultrahigh speeds needed to compress and heat solid projectiles in a state of hot, extremely dense plasma, typically without field magnetic or with a magnetic field with only minimal containment properties. This typically requires the use of an extremely long electromagnetic accelerator (for example, up to several kilometers in length) to develop the necessary speed, resulting in prohibitive construction costs.
    [00019] Several embodiments of the present description address some of these and other challenges. For example, in most systems that use projectiles, there has been no method for recycling projectile material, which results in the destruction of high-precision parts, greatly increasing the cost per pulse. In addition, the mechanisms for absorbing plasma radiation products for useful purposes have not been integrated into previous models and, therefore, any absorbent mat must be added as a later resource, possibly with significant engineering complications.
    [00020] Some embodiments of the present approach involve using the impact of a projectile to trigger plasma compression and provide a system configuration that allows for a significantly smaller scale system with higher repetition rates and / or longer system life than previous approaches. In contrast to some impact compression methods (see, for example, U.S. Patent No. 4,435,354, which is incorporated herein by reference in its entirety), certain embodiments of the present approach use a greater mass displacement in lower speed, which acts to compress a well magnetized plasma. This may allow the use of a less complex and less expensive projectile acceleration method for plasma compression. For example, a light gas gun can be used to accelerate the projectile to a speed of up to several km / s over a range of, for example, approximately 100 meters. Examples of lightweight gas guns and projectile launchers that can be used with the embodiments of the plasma compression system disclosed here are described in U.S. Patent No. 5,429,030 and U.S. Patent No. 4,534,263, each one of which is incorporated herein by reference in its entirety. The projectile launcher described in the publication by L.R. Bertolini, et al., "SHARP, a first step towards a full sized Jules Verne Launcher", Report Number UCRL-JC-114041; CONF-9305233-2, Lawrence Livermore National Lab, May 1993, which is incorporated herein in its entirety, can also be used with embodiments of the plasma compression system.
    [00021] The embodiments of the present approach may incorporate an integrated passive recycling system for projectile material. This can allow for an improved repetition rate (for example, relatively high) and / or an increase in system durability. With the proper choice of materials, the projectile and the coating fluid can act as an efficient absorber of plasma radiation products, resulting in a system that has an economic viability and practical utility. Systems andExample Methods for Plasma Compression
    [00022] Embodiments of systems and methods for plasma compression are described. In some embodiments, plasma can be compressed by the impact of a projectile on a magnetized plasma toroid in a liquid metal cavity. The projectile can fuse in the liquid metal cavity and the liquid metal can be recycled to form new projectiles. The plasma can be heated during compression.
    [00023] With reference to the drawings, a schematic cross-sectional diagram of an embodiment of a new and improved example plasma compression system 10 is shown in figure 1. The example system 10 includes an injection forming / injection device magnetized plasma 34, an accelerator 40 (for example, a light gas pneumatic gun or an electromagnetic accelerator), which fires projectiles 12 along an acceleration axis 40a towards the compression chamber 26, defined in part by a convergent flow liquid metal 46. The liquid metal 46 is contained within the liquid metal recirculation vessel 18 and a conical nozzle 24 directs the flow of liquid metal 46 into a magnetic flow conservation liner having a desired shaped surface 27 in the chamber of compression 26. The compression chamber 26 can be substantially symmetrical about a geometric axis. The geometric axis of the compression chamber 26 can be substantially collinear with the acceleration axis 40a (see, for example, figures 1 and 2). System 10 may include a timing system (not shown) configured to coordinate the relative timing of events, such as, for example, plasma formation, plasma acceleration, projectile firing or acceleration, etc. For example, since, in some embodiments, the velocity of the projectile can be significantly less than the speed of plasma injection, plasma formation and injection can be delayed and triggered by the timing system when projectile 12 reaches a prescribed position (for example, near the barrel) of the accelerator 40.
    [00024] Figure 1 schematically illustrates three example projectiles 12a, 12b and 12c moving towards the compression chamber 26. A fourth projectile 12d is in liquid metal 46, close to the point of maximum plasma compression. The four projectiles 12a - 12d are intended to illustrate features of system 10 and are not intended to be limiting. For example, in other embodiments, different numbers of projectiles (for example, 1, 2, 4 or more) can be accelerated by accelerator 40 at any time. Figure 1 also schematically illustrates a plasma torus in three different positions in the system 10. In the illustrated embodiment, the magnetized plasma torus can be formed near a forming region 36a of the forming / injection device 34. The magnetized plasma shown in position 36b it was accelerated and compressed between coaxial electrodes 48 and 50. In position 36c, near the accelerator barrel 40, the magnetized plasma expands outside the end of coaxial electrodes 48 and 50 in the largest volume of the compression chamber 26, defined through the front surface of the projectile 12c (see figure 1) and the surface 27 of the liquid metal. The magnetized plasma can persist at position 36c in the compression chamber 26 with a magnetic decay time that is several times longer than the compression time.
    [00025] The movement of the projectile 12c can compress the plasma close to position 36c, with the internal magnetic confinement of the plasma, reducing or preventing significant loss of particles in the plasma injector during the initial compression phase. In the system 10 illustrated schematically in figure 1, the size of the projectile 12c transverse to the acceleration axis 40a is smaller than the size of the opening for the compression chamber 26, so that there is an annular opening around the outside of the projectile, when the projectile is near position 36c. A later stage of compression begins after the projectile 12c closes the opening for the chamber and the compression chamber 26 is substantially or completely covered by the surface 27 of the liquid metal and the projectile 12c. See, for example, figure 3 which schematically represents a simulated time sequence of compression geometry. Therefore, the impact of the projectile 12 on the plasma in the compression chamber can increase the pressure, density and / or temperature of the plasma. For example, the plasma may have a first pressure (or density or temperature), when in the compression chamber 26 and a second pressure (or density or temperature) after the impact of the projectile 12, the second pressure (or density or temperature) higher than the first pressure (or density or temperature). The second pressure (or density or temperature) can be greater than the first pressure (or density or temperature), for example, by a factor of 1.5; two; 4; 10; 25, 50, 100 or more. After the projectile is swallowed in liquid metal 46 (represented in figure 1 as projectile 12d), the projectile can disintegrate quickly and fuse back into metal 46. As will be described below, liquid metal 46 in vessel 18 can be recycled to form new projectiles.
    [00026] As a result of the compression, the plasma can be heated. The liquid heating of the liquid metal 46 can occur due to the absorption of radiation products from the compressed plasma, as well as thermalization of the projectile kinetic energy. For example, in some implementations, liquid metal 46 can be heated as much as several hundred degrees Celsius by the plasma compression event. Thus, as shown in the example in figure 1, as the liquid metal 46 is recirculated by a pump 14, the liquid metal 46 can be cooled via a heat exchange system 16 in order to maintain a desired temperature in the inlet 28 or conical nozzle 24. In some implementations, the heat generated by the compression of the plasma can be extracted by the heat exchanger and used in an electricity generation system (for example, a turbine driven by steam generated from the extracted heat) . In some embodiments, the temperature of the liquid metal can be kept moderately above its melting point (for example, Tmelt + approximately 10 - 50 ° C). The heat exchanger 16 can be any suitable heat exchanger.
    [00027] In some embodiments, the heat exchanger outlet can be used in other processes. For example, in addition to the inlet tube 28, which directs the flow of liquid metal 46 to the conical nozzle 24 in order to create the surface 27 of the compression chamber 26, a recirculation tube 30 can distribute a supply of liquid metal 46 to the projectile molds 32 in a subsystem to make new batches of projectiles (for example, projectile factory 37, shown in figure 1). In some embodiments, a loading mechanism 38 can be used to automatically load new projectiles into the throttle opening 40. In certain embodiments, an array of projectiles 12 can be located within a cartridge structure that can be loaded by the delivery mechanism. loading 38 at the opening of the accelerator 40 and fired in a relatively rapid sequence along the acceleration axis 40a. In some cases, a short period of time, possibly as short as 1 - 2 seconds in some implementations, without the accelerator 40 firing, may be provided to allow the next projectile cartridge to be loaded. In some embodiments, the loading mechanism 38 may have a direct charge - fire - charge - fire cycle, in which case a cartridge structure does not need to be used and a substantially constant rate of projectile fire can be maintained.
    [00028] In some embodiments, projectile molds 32 can be automated to receive recycled liquid metal 46 and provide an appropriate cooling cycle to allow new projectiles to be smelted using various fabrication methods. The rate of liquid metal recirculation and new projectile production can be sufficient to feed projectiles at the desired launch rate. The total cooling time for the liquid metal to solidify sufficiently within the molds can be determined by parallelism within the method of preparing batches of new projectiles. In some implementations of system 10, the cooling time can be made as short as practical and / or can be determined by the amount of stiffness required for the proper mechanical function of the loading mechanism and / or by the ability of the projectile 12 to survive acceleration of the weapon. With this highly automated firing cycle, a reasonably high repetition rate can be achieved for long periods. In addition, with the possible exception of plasma injection for each shot, certain embodiments of the system 10 have the advantages of being effectively a closed loop, in which the solid projectile 12 can be fired into a vessel 18 substantially filled with the same material in liquid form, and liquid metal 46 can be recycled to form new projectiles 12. In some embodiments, projectile fabrication can be carried out using the systems and methods described, for example, in U.S. Patent No. 4,687,045 , which is incorporated here in its entirety.
    [00029] System 10 can be used in a variety of practical and useful applications. For example, in applications involving the transmutation of isotopes by the absorption of radiation products, there may be another branch of the liquid metal flow cycle (not shown), in which isotopes can be extracted from liquid metal 46, for example, using standard bed-absorbent techniques. If necessary, in some embodiments, additional metal can be added to the flow to replenish the amounts that are lost to transmutation or other losses or inefficiencies.
    [00030] In some implementations of system 10, some or all of the liquid metal recirculation system may be similar to the systems used for some implementations of the compression schemes 4 and 5 described above. A certain implementation of this scheme may be different from certain implementations of scheme 4 in that no vortex hydrodynamics are used to create the central cavity of the compression chamber 26, in contrast, linear nozzle flow can be used. Some implementations of the present approach may also be different from some implementations of Scheme 4 in that only a single projectile is used to trigger each compression and the timing of the impact of a number of pistons used to create a substantially symmetrical acoustic pulse may not be needed.
    [00031] Certain embodiments of the present approach also have some possible advantages over scheme 5, which typically uses a significantly larger and more powerful plasma injector to develop the kinetic energy required for the development of full plasma compression, resulting in a higher construction cost, due to the price of capacitive energy storage. In some embodiments of the present approach, the energy that can be used to compress plasma can be derived mainly from pressurized gas that accelerates projectile 12 on accelerator 40. In some cases, this may be a less complex and less expensive technology than used in certain implementations of scheme 5.
    [00032] Embodiments of the plasma compression system 10 may include the accelerator 40 to fire a projectile 12 along a substantially linear path that passes along axis 40a substantially through the center of the plasma injector 34 and ends in impact with the plasma and the liquid metal walls of the compression chamber 26 inside the recirculation vessel 18. In some embodiments, the accelerator 40 can be configured so that it can efficiently achieve high projectile speeds (such as about 1- 3 km / s) for a large caliber projectile (such as, for example, about 100 kg mass, about 400 mm in diameter) and may be able to operate in an automated repeat firing mode. There are a number of known acceleration devices that can be adapted for this application. One possible approach may be to use a light gas gun. In some implementations, the pistol design may allow for a quick recharge of the plenum volume behind the projectile with a light pressurized "propellant gas" (which may comprise, for example, hydrogen or helium). In some implementations, it may be advantageous for the region in front of the projectile to be at least partially evacuated prior to the subsequent firing of the pistol. For example, as a projectile 12 advances, it can push a fraction of the gas on its way into the compression chamber 26. Depending on the composition of the gas, this can possibly contaminate the plasma that is injected into the compression chamber 26. The presence of another gas (impurity) can, in some cases, cool the plasma by emitting line radiation, which reduces the energy available to heat the plasma. In embodiments in which hydrogen is used as the propellant gas, hydrogen can be completely ionized and incorporated into the plasma without a high likelihood of these cooling problems. In addition, the residual gas in front of the projectile acts as a drag force, slowing down the acceleration of the projectile in the gun. Thus, in embodiments with at least a partial vacuum in front of the projectile, the enhanced efficiency of the pistol can be achieved.
    [00033] In some embodiments, a conventional light gas gun can provide rapid evacuation of the barrel from gun 44, during the inter-firing period. For example, in a possible gun design, the main gun barrel 44 can be surrounded by a significantly larger vacuum tank (not shown in FIG. 1), with a large number of actuating vent valves 42 distributed along the length of gun 44. One possible example method of operating the valves includes the following. During the inter-firing period all (or at least a substantial fraction) the valves 42 can be opened and the propellant-firing gas from previous projectiles can be exhausted in the vacuum tank. Once the valves open, without including the outlet effect due to active pumping on the surface of the vacuum tank, an estimate for the initial equilibrium pressure is Pequ = Ppush Vgun / Vtank = Ppush (rgun / rtank). where Ppush is the final gun pressure after the projectile has left the barrel, Vgun, Vtank are the volumes of the pistol barrel 44 and the vacuum tank, respectively, which, for a cylindrical pistol-tank coaxial system, is also proportional to the square of the ratios of the spokes of the pistol barrel and the tank. For example, if (rgun / rtank) = 1/10 and the final boost pressure is Ppush = 1 atmosphere (where 1 atmosphere is approximately 1.013 x 105 Pa), then the initial equilibrium pressure will be about 1 / 100 of an atmosphere. In some of these embodiments, this volumetric drop in pressure allows the use of standard high-speed turbine pump technology to evacuate the system, which is not normally used at the very high pressures provided in some gas gun models. In certain embodiments, vacuum turbine pumps (not shown) can be distributed across the surface of the vacuum tank and, in the case of parallel pumping, may have a combined pumping rate that equals or exceeds the gas inflow rate in average time due to the injection of the propellant gas to propel the projectile. A possible arrangement may be a closed circuit for the propellant gas, in which compressors capture the exhaust of the vacuum pumps and pressurize the gun plenum directly. Curing energy from the heat exchange system 16 can additionally or alternatively be used to thermally pressurize the gas in the plenum.
    [00034] Continuing with the example valve operation method, once the pressure in gun 40 is reduced to sufficient levels, valves 42 can begin to close and can be synchronized so that the valves closest to the gun breech 40 can close completely first. In some cases, the total closing time of valves 42 can be staggered in a linear sequence along the length of the pistol 40, in such a way that it follows the trajectory of the projectile. Other synchronization patterns can be used. With proper timing, some embodiments of pistol 40 can be configured to fire another projectile 12, as soon as valves 42 near the breech have closed, and then, as projectile 12 advances under gun 40, the projectile can pass through newly closed valves, with the valves in front of the projectile being in the closing process, but still open enough that any residual gas is pushed into the vacuum tank. Other pistol firing patterns can be used in other embodiments.
    [00035] Ventilation valves activated 42 can, for example, operate via movement that can be linear or rotating in nature. FIG. 5 schematically illustrates an example of synchronization of rotary gas vent valves 42a-42d in an embodiment of a projectile accelerator. Motors 78a-78d can be used to rotate valve rotors 72a-72d, respectively. In this example, timing can be arranged in such a way that valve rotors 72a and 72b, at least partially closed by one or more ventilation holes 74a and 74b, respectively, behind the location 76 of the projectile (which is moving towards right in this example), and valve rotors 72c and 72d leave at least one or more ventilation holes 74c and 74d, respectively, behind the projectile location 76 so that the gas can be at least partially confined in the region behind of the projectile, while the region in front of the projectile can be at least partially evacuated. In some implementations, recycling the propellant gas through the system may require significant energy loss over a short (eg sub-second) inter-shot time period. In other gun operating methods, the vent valves (if used) can be operated in a different way than described above.
    [00036] In certain embodiments, the repetition rate of the projectile acceleration system may be greater than or equal to the intrinsic repetition rate of the compression scheme. In other embodiments, the repetition rate of the projectile acceleration system may be less than the intrinsic repetition rate of the compression scheme.
    [00037] Other methods of projectile acceleration can be used. For example, another possible projectile acceleration method includes the use of an inductive coil gun, which in some embodiments uses a sequence of pulsed electromagnetic coils to apply repulsive magnetic forces to accelerate the projectile. A possible advantage of the inductive coil gun may be that the coil gun can be kept in a high evacuation state on a constant basis.
    [00038] In some embodiments of system 10, additional sensors (not shown) and a trip circuit (not shown) can be incorporated for the precise triggering of throttle 40.
    [00039] Embodiments of projectile 12 and / or liquid metal 46 can be made of a metal, alloy, or a combination thereof. For example, a lead / lithium alloy with approximately 17% lithium per atomic concentration can be used. This alloy has a melting point of about 280 ° C and a density of about 11.6 g / cm3. Other concentrations of lithium can be used (for example, 5%, 10%, 20%) and, in some implementations, lithium is not used. In some embodiments, projectile 12 and liquid metal 46 have substantially the same composition (for example, in some recycled, pulsed implementations). In other embodiments, projectile 12 and liquid metal 46 can have different compositions. In some embodiments, projectile 12 and / or liquid metal 46 can be made from metals, alloys or combinations thereof. For example, the projectile and / or the liquid metal may comprise iron, nickel, cobalt, copper, aluminum, etc. In some embodiments, liquid metal 46 can be selected to have neutron absorption low enough that a useful neutron stream escapes the liquid metal.
    [00040] Embodiments of the plasma torus injector 34 may, in general, be similar to some known designs of the coaxial railgun type. See, for example, several embodiments of the plasma torus injector described in: J. H. Degnan, et al, "Compact toroid formation, compression, and acceleration," Phys. Fluids B, vol. 5, no. 8, pp. 2938-2958, 1993; R. E. Peterkin, "Direct electromagnetic acceleration of a compact toroid to high density and high speed", Physical Review Letters, vol. 74, no. 16, pp. 3165-3170, 1995; and J. H. Hammer, et al., "Experimental demonstration of acceleration and focusing of magnetically confined plasma rings," Physical Review Letters, vol. 61, no. 25, pp. 2843-2846, December 1988. See also the injector design that was experimentally tested and described in H. S. McLean et al., "Design and operation of a passively switched repetitive compact toroid plasma accelerator." Fusion Technology, vol. 33, pp. 252-272, May 1998. Each of the aforementioned publications is incorporated herein by reference in its entirety. Also, embodiments of the plasma generators described in United States Patent Application Publications No. 2006/0198483 and 2006/0198486, each of which is incorporated herein by reference in its entirety for all that is disclosed, can be used with embodiments of the plasma torus injector 34.
    [00041] The toroidal plasma generated by the plasma injector 34 can be a compact toroid, such as, for example, a spheromak, which is a toroidal plasma confined by its own magnetic field produced by the current flowing in the conductive plasma. In other embodiments, the compact toroid may be a plasma reverse field (FRC) configuration, which may have substantially closed magnetic field lines with little or no central penetration of the field lines.
    [00042] Some plasma torus injector designs can produce high density plasma with a strong internal magnetic field of a toroidal topology, which acts to confine charged plasma particles within the plasma core for a period that can be comparable or longer than the compression and recovery time. Injector embodiments can be configured to provide significant plasma preheating, for example, ohmically, or resistive heating by externally conducting currents and allowing partial decay of internal magnetic fields and / or direct heating of kinetic energy thermal injection ions , when the plasma comes to rest in the compression chamber 26.
    [00043] As schematically shown in FIG. 2, some embodiments of the plasma injector 34 may include several systems or regions: a plasma forming system 60, a plasma expansion region 62 and a plasma focusing / accelerating system or accelerator 64. In the embodiment shown in FIG. 2, the plasma acceleration / focusing system or accelerator 64 is limited by electrodes 48 and 50. One or both electrodes 48, 50 can be tapered or tapered to provide plasma compression as the plasma moves along the axis of the accelerator 64. In the illustrated embodiment, the forming system 60 has the largest diameter and includes a separate forming electrode 68, coaxial with the outer wall of the plasma forming system 60, which can be energized to ionize the injected gas through of a discharge of high voltage, high current, thus forming a plasma. Plasma forming system 60 may also have a set of one or more solenoid coils that produce the initial magnetic field prior to the ionization discharge, which then becomes incorporated within the plasma during formation. After being shaped by plasma processes during expansion and relaxation in the expansion region 60, the initial field can evolve into a set of closed magnetic flux toroidal surfaces, which can provide strong particles and energy confinement, which is mainly maintained by internal plasma currents.
    [00044] Once this magnetized plasma torus 36 has been formed, an acceleration current can be triggered from the conical central accelerator electrode 48 through the plasma and back along the external electrode 50. The Lorentz force (JxB) The resulting accelerates the plasma down from the accelerator 64. The plasma accelerator 64 can have an acceleration axis that is substantially collinear with the accelerator axis 40a. Conical, converging electrodes 48, 50 can cause the plasma to compress to a smaller radius (for example, at positions 36b, 36c, as schematically shown in FIG 1). In some embodiments, a radial compression factor of about 4 can be achieved from a medium sized injector 34, which is approximately 5 m long with an outside diameter of approximately 2 m. This can result in a density of injected plasma that can be about 64 times the original density in the expansion region of the injector, thereby providing the impact compression process with an initial high density initiation plasma. In other embodiments, the compression factor can be, for example, 2, 3, 5, 6, 7, 10 or more. In some embodiments, compression on the plasma accelerator is not used, and system 10 compresses the plasma primarily through the impact of the projectile on the plasma. In the illustrated embodiment, electrical energy for the formation, magnetization and acceleration of the plasma torus can be provided by the pulsed electrical energy system 52. The pulsed electrical energy system 52 may include a capacitor bank. In other embodiments, electrical energy can be applied in a standard manner, as described in, for example, JH Hammer, et al. "Experimental demonstration of acceleration and focusing of magnetically confined plasma rings", Physical Review Letters, vol. 61, n ° 25, pp 2843-2846, December 1988, which is incorporated by reference, in its entirety.
    [00045] Embodiments of the circulating liquid metal vessel 18 can be configured to have a substantially cylindrical central portion which is shown in cross section in FIG. 1, and which supports a liquid flow of liquid metal along the axial direction that enters the main chamber through a tapered opening 24 (conical nozzle) at one end and exits at the opposite end through a tube 20 or a set of those tubes. Also shown in FIG. 1 is an optional recirculating tube 30 for directing liquid metal 46 for projectile molds 32. Optionally, the recirculating tube 30 can be a separate tube from another region of vessel 18. In different embodiments, flow rates in the liquid metal 46 can vary from a few m / s to a few tens of m / s, and in some implementations, it can be advantageous for the substantially laminar flow to be maintained substantially throughout the system 10. To promote the laminar flow, alveolar elements can be incorporated in vessel 18. Directional vanes or hydrofoil structures can be used to direct the flow in the desired shape in the compression region. The cone angle of the converging flow can be chosen to improve the impact hydrodynamics for a given projectile-shaped cone angle. The recirculation vessel 18 can be made of materials with sufficient strength and thickness to be able to withstand the outgoing pressure wave emanating from the projectile impact and plasma compression event. Optionally, special flow elements near the outlet of vessel 18 (or in other suitable positions) can be used to dampen pressure waves that could cause damage to the heat exchange system. Optionally, heaters (not shown) can be used to increase the temperature of the liquid metal above its melting point for start-up operations or after maintenance cycles. In certain embodiments, the systems and methods for the flow of liquid metal disclosed in U.S. Patent Application Publications No. 2006/0198483 and 2006/0198486, each of which is incorporated by reference into this document in its entirety for all that reveals, can be used with system 10.
    [00046] During the acceleration and impact of projectiles there may be a significant momentum transfer, resulting in recoil forces applied to the apparatus structures. In some implementations, the mass of the fluid in volume in the recirculating vessel 18 may be sufficient (for example, greater than about 1000 times the mass of the projectile) so that the recoil forces of the impact can be addressed by assembling the vessel 18 in a set of hard shock absorbers so that the displacement of vessel 18 can be on the order of about one cm. Accelerator 40 can also experience a recoil reaction as it acts to accelerate the projectile. In some embodiments, the accelerator 40 may be a few hundred times as massive as the projectile 12, and the accelerator 40 may tend to experience correspondingly greater recoil accelerations, and full range of travel during firing, than vessel 18. With these relative finite movements, the three components of the system in the illustrated embodiment (for example, the accelerator 40, the plasma injector 34 and the recirculation vessel 18) can advantageously be joined by substantially flexible connections such as bellows, in order to maintain a desired vacuum and fluid seals. During the complete operation of some systems 10, the driving force can be approximately periodic at a frequency of a few Hz (for example, in a range from about 1 Hz to about 5 Hz). Therefore, it can be advantageous for the mechanical oscillator system (for example, mass, in addition to shock absorber springs), to be built to have a resonance frequency significantly different from the drive frequency and that strong damping is present.
    [00047] In some embodiments, the size of the recirculating vessel 18 may be such that the volume of liquid metal 46 around the maximum compression point 22 provides sufficient absorption of radiation by an absorbent element (e.g., lithium), so that there may be very little, if any, transfer of radiation to solid metallic structures of system 10. For example, in some embodiments, a net thickness of approximately 1.5 meters for a lead / lithium mixture of about 17% concentration Li's atomic atom can reduce the flow of radiation to the solid support structure by a factor of at least about 104.
    [00048] FIG. 3 shows cross-sectional diagrams (A - I) illustrating, schematically, a time sequence of an example of possible compression geometry during an impact of a projectile 12 on a fluid comprising liquid metal 46. The diagrams show the density of the fluid and material of the projectile during the impact event. The diagrams are based on a simulation using a finite non-viscous volume method in a fixed mesh, in which the plasma volume 36 has been added by hand to illustrate, schematically, the approximate collapse dynamics. In this example, before the time shown in diagram A, accelerator 40 launches projectile 12, which passes through sensors near the end of the pipe, which in turn triggers the firing sequence of the plasma injector. The plasma torus in this example can be injected steadily into the closing volume between the projectile 12 and the conical surface 27 of the compression chamber 26 formed in part by the flow of liquid metal 46. As projectile 12 impacts the compression chamber 26, the plasma torus 36, in this example, is substantially and uniformly compressed to a smaller radius in the conical compression chamber 26 formed by the flow of liquid metal. Plasma can be compressed so that there can be an increase in density (or pressure or temperature) by a factor of two or more, by a factor of four or more, by a factor of 10 or more, by a factor of 100 or more, or by some other factor.
    [00049] When the front end of the projectile 12 hits the surface 27 of the liquid metal (as shown in diagram A), the plasma 36 becomes sealed within a closed volume. As the projectile's edge begins to penetrate the liquid metal (for example, as shown in diagrams B, C and D) the compression rate increases. For a projectile impact speed at or exceeding the speed of sound in the liquid metal, the impact can produce a shock wave that moves with the projectile.
    [00050] The front surface of the projectile 12 may comprise a portion molded to increase the amount of compression. For example, in the illustrative simulation shown in FIG. 3, the projectile 12 comprises a front, concave, cone-shaped portion (see, for example, FIG. 4A). In some embodiments, the cone angle of the projectile can be selected to be substantially the same as the angle of the shock wave for a given impact speed. In some embodiments, this cone angle selection may be such that compression occurs during the projectile 12's deceleration time, rather than earlier, during the shock wave crossing, which may be in front of the projectile's surface 12 .
    [00051] Since projectile 12 first encounters resistance from the first impact, a compression wave 70 can be launched backward through the projectile causing mass compression of the projectile, while at the same time the normal impact force tends to cause a tapering of the projectile opening and the deformation process begins. At the outer edge of the projectile, possibly, a turbulent mat 72 may form in the liquid. As the projectile slows below the sound speed of the liquid metal (for example, diagram E), a compression wave 70 can also be launched forward in the flow of liquid metal. Peak plasma compression can occur after that compression wave has passed beyond the compression chamber 26 (for example, an F diagram). When the backward compression wave reaches the rear surface of the projectile, it can reflect, generating a decompression wave 74 that propagates forward through the projectile. After the decompression wave reaches the plasma containment cavity, the collapse of the inner wall surface may begin to decelerate in rhythm, stagnate in pressure, temperature and peak plasma magnetic field strength and then begin to re-expand, driven by the increased net pressures in the plasma.
    [00052] As an illustrative, non-limiting example, in the case of a 100 kg projectile traveling at an impact speed of 3 km / s, having a kinetic energy of 450 MJ there may be an energy transfer time of, approximately 200 microseconds, resulting in an average power of 2 x 1012 Watts. Since the peak compression time can be approximately half the energy transfer time, and there can be an angular divergence of energy in the fluid with approximately 1/3 of the energy going to compress the plasma at any given time. For example, in this illustrative simulation, there may be a maximum of about 1/6 of the total energy going to compress the plasma. Thus, in this illustrative simulation, about 75MJ of work would be done to compress the plasma. After the projectile becomes fully immersed in the flow of liquid metal, the projectile can develop fracture lines 76 and begin to split into smaller fragments, which melt into the flow over the span of several seconds or less.
    [00053] Projectile 12 shown in the simulations illustrated in FIG. 3 comprises a conical concave surface. There are other possible projectile designs that can provide different compression characteristics, and some examples of projectile designs 12a-12f are shown schematically in Figs. 4A-4F, respectively. The projectiles 12a-12f have a surface 13a-13f, respectively, that confines the liquid metal in the compression chamber 26. In some embodiments, the surface may be substantially conical, and portions of the surface may be concave or convex. Other surface shapes can be used, for example, portions of spheres, other conical sections, etc. In some embodiments, which comprise a conical surface, a possible parameter that can be adjusted to provide various models of concave surface is a cone angle, shown as angle Φ in Figs. 4A and 4B. The cone angle can be chosen to improve shock and flow dynamics as the projectile impacts the liquid metal coating. The cone angle Φ is greater in projectile 12a than in projectile 12f. The cone angle Φ can be about 20 degrees, about 30 degrees, about 40 degrees, about 45 degrees, about 50 degrees, about 60 degrees, or some other angle. In various embodiments, the cone angle Φ can be in the range of about 20 degrees to about 80 degrees, in the range of about 30 degrees to about 60 degrees, etc.
    [00054] In some embodiments, projectile 12c includes an elongated member 15 (for example, a center point; see FIG 4C), which can act to maintain the central electrode of the plasma injector 34. In some implementations of system 10, this elongated member 15 can prevent movement of the magnetized plasma torus when it exits the plasma injector 34. In some of these implementations, the plasma can advantageously be injected exactly when the front end of the tip 15 contacts the liquid metal 46 in the chamber of compression 26, and the plasma volume can be maintained in a substantially toroidal topology during compression. These implementations may advantageously allow for better magnetic confinement than a spherical collapse topology, but may have more areas of metal surface exposed directly to plasma, which can possibly increase impurity levels and decrease peak temperature plasma in some cases.
    [00055] In some projectile models, it is also possible to have plasma compression less dominated by the fluid shock effect using a 12d projectile properly modeled in a convex shape (see, for example FIG. 4D), which can compress the plasma by a significant fraction of total collapse time before the projectile crosses the surface of the liquid metal. To reduce or mitigate impurities in the plasma, the surface 13e of projectile 12e may comprise a coating 19 formed from a second material (see, for example, FIG. 4E), such as, for example, lithium or lithium-deuteride. Other parts of the projectile may include one or more coatings. Materials like these are generally less likely to have impurities that can lead, for example, to unwanted plasma cooling, if the impurities are dragged to the edge of the plasma. In some embodiments, multiple coatings can be used. In some models, the projectile may have features such as, for example, grooves and / or notches, around its surface to accommodate mechanical operation of the loading system, or as a seal for an accelerator air gun. Projectile 13f schematically illustrated in FIG. 4F has a groove 17 around the circumference of the rear end on which a reusable seal flange can be mounted, for example, during the initial casting of the projectile. In some embodiments using a pneumatic gun to accelerate the projectile 12f, firing of projectile 12f can occur when the propellant gas reaches sufficiently high pressure so that the ring behind the sealing flange can be cut, thereby releasing the projectile for acceleration , a little like the action of an explosion diaphragm on a conventional gas gun.
    [00056] FIG. 6 is a flow chart schematically illustrating an example embodiment of a method 100 of plasma compression in a liquid metal chamber using a projectile impact on the plasma. In block 104, a projectile 12 is accelerated towards a compression liquid metal compression chamber. The projectile can be accelerated using an accelerator, such as accelerator 40. For example, the accelerator can be a light gas gun or electromagnetic accelerator. The compression chamber can be formed of a liquid material, such as liquid metal. For example, in some implementations, at least a part of the compression chamber is formed by the flow of a liquid metal, as described herein with reference to FIG. 1. In block 108, a magnetized plasma is accelerated towards the liquid metal chamber. For example, the magnetized plasma can comprise a compact torus (for example, a spheromak or FRC). The magnetized plasma can be accelerated using the plasma torus accelerator 34 in some embodiments. In some of these embodiments, the magnetized plasma is generated and accelerated after the projectile has started accelerating towards the compression chamber, because the speed of the magnetized plasma can be much greater than the speed of the projectile. In block 112, the impact of the projectile on the liquid metal (when the plasma is in the compression chamber) compresses the magnetized plasma in the compression chamber. The plasma can be heated during compression. The projectile can break and melt into the liquid metal. In optional block 116, a portion of the liquid metal is recycled and used to form one or more new projectiles. For example, the liquid metal recirculation system and projectile plant 37 described with reference to FIG. 1 can be used for recycling. The new projectiles can be used in block 104 to provide a pulsed system for plasma compression.
    [00057] Embodiments of the system and method described above are suitable for applications in the study of high energy density plasma, including, for example, applications involving the study in the laboratory of astrophysical phenomena or nuclear weapons. Certain embodiments of the system and method described above can be used to compress a plasma that comprises fusion material sufficiently that useful neutron-producing and fusion reactions can take place. The gas used to form the plasma can comprise a fusion material. For example, the fusion material can comprise one or more isotopes of light elements, such as, for example, hydrogen isotopes (for example, deuterium and / or tritium), helium isotopes (for example, helium-3), and / or lithium isotopes (for example, lithium-6 and / or lithium-7). Other fusion materials can be used. Combinations of elements and isotopes can be used. Thus, certain embodiments of system 10 can be configured to act as a pulsed operation of high-flow neutron generators or neutron sources. Neutrons produced by embodiments of System 10 have a wide range of uses in research and industrial fields. For example, embodiments of system 10 can be used for the remediation of nuclear waste and the generation of medicinal nucleotides. In addition, embodiments of system 10 configured as a neutron source can also be used for materials research, either by testing a material's response (such as an external sample) to high-flux neutron exposure, or by introducing the sample of material in the compression region and subjecting the sample to extreme pressures, where the neutron flux can be used either as a diagnosis or as a means to transmute the material while under high pressure. Embodiments of system 10 configured as a neutron source can also be used for remote imaging of the internal structure of objects through neutron radiography and tomography, and can be advantageous for applications that require a rapid pulse (for example, several microseconds) neutrons with high luminosity.
    [00058] For some large-scale industrial applications, it may be economical to process multiple plasma compression systems in the same installation, in the event that some savings can accrue by having a single, shared projectile casting facility that recycles the liquid metal from more than one system, and then distributes the finished projectiles to the loading mechanisms at the opening of each accelerator. Some of these embodiments can be advantageous in that a failure in a single accelerator cannot bring the entire installation cycle to a halt, because the remaining compression devices can continue to operate. Additional Achievements and Examples
    [00059] The systems and methods described here can be incorporated in a wide variety of ways. For example, in one embodiment, a method for compressing a plasma is provided. The method includes (a) circulating a liquid metal through a vessel and directing the liquid metal through a nozzle to form a cavity, (b) generating and injecting a magnetized plasma torus into the liquid metal cavity, (c) acceleration of a projectile, having substantially the same composition as liquid metal, in the direction of the cavity so that it impacts on the magnetized plasma torus, through which the plasma is heated and compressed, and the projectile disintegrates and melts into the metal liquid. The method may also include (d) directing a portion of the liquid metal to a projectile-forming apparatus in which new projectiles are formed for use in step (c). One or more steps of the method can be performed repeatedly. For example, in some embodiments, steps (a) - (c) are repeated at a rate ranging from about 0.1 Hz to about 10 Hz.
    [00060] In some embodiments of the method, the cavity may be more or less conical in shape. In some embodiments, the liquid metal comprises a lead-lithium alloy. In some embodiments, the liquid metal comprises a lead-lithium alloy, with about 17% atomic concentration of lithium. In some embodiments, the liquid metal comprises a lead-lithium alloy with an atomic concentration of lithium in the range of about 5% to 20%. In some embodiments, the liquid metal can be circulated through a heat exchanger to reduce the temperature of the liquid metal.
    [00061] In some embodiments of the method, the plasma comprises a material that can be melted. In some embodiments, the material that can be melted comprises deuterium and / or tritium. In some embodiments, deuterium and tritium are supplied in a mixture of about 50% deuterium and about 50% tritium. In some embodiments of the method, the compression of the plasma results in the heating of the plasma and / or the production of neutrons and / or other types of radiation.
    [00062] An embodiment of a plasma compression system is provided. The system comprises a liquid metal recirculation subsystem comprising a containment vessel and a circulation pump to direct the liquid metal through a nozzle to form a cavity within the vessel. The system also comprises a plasma forming and injection device to repeatedly form a magnetized plasma torus and inject it into the metal cavity. The system also comprises a linear accelerator to direct projectiles, repeatedly, having substantially the same composition as the liquid metal, towards the cavity. The system also includes a projectile formation subsystem that comprises projectile-shaped molds in which new projectiles are formed and then directed to the linear accelerator, in which the molds are connected at least periodically to receive liquid metal, comprising molten projectiles, which are recirculated from the containment vessel.
    [00063] An embodiment of a plasma compression device is provided. The device comprises a linear accelerator for firing a projectile at high speed into a pipe coupled to a vacuum pump to create at least a partial vacuum inside the pipe. The system also comprises a conical focusing plasma injector having tapered coaxial electrodes connected to a power supply circuit to supply an electrical current. The electrodes can form a cone, tapering to a focusing region. The system also includes a coaxial magnetized plasma gun for material injection to generate a compact magnetized torus (for example, a spheromak), and the open end of the gun barrel can be seated inside the cone in conductive contact with the electrode internal. The system also includes a suitable recirculation vessel for containing the metal fluid and having an opening to receive the tapered accelerator cone and a base region, and a heat exchange line connected between the base and conical opening regions with a recirculation pump to pump fluid from the base to the conical opening. The tapered electrodes of the accelerator are seated inside the conical opening in such a way that the outer surface of the electrode guides a converging flow path to the pressurized metal fluid, creating a focusing region within the tapered fluid walls that confines and still concentrates the compact spheromak magnetized torus, which can be compressed to a maximum compression zone in the internal cavity of the vessel. When the recirculating vessel is filled with fluid metal and material that can be melted is injected, a projectile is fired by the gun to intercept the magnetized plasma ring when it has traveled close to the tapered fluid wall and compresses the plasma within the fluid to a increased pressure, thus transmitting kinetic energy to the plasma in order to increase the ion temperature.
    [00064] An embodiment of a plasma compression system includes an accelerator for firing a projectile towards a magnetized plasma (for example, a plasma torus) into a cavity in a solid metal or a liquid metal. The system can also include a plasma injector to generate the magnetized plasma and inject the magnetized plasma into the cavity. In embodiments comprising a cavity in the liquid metal, the system may include a vessel configured to contain the liquid metal and having a tapered nozzle to form the cavity through flow of the liquid metal. The magnetized plasma is injected into the cavity, and a projectile fired by the accelerator intercepts the plasma and compresses the plasma against the surface of the cavity, creating a high pressure impact event that compresses the magnetized plasma. Plasma compression can result in heating of the plasma. The impact of the projectile with the cavity can cause the projectile to disintegrate. In embodiments comprising a liquid metal cavity, the projectile can melt into the liquid metal. In some of these embodiments, a portion of the liquid metal can be deflected to shape new projectiles that can be used to maintain a repetitive firing cycle with a substantially closed inventory of liquid metal.
    [00065] Although particular elements, embodiments and applications of the present description have been shown and described, it will be understood that the scope of the description is not limited to them, since modifications can be made by those skilled in the art, without departing from the scope of the present description, particularly in the light of the aforementioned teachings. Thus, for example, in any method or process disclosed in this document, the acts or operations that make up the method / process can be performed in any appropriate sequence and are not necessarily limited to any particular disclosed sequence. Elements and components can be configured or arranged differently, combined, and / or eliminated in various embodiments. The different characteristics and processes described above can be used independently of each other, or can be combined in different ways. All possible combinations and sub-combinations are intended to be within the scope of this description. Reference throughout this description to "some embodiments", "an embodiment", or the like, means that a particular characteristic, structure, step, process, or characteristic described with respect to the embodiment is included in at least one embodiment. Thus, the meanings of the phrases "in some embodiments", "in one embodiment", or similar, throughout this description are not all, necessarily, referring to the same embodiment and may refer to one or more of the same or different embodiments . In fact, the new methods and systems described in this document can be realized in a variety of other ways; in addition, various omissions, additions, equivalent substitutions, re-dispositions and changes in the form of the embodiments described herein can be made without departing from the spirit of the inventions described here.
    [00066] Various aspects and advantages of the embodiments have been described here where appropriate. It must be understood that not necessarily all of these aspects or advantages can be achieved according to any particular embodiment. Thus, for example, it must be recognized that the various embodiments can be obtained in a way that achieves or optimizes an advantage or a group of advantages, as taught here, without necessarily arriving at other aspects or advantages that can be taught or suggested here.
    [00067] Conditional language used here, such as, among others, "may", "could", "could", "may", "for example" and the like, unless otherwise stated, or not understood within the context as used, it is generally intended to convey that certain embodiments include, while other embodiments do not include, certain characteristics, elements and / or steps. Thus, this conditional language is generally not intended to suggest that characteristics, elements and / or steps are somehow necessary for one or more embodiments, or that one or more embodiments necessarily include the logic to decide, with or without intervention or request by the operator, if these characteristics, elements and / or steps are included or are to be carried out in any particular embodiment. No feature or set of features is necessary or indispensable for any particular embodiment. The terms "comprising", "including", "having", and the like are synonymous and are even used, in an open way, and do not exclude additional elements, characteristics, acts, operations and so on. In addition, the term "or" is used in its broad sense (and not in its exclusive sense) so that when used, for example, to connect a list of elements, the term "from" means one, some or all elements in the list.
    [00068] The calculations, simulations, results, graphs, values and parameters of the embodiments described here are intended to illustrate and not to limit the disclosed embodiments. Other embodiments can be configured and / or operated differently from the examples described here.
    [00069] Thus, although certain example embodiments have been described, those embodiments have been presented by way of example only, and are not intended to limit the scope of the inventions disclosed in this document. Thus, nothing in the description above is intended to imply that any aspect, element, component, characteristic, stage, module or block is necessary or indispensable. In fact, the new methods and systems described in this document can be realized in a variety of other ways; in addition, various omissions, substitutions and changes in the form of the methods and systems described in this document can be made without departing from the spirit of the inventions disclosed in this document. The attached claims and their equivalents are intended to cover such forms or modifications that would affect the scope and spirit of some of the inventions disclosed in this document.
    权利要求:
    Claims (13)
    [0001]
    1. A plasma compression system comprising: a plasma injector (34) comprising: - a plasma formation system (60) configured to generate a magnetized plasma (36); and - a plasma accelerator (64) having a first portion (36a), a second portion (36c), and a longitudinal axis between the first portion and the second portion, the plasma accelerator (64) configured to receive the plasma ( 36) magnetized in the first portion (36a) and accelerate the magnetized plasma (36) along the longitudinal axis towards the second portion (36c); the system being characterized by: - a liquid metal circulation system configured to supply liquid metal (46) forming at least a portion of a chamber (26) configured to receive the magnetized plasma (36) from the second accelerator portion (36c) plasma (64), the plasma (36) magnetized having a first pressure when received in the chamber (26); and - a projectile accelerator (40) configured to accelerate a projectile (12) along at least a portion of the longitudinal axis towards the chamber (26), and a timing system configured to coordinate the acceleration of the plasma (36) magnetized and the acceleration of the jet (12); wherein the system is configured such that the projectile (12) compresses the magnetized plasma (36) in the chamber (26), the compressed magnetized plasma (36) having a second pressure which is greater than the first pressure.
    [0002]
    2. System according to claim 1, characterized in that the projectile accelerator (40) comprises a gas gun (40) configured to accelerate (12) the projectile using a pressurized gas.
    [0003]
    3. System according to claim 2, characterized in that the gas gun (40) comprises a valve system (42) configured to evacuate, at least partially, a region in front of the projectile (12), in which the valve system (42) is configured to be synchronized so that a high pressure region is maintained behind the projectile (12) and a low pressure region is maintained in front of the projectile (12).
    [0004]
    4. System according to claim 1, characterized in that the projectile accelerator comprises an electromagnetic accelerator.
    [0005]
    5. System, according to claim 1, characterized by the fact that the projectile (12a, b, c, d, e, f) comprises a surface (13a, b, c, d, e, f) configured to confine the plasma (36) magnetized in the chamber (26), the surface comprising a conical shape, in which the conical shape is concave and has a cone angle in a range of about 20 degrees to about 80 degrees.
    [0006]
    6. System according to claim 1, characterized in that the projectile (12c) comprises a surface (13c) configured to confine the magnetized plasma (36) in the chamber (26), the surface (13c) comprising an elongated element (15) extending along a longitudinal geometric axis of the projectile (12c).
    [0007]
    7. System according to claim 1, characterized in that the projectile (12e) comprises a surface (13e) configured to confine the magnetized plasma (36) in the chamber (26), the surface (13e) comprising one or more coatings (19), at least one of the coatings (13) comprising lithium or lithium-deuteride.
    [0008]
    8. System according to claim 1, characterized in that the liquid metal circulation system comprises a tapered nozzle (24) configured to exit a flow of liquid metal and a pump system (14) configured to provide a flow of liquid metal (46) to a containment system, the flow configured to form at least a portion of the chamber (26), wherein the chamber (26) in the liquid metal (46) has a substantially conical shape.
    [0009]
    9. System according to claim 1, characterized in that it also comprises a projectile recycling system configured to receive a portion of the liquid metal (46) and to form one or more projectiles (12) of the received portion of the liquid metal (46).
    [0010]
    10. System according to claim 9, characterized in that the projectile recycling system comprises a loading mechanism (38) configured to automatically load a projectile (12) recycled on the projectile accelerator (40).
    [0011]
    11. Plasma compression method comprising: - generating a toroidal plasma (36); - accelerate the toroidal plasma (36) towards a cavity (26) in a liquid metal (46); the method being characterized by the fact that: - accelerating a projectile (12) towards the cavity (26) in the liquid metal (46); and - compressing the toroidal plasma (36) with the projectile (12), while the toroidal plasma (36) is in the cavity (26) in the liquid metal (46).
    [0012]
    12. Method according to claim 11, characterized in that it also comprises the formation of the cavity (26) in the liquid metal (46), in which the formation of the cavity (26) comprises the circulation of a liquid metal (46) to form the cavity (26).
    [0013]
    13. Method according to claim 11, characterized in that it still comprises the recycling of a portion of the liquid metal (46) to form at least one new projectile (12)
    类似技术:
    公开号 | 公开日 | 专利标题
    BR112012002147B1|2020-12-22|systems and methods for plasma compression with projectile recycling
    JP6023876B2|2016-11-09|Method for generating high specific thrust and moderate thrust from fusion power rocket engine
    Thio2008|Status of the US program in magneto-inertial fusion
    US20130058446A1|2013-03-07|Continuous fusion due to energy concentration through focusing of converging fuel particle beams
    Winterberg2010|The Release of Thermonuclear Energy by Inertial Confinement: Ways Towards Ignition
    US20130064340A1|2013-03-14|Method and System to Remove Debris from a Fusion Reactor Chamber
    Clery2019|Alternatives to tokamaks: a faster-better-cheaper route to fusion energy?
    Turchi2018|Review of controlled fusion power at megagauss field levels
    Ryutov et al.2006|Plasma liner with an intermediate heavy shell and thermal pressure drive
    US20180254153A1|2018-09-06|Apparatus for plasma confinement and for ion separation
    Vyas et al.2020|Numerical modeling of compact toroid formation and propagation for magneto-inertial fusion research
    Perkins et al.2004|On the utility of antiprotons as drivers for inertial confinement fusion
    Thio2008|Magneto-inertial fusion: An emerging concept for inertial fusion and dense plasmas in ultrahigh magnetic fields
    Winterberg2019|Coriolis force-assisted inertial confinement fusion
    KR20140012519A|2014-02-03|Nuclear fusion power by hypervelocity bullet collision
    Ligon1998|The World's Simplest Fusion Reactor, And How to Make It Work
    JPWO2019168030A1|2021-02-25|Fusion system, fusion method, transmutation shortening treatment system for long-lived fission products, and transmutation shortening treatment method for long-lived fission products
    JP7018222B2|2022-02-10|Fusion system, fusion method, nuclide conversion short-lived treatment system for long-lived fission products and nuclide conversion short-lived treatment method for long-lived fission products
    Gebhart III2013|A Computational Study of a Lithium Deuteride Fueled Electrothermal Plasma Mass Accelerator
    ES2727006A1|2019-10-11|NUCLEAR FUSION REACTOR FOR MAGNETICALLY CONFINED REACTIONS |
    Kirtley et al.2013|Neutral Entrainment Demonstration in a Xenon FRC Thruster Experiment
    Slough2015|Inductively Driven, 3D Liner Compression of a Magnetized Plasma to Megabar Energy Densities
    KR20140123177A|2014-10-22|Nuclear fusion power by plasma and hypervelocity bullet
    Winterberg2006|Magnetic booster fast ignition macron accelerator
    Obousy0|Project Icarus
    同族专利:
    公开号 | 公开日
    JP5363652B2|2013-12-11|
    RU2012101217A|2013-09-10|
    KR101488573B1|2015-02-02|
    US20110026658A1|2011-02-03|
    EP2460160B8|2013-12-04|
    EP2460160A1|2012-06-06|
    WO2011014577A1|2011-02-03|
    JP2013501314A|2013-01-10|
    EP2460160B1|2013-06-05|
    US20160150627A1|2016-05-26|
    CA2767904C|2014-10-14|
    US8891719B2|2014-11-18|
    US20150036777A1|2015-02-05|
    CN102483959A|2012-05-30|
    IN2012DN00841A|2015-06-26|
    CA2767904A1|2011-02-03|
    US9271383B2|2016-02-23|
    CN102483959B|2014-09-24|
    US20110243292A1|2011-10-06|
    RU2535919C2|2014-12-20|
    KR20120039740A|2012-04-25|
    BR112012002147A2|2020-08-04|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US2715389A|1949-12-19|1955-08-16|Hartford Special Machinery Co|Hydro-pneumatic power mechanisms and cycling controls therefor|
    BE538825A|1954-06-15|1900-01-01|
    GB825026A|1956-09-14|1959-12-09|Schmidt Paul|An arrangement for the production of shock waves in rapid sequence inside a shock wave chamber|
    US4207154A|1957-06-27|1980-06-10|Lemelson Jerome H|Wave generating apparatus and method|
    US4367130A|1970-11-30|1983-01-04|Lemelson Jerome H|Chemical reaction|
    US4385880A|1957-06-27|1983-05-31|Lemelson Jerome H|Shock wave processing apparatus|
    US2992345A|1958-03-21|1961-07-11|Litton Systems Inc|Plasma accelerators|
    US2953718A|1958-05-01|1960-09-20|Plasmadyne Corp|Apparatus and method for generating high temperatures|
    US2939048A|1958-05-29|1960-05-31|Plasmadyne Corp|Apparatus for creating extremely high temperatures|
    US2991238A|1958-06-19|1961-07-04|James A Phillips|Pinched plasma reactor|
    US3313707A|1959-05-04|1967-04-11|Amsler Joachim|Apparatus for compressing and heating a plasma containing a fusionable material|
    US3189523A|1961-03-27|1965-06-15|Avco Corp|Means for producing high temperature plasma|
    GB1029558A|1961-12-08|1966-05-11|Houdaille Industries Inc|Improvements in or relating to hydraulic buffers|
    US3338788A|1962-01-22|1967-08-29|Euratom|Apparatus for producing high intensity magnetic fields for use in controlled thermonuclear reactions|
    DE1251879B|1962-08-20|
    DE1212229B|1963-11-28|1966-03-10|Schmidt Paul|Method for treating substance introduced into the inner area of a shock wave space, in particular for converting the substance into the plasma state|
    US3309967A|1965-01-25|1967-03-21|John F Taplin|Rolling diaphragm devices having loose coupling between piston and piston rod to render the piston floating|
    US3465742A|1966-11-03|1969-09-09|Theodore R Herr|Air pressure operated ball pitching device|
    DE1282886B|1967-03-22|1968-11-14|Fichtel & Sachs Ag|Hydropneumatic lifting unit|
    US3631760A|1969-12-05|1972-01-04|Us Navy|Pneumatic torpedo launcher with hydraulic operated snubber|
    US3624239A|1970-02-11|1971-11-30|Atomic Energy Commission|Pulsed laser-ignited thermonuclear reactor|
    US3753304A|1971-02-02|1973-08-21|Energy Sciences Inc|Pressure wave generator|
    US3973468A|1973-11-21|1976-08-10|Russell Jr Wayne B|Multi-stage extendible and contractible shaft with shock absorption|
    US4026192A|1971-11-12|1977-05-31|Atlas Copco Aktiebolag|Motor driven by a pressurized fluid medium for operating an impacting tool in a linear direction|
    US3990351A|1972-03-10|1976-11-09|Atlas Copco Aktiebolag|Pneumatic impact device|
    US3748226A|1972-05-18|1973-07-24|Atomic Energy Commission|Pulsed high beta fusion reactor|
    JPS554519B2|1972-10-06|1980-01-30|
    US4182650A|1973-05-17|1980-01-08|Fischer Albert G|Pulsed nuclear fusion reactor|
    US3925990A|1973-08-28|1975-12-16|Us Air Force|Shock heated, wall confined fusion power system|
    US4269659A|1973-09-12|1981-05-26|Leon Goldberg|Neutron generator|
    US5015432A|1973-10-24|1991-05-14|Koloc Paul M|Method and apparatus for generating and utilizing a compound plasma configuration|
    US5041760A|1973-10-24|1991-08-20|Koloc Paul M|Method and apparatus for generating and utilizing a compound plasma configuration|
    US4023065A|1973-10-24|1977-05-10|Koloc Paul M|Method and apparatus for generating and utilizing a compound plasma configuration|
    JPS50120100U|1974-03-15|1975-10-01|
    NL7405069A|1974-04-16|1975-10-20|Philips Nv|PROCESS FOR THE MANUFACTURE OF METAL ARTICLES WITH A CORROSION BY A LEAD CONTAINING METAL MELT PROTECTIVE LAYER OF ZIRCOON NITRIDE AND OBJECT OBTAINED BY THIS PROCESS.|
    US4012166A|1974-12-04|1977-03-15|Deere & Company|Supersonic shock wave compressor diffuser with circular arc channels|
    US4158598A|1975-04-21|1979-06-19|The United States Of America As Represented By The United States Department Of Energy|Parabolic lithium mirror for a laser-driven hot plasma producing device|
    US4269658A|1975-10-14|1981-05-26|General Atomic Company|Mechanical compression plasma device|
    US4305784A|1977-02-14|1981-12-15|The United States Of America As Represented By The United States Department Of Energy|Tokamak with mechanical compression of toroidal magnetic field|
    US4068147A|1975-11-06|1978-01-10|Wells Daniel R|Method and apparatus for heating and compressing plasma|
    CH607236A5|1975-11-12|1978-11-30|Friedwardt Winterberg|Thermonuclear micro:explosion generated by shock wave|
    US4129772A|1976-10-12|1978-12-12|Wisconsin Alumni Research Foundation|Electrode structures for high energy high temperature plasmas|
    US4363775A|1976-12-30|1982-12-14|International Nuclear Energy Systems Co.|Controlled nuclear fusion apparatus|
    FR2388284B1|1977-04-22|1982-05-21|Nal Pour Expl Oceans Centre|
    US4252605A|1977-08-15|1981-02-24|General Atomic Company|Self-imploding liner system for magnetic field compression|
    US4217171A|1977-08-15|1980-08-12|General Atomic Company|Blanket design for imploding liner systems|
    US4166760A|1977-10-04|1979-09-04|The United States Of America As Represented By The United States Department Of Energy|Plasma confinement apparatus using solenoidal and mirror coils|
    US4140057A|1978-05-02|1979-02-20|The United States Of America As Represented By The Secretary Of The Navy|Axisymmetric stabilized liner implosion system|
    US4563341A|1978-05-19|1986-01-07|Flynn Hugh G|Method and means for converting graphite to diamond|
    US4333796A|1978-05-19|1982-06-08|Flynn Hugh G|Method of generating energy by acoustically induced cavitation fusion and reactor therefor|
    CA1162333A|1978-06-06|1984-02-14|Paul M. Koloc|Method and apparatus for generating and utilizing acompound plasma configuration|
    AU523583B2|1978-07-13|1982-08-05|Interx Research Corp.|Thiazolidine prodrugs|
    US4290848A|1978-08-25|1981-09-22|Cornell Research Foundation, Inc.|Ion-ring ignitor for inertial fusion|
    US4304627A|1978-09-28|1981-12-08|Texas Gas Transmission Corporation|Expandable chamber fusion reactor system|
    US4342720A|1978-10-24|1982-08-03|Trisops, Inc.|Method and apparatus for generation of thermonuclear power|
    US4449892A|1978-11-08|1984-05-22|Bentley Arthur P|Pump with rotary sonic pressure wave generator|
    US4277305A|1978-11-13|1981-07-07|The United States Of America As Represented By The United States Department Of Energy|Beam heated linear theta-pinch device for producing hot plasmas|
    US4263095A|1979-02-05|1981-04-21|The United States Of America As Represented By The United States Department Of Energy|Device and method for imploding a microsphere with a fast liner|
    US4292126A|1979-02-28|1981-09-29|The United States Of America As Represented By The United States Department Of Energy|Tokamak with liquid metal for inducing toroidal electrical field|
    US4228380A|1979-03-16|1980-10-14|Trisops Inc.|Method and apparatus for heating and compressing plasma|
    US4292568A|1979-03-16|1981-09-29|Triosops, Inc.|Method and apparatus for heating and compressing plasma|
    US4257798A|1979-07-26|1981-03-24|The United States Of America As Represented By The United States Department Of Energy|Method for introduction of gases into microspheres|
    US4284164A|1979-12-21|1981-08-18|Atlantic Richfield Company|Acoustic pulse generator|
    US4328070A|1980-03-03|1982-05-04|Winterberg Friedwardt M|Method for the initiation of fusion reactions for the controlled release of energy|
    US4435354A|1980-10-14|1984-03-06|Winterberg Friedwardt|Method for the release of thermonuclear energy combining impact, magnetic and inertial confinement fusion|
    JPS5822675Y2|1980-10-22|1983-05-14|
    US4390322A|1981-02-10|1983-06-28|Tadeusz Budzich|Lubrication and sealing of a free floating piston of hydraulically driven gas compressor|
    US4643854A|1982-04-26|1987-02-17|California Institute Of Technology|Shell forming system|
    US4534263A|1982-07-19|1985-08-13|Westinghouse Electric Corp.|Electromagnetic launcher with high repetition rate switch|
    JPS632607Y2|1982-12-10|1988-01-22|
    US4735762A|1983-09-29|1988-04-05|The United States Of America As Represented By The United States Department Of Energy|Laser or charged-particle-beam fusion reactor with direct electric generation by magnetic flux compression|
    US4790735A|1983-10-03|1988-12-13|Kms Fusion, Inc.|Materials processing using chemically driven spherically symmetric implosions|
    JPH056016B2|1984-02-10|1993-01-25|Sutabiraizaa Kk|
    US5430776A|1984-08-09|1995-07-04|Stauffer; J. Christian|Fuel pellets for thermonuclear reactions|
    US6418177B1|1984-08-09|2002-07-09|John E Stauffer|Fuel pellets for thermonuclear reactions|
    JPS61116683U|1984-12-28|1986-07-23|
    IT1187318B|1985-02-22|1987-12-23|Franco Zanarini|VOLUMETRIC ALTERNATE COMPRESSOR WITH HYDRAULIC OPERATION|
    AT383067B|1985-04-09|1987-05-11|Roller Johannes|BULLET CHILLER|
    US5087435A|1987-05-26|1992-02-11|California Institute Of Technology|Polycrystalline diamond and method for forming same|
    DE3802500C1|1988-01-28|1989-06-22|Roboflex Ag, Weinfelden, Ch|
    WO1990013129A2|1989-04-10|1990-11-01|Massachusetts Institute Of Technology|Fusion apparatus|
    AU6068190A|1989-04-17|1990-11-16|Richard C. Auchterlonie|Magnetic fusion reactor and ignition method|
    WO1990014670A1|1989-05-02|1990-11-29|Electric Power Research Institute, Inc.|Isotope deposition, stimulation, and direct energy conversion for nuclear fusion in a solid|
    US5114261A|1989-07-31|1992-05-19|Honda Giken Kogyo Kabushiki Kaisha|Swashplate type hydraulic device having a ball joint connection|
    JPH0367196A|1989-08-05|1991-03-22|Akihiro Fujimura|Experimenting device for nuclear fusion|
    DE3942542C2|1989-12-22|1992-12-03|Lungu Cornelius|
    JPH03226694A|1990-02-01|1991-10-07|Semiconductor Energy Lab Co Ltd|Method of electro-chemical low temperature nuclear fusion|
    US5160695A|1990-02-08|1992-11-03|Qed, Inc.|Method and apparatus for creating and controlling nuclear fusion reactions|
    GB9003390D0|1990-02-14|1990-04-11|Univ Manchester|Method of generating energy|
    US5227239A|1990-11-30|1993-07-13|The United States Of America As Represented By The United States Department Of Energy|Production of hollow aerogel microspheres|
    CA2031841A1|1990-12-10|1992-06-11|Bruno A. A. Krawzik|Ultrasonic fusion of deuterium and deuterium mixed with tritium|
    US20020090047A1|1991-10-25|2002-07-11|Roger Stringham|Apparatus for producing ecologically clean energy|
    WO1993023587A1|1992-05-19|1993-11-25|Igenwert Gmbh|Process and device for applying pulses on the surface of a solid body|
    US5526885A|1992-08-19|1996-06-18|Aktsionernoe Obschestvo Zakrytogo Tipa "Rossiiskaya Patentovannaya Tekhnika" |Hydraulic device for driving piles|
    US5305091A|1992-12-07|1994-04-19|Oreo Products Inc.|Optical coordinate measuring system for large objects|
    JPH06317684A|1993-01-05|1994-11-15|Masutaazu Shoji Kk|Takeout method of low-temperature nuclear fusion reaction energy|
    WO1994016446A1|1993-01-07|1994-07-21|Jerome Drexler|Self-catalyzed nuclear fusion of lithium-6 and deuterium using alpha particles|
    US5992354A|1993-07-02|1999-11-30|Massachusetts Institute Of Technology|Combustion of nanopartitioned fuel|
    WO1995003611A1|1993-07-26|1995-02-02|Diego Orellana Hurtado|Generator for nuclear fusion by centripetal compression|
    CA2104939A1|1993-08-26|1995-04-15|Bruno A. A. Krawzik|Ultrasonic fusion of deuterium and deuterium mixed with tritium 1:1, and deuterium compounds and tritium compounds|
    US5858104A|1993-09-30|1999-01-12|The United States Of America As Represented By The Secretary Of The Navy|System for focused generation of pressure by bubble formation and collapse|
    US5429030A|1993-11-09|1995-07-04|Gt-Devices|Hybrid electrothermal light gas gun and method|
    WO1995016995A1|1993-12-03|1995-06-22|E-Quest Sciences|Method for producing heat|
    JP2500374B2|1993-12-17|1996-05-29|核融合科学研究所長|Continuous multi-stage acceleration coaxial gun|
    US5397961A|1993-12-20|1995-03-14|Ayers; Richard A.|Apparatus for generating a pulsed plasma in a liquid medium|
    JPH07201497A|1993-12-29|1995-08-04|Kobe Steel Ltd|Coaxial type electromagnetic accelerating flame spraying device|
    US5659173A|1994-02-23|1997-08-19|The Regents Of The University Of California|Converting acoustic energy into useful other energy forms|
    CA2124364A1|1994-05-26|1995-11-27|Emilio Panarella|Process and apparatus for radiation generation|
    WO1996021230A1|1995-01-06|1996-07-11|Rensselaer Polytechnic Institute|A nonperiodically forced bubble fusion reactor|
    WO1996023400A2|1995-01-26|1996-08-08|Pless Irwin A|A method and apparatus for generating large velocity, high pressure, and high temperature conditions|
    GB9509982D0|1995-05-17|1995-08-02|Browne Peter F|Shock wave fusion reactor|
    US5920394A|1995-09-01|1999-07-06|Research Corporation Technologies, Inc.|Optical coordinate measuring machine|
    US6628740B2|1997-10-17|2003-09-30|The Regents Of The University Of California|Controlled fusion in a field reversed configuration and direct energy conversion|
    US6894446B2|1997-10-17|2005-05-17|The Regents Of The University Of California|Controlled fusion in a field reversed configuration and direct energy conversion|
    AT254333T|1995-09-25|2003-11-15|Paul M Koloc|DEVICE FOR PRODUCING A PLASMA|
    US5818498A|1995-10-16|1998-10-06|Creo Products Inc.|Method of multi-channel thermal recording|
    JP3073436B2|1996-01-05|2000-08-07|三菱重工業株式会社|Control method of fusion plasma|
    AU3384297A|1996-06-11|1998-01-14|American Technologies Group, Inc.|A method for generating nuclear fusion through high pressure|
    US5821705A|1996-06-25|1998-10-13|The United States Of America As Represented By The United States Department Of Energy|Dielectric-wall linear accelerator with a high voltage fast rise time switch that includes a pair of electrodes between which are laminated alternating layers of isolated conductors and insulators|
    US5811944A|1996-06-25|1998-09-22|The United States Of America As Represented By The Department Of Energy|Enhanced dielectric-wall linear accelerator|
    AU3911997A|1996-08-05|1998-02-25|Tetra Corporation|Electrohydraulic pressure wave projectors|
    IT1292817B1|1997-03-20|1999-02-11|Renzo Boscoli|METHOD AND MACHINE FOR THE PRODUCTION OF ENERGY BY NUCLEAR FUSION REACTIONS.|
    WO2000058989A1|1999-03-31|2000-10-05|Science Research Laboratory, Inc.|Plasma gun and methods for the use thereof|
    US6252662B1|1997-10-14|2001-06-26|Canon Kabushiki Kaisha|Projection exposure apparatus and device manufacturing method using the same|
    JPH11144890A|1997-11-06|1999-05-28|Mitsubishi Heavy Ind Ltd|Plasma generation accelerator|
    AU1995899A|1997-11-12|1999-05-31|Board Of Trustees Of The University Of Illinois, The|Inertial electrostatic confinement fusion device with gate-valve pulsing|
    WO1999056284A2|1998-04-29|1999-11-04|Herzel Laor|Method and apparatus for compressing a bose-einstein condensate of atoms|
    US6411666B1|1998-10-21|2002-06-25|The United States Of America As Represented By The United States Department Of Energy|Method and apparatus to produce and maintain a thick, flowing, liquid lithium first wall for toroidal magnetic confinement DT fusion reactors|
    JP3122081B2|1998-11-25|2001-01-09|石油公団|Neutron generator tube|
    US6252622B1|1999-01-06|2001-06-26|Creo Products Inc.|Fault tolerant laser diode array|
    US6377739B1|1999-03-09|2002-04-23|Creo Srl|Two dimensional fiber optic output array|
    US6181362B1|1999-03-11|2001-01-30|Creo Srl|Fault tolerant laser diode array|
    US6587211B1|1999-07-28|2003-07-01|Creo Srl|Interferometric torque and power sensor|
    US6784591B2|1999-11-19|2004-08-31|Robert M. L. Baker, Jr.|Gravitational wave generator utilizing submicroscopic energizable elements|
    AU2724801A|1999-11-24|2001-06-04|Impulse Devices, Inc.|A new and improved system for removing heat from a cavitation nuclear reactor|
    AU3072901A|1999-11-24|2001-06-04|Impulse Devices, Inc.|Materials for enhancing nuclear cavitation reactions and processes for making the same|
    AU3262501A|1999-11-24|2001-06-04|Impulse Devices, Inc.|Cavitation nuclear reactor and method of operating same|
    AU2905801A|1999-11-24|2001-06-04|Impulse Devices, Inc.|A composite reactor assembly for a cavitation nuclear reactor|
    AU2905301A|1999-11-24|2001-06-04|Impulse Devices, Inc.|A liquid based cavitation nuclear reactor including a system for externally processing the reactor liquid|
    WO2001039199A2|1999-11-24|2001-05-31|Impulse Devices, Inc.|Enhancing electrolytic cavitation reactions|
    WO2001039198A2|1999-11-24|2001-05-31|Impulse Devices, Inc.|Cavitation nuclear reactor system|
    AU3435001A|1999-11-24|2001-06-04|Impulse Devices, Inc.|A new and improved system for facilitating heat removal from a cavitation nuclear reactor|
    US6593539B1|2000-02-25|2003-07-15|George Miley|Apparatus and methods for controlling charged particles|
    US6408052B1|2000-04-06|2002-06-18|Mcgeoch Malcolm W.|Z-pinch plasma X-ray source using surface discharge preionization|
    WO2002005292A2|2000-07-06|2002-01-17|Yensen Robert M|Controlled-nuclear-fusion apparatus|
    US20020101949A1|2000-08-25|2002-08-01|Nordberg John T.|Nuclear fusion reactor incorporating spherical electromagnetic fields to contain and extract energy|
    JP2002147260A|2000-11-14|2002-05-22|Honda Motor Co Ltd|Electromagnetic valve control device|
    US6680480B2|2000-11-22|2004-01-20|Neil C. Schoen|Laser accelerator produced colliding ion beams fusion device|
    US6664740B2|2001-02-01|2003-12-16|The Regents Of The University Of California|Formation of a field reversed configuration for magnetic and electrostatic confinement of plasma|
    US6611106B2|2001-03-19|2003-08-26|The Regents Of The University Of California|Controlled fusion in a field reversed configuration and direct energy conversion|
    US6842553B2|2001-04-17|2005-01-11|Creo Srl|Method for cross-connecting optical signals at high speed|
    US6660997B2|2001-04-26|2003-12-09|Creo Srl|Absolute position Moiré type encoder for use in a control system|
    US6941035B2|2001-04-26|2005-09-06|Creo Srl|Optical cross-connect switch|
    US6763160B2|2001-04-26|2004-07-13|Creo Srl|Optical cross connect switch having improved alignment control system|
    US20030002611A1|2001-05-18|2003-01-02|Wilson Greatbatch|3He reactor with direct electrical conversion|
    WO2002097823A1|2001-05-25|2002-12-05|Ut-Battelle, Llc|Methods and apparatus to induce d-d and d-t reactions|
    US6832552B2|2001-06-26|2004-12-21|Creo Inc.|Method of automated setting of imaging and processing parameters|
    US8090071B2|2001-08-08|2012-01-03|James Robert DeLuze|Apparatus for hot fusion of fusion-reactive gases|
    US6532887B1|2001-10-01|2003-03-18|The United States Of America As Represented By The Secretary Of The Navy|Small device launch system|
    US20030074010A1|2001-10-17|2003-04-17|Taleyarkhan Rusi P.|Nanoscale explosive-implosive burst generators using nuclear-mechanical triggering of pretensioned liquids|
    AUPR831501A0|2001-10-18|2001-11-08|Symons, Ian Robert|Fusion reactor|
    US6665048B2|2002-01-22|2003-12-16|Creo Inc.|Method for imaging a continuously moving object|
    US20050129161A1|2002-03-12|2005-06-16|Michel Laberge|Apparatus and method for fusion reactor|
    US6870894B2|2002-04-08|2005-03-22|The Regents Of The University Of California|Compact neutron generator|
    US20030215046A1|2002-05-16|2003-11-20|Hornkohl Jason L.|Pressure generating structure|
    CN1295946C|2002-08-14|2007-01-17|质子－21有限公司|Method and device for compressing a substance by impact and plasma cathode thereto|
    US6837145B1|2002-12-18|2005-01-04|Air Power Systems Co., Inc.|Fluid powered actuator|
    US20040141578A1|2003-01-16|2004-07-22|Enfinger Arthur L.|Nuclear fusion reactor and method|
    DE10304711B4|2003-02-06|2007-10-18|Daimlerchrysler Ag|Method for controlling a solenoid valve, in particular for an automatic transmission of a motor vehicle|
    US20050271181A1|2003-04-24|2005-12-08|Board Of Regents Of The University And Community College System Of Nevada|Apparatus and method for ignition of high-gain thermonuclear microexplosions with electric-pulse power|
    WO2005004555A1|2003-06-27|2005-01-13|Commissariat A L'energie Atomique|Method and device for producing extreme ultraviolet radiation or soft x-ray radiation|
    DE10356404B4|2003-12-03|2005-10-06|Danfoss Compressors Gmbh|piston assembly|
    US7173385B2|2004-01-15|2007-02-06|The Regents Of The University Of California|Compact accelerator|
    US7180082B1|2004-02-19|2007-02-20|The United States Of America As Represented By The United States Department Of Energy|Method for plasma formation for extreme ultraviolet lithography-theta pinch|
    US7559542B2|2004-08-19|2009-07-14|Diebolt International, Inc.|Low impact gas spring|
    US20090152094A1|2004-11-30|2009-06-18|Zakrytoe Aktsionernoe Obschestvo Rustermosintez|Method of forming stable states of dense high-temperature plasma|
    US20070058770A1|2004-11-30|2007-03-15|Fissenko Stanislav I|Method of forming stable states of sense high-temperature plasma|
    WO2006074427A2|2005-01-07|2006-07-13|Board Of Regents Of The Nevada System Of Higher Education, On Behalf Of The University Of Nevada, Reno|Amplification of energy beams by passage through an imploding liner|
    ITRM20050047A1|2005-02-03|2006-08-04|Gioscia Maria Chiara|PROCEDURE FOR THE PRODUCTION OF ENERGY AND APPARATUS FOR ITS IMPLEMENTATION.|
    US7679025B1|2005-02-04|2010-03-16|Mahadevan Krishnan|Dense plasma focus apparatus|
    US7510321B2|2005-02-28|2009-03-31|Impulse Devices, Inc.|Hydraulic actuated cavitation chamber|
    US20060198487A1|2005-03-04|2006-09-07|General Fusion Inc.|Fusionable material target|
    US20060198483A1|2005-03-04|2006-09-07|General Fusion Inc.|Magnetized plasma fusion reactor|
    US20060198486A1|2005-03-04|2006-09-07|Laberge Michel G|Pressure wave generator and controller for generating a pressure wave in a fusion reactor|
    CN101189684B|2005-03-07|2013-04-24|加州大学评议会|Plasma electric generation system|
    US8031824B2|2005-03-07|2011-10-04|Regents Of The University Of California|Inductive plasma source for plasma electric generation system|
    US9607719B2|2005-03-07|2017-03-28|The Regents Of The University Of California|Vacuum chamber for plasma electric generation system|
    US9123512B2|2005-03-07|2015-09-01|The Regents Of The Unviersity Of California|RF current drive for plasma electric generation system|
    US7679027B2|2005-03-17|2010-03-16|Far-Tech, Inc.|Soft x-ray laser based on z-pinch compression of rotating plasma|
    JP4769014B2|2005-04-28|2011-09-07|学校法人日本大学|Coaxial magnetized plasma generator and film forming apparatus using coaxial magnetized plasma generator|
    GB2426862B|2005-06-04|2007-04-11|Alan Charles Sturt|Thermonuclear power generation|
    US7372059B2|2005-10-17|2008-05-13|The University Of Washington|Plasma-based EUV light source|
    US7825391B2|2005-10-17|2010-11-02|The University Of Washington|Plasma-based EUV light source|
    US7831008B2|2005-10-21|2010-11-09|General Atomics|Microwave-powered pellet accelerator|
    US7482607B2|2006-02-28|2009-01-27|Lawrenceville Plasma Physics, Inc.|Method and apparatus for producing x-rays, ion beams and nuclear fusion energy|
    CA2580290C|2006-03-09|2017-10-24|Nicholas A. Tomory|A sonofusion device and method of operating the same|
    US20080008286A1|2006-05-09|2008-01-10|Jacobson Joseph M|Fusion energy production|
    ES2299348B1|2006-05-11|2009-02-01|Alset Technology Llc|CONTROLLED NUCLEAR FUSION PROCESS.|
    US9036765B2|2006-05-30|2015-05-19|Advanced Fusion Systems Llc|Method and system for inertial confinement fusion reactions|
    US20110170647A1|2006-09-27|2011-07-14|Emc2|Method and apparatus for controlling charged particles|
    US20080187086A1|2006-09-27|2008-08-07|Emc2|Method and apparatus for controlling charged particles|
    US7550741B2|2006-10-18|2009-06-23|Sanns Jr Frank|Inertial electrostatic confinement fusion|
    US7486758B1|2006-10-30|2009-02-03|The United States Of America As Represented By The Secretary Of The Air Force|Combined plasma source and liner implosion system|
    GB2444525B|2006-12-04|2011-10-05|Alan Charles Sturt|Method and apparatus for reducing the radioactivity of a particle|
    RU2337300C1|2007-02-07|2008-10-27|Пензенский государственный университет |Bursting tubular booster|
    US7501640B2|2007-02-24|2009-03-10|Larson Delbert J|Low energy electron cooling system and method for increasing the phase space intensity and overall intensity of low energy ion beams|
    US20080205573A1|2007-02-24|2008-08-28|Larson Delbert J|Cellular, Electron Cooled Storage Ring System and Method for Fusion Power Generation|
    US20110158369A1|2007-02-24|2011-06-30|Delbert John Larson|Cellular, electron cooled storage ring system and method for fusion power generation|
    CN101821813B|2007-10-04|2013-11-27|劳伦斯·利弗莫尔国家安全有限责任公司|Solid hollow core fuel for fusion-fission engine|
    JP2009094288A|2007-10-09|2009-04-30|Nec Electronics Corp|Semiconductor device|
    US8678763B2|2008-02-22|2014-03-25|Kaidou Ikeda|Circular ring, rotating duct, shroud, trunk and cylindrical external wall prepared by lamination of sheet belt, and apparatus and method for preparing the same|
    US7973296B2|2008-03-05|2011-07-05|Tetraheed Llc|Electromagnetic systems with double-resonant spiral coil components|
    US20100066252A1|2008-04-18|2010-03-18|The Regents Of The University Of California|Spiral rf-induction antenna based ion source for neutron generators|
    US20090290673A1|2008-05-20|2009-11-26|Vladimir Aleksandrovich Svidzinski|Method and device for realizing stable plasma confinement by pressure of AC magnetic field which can be used for controlled nuclear fusion|
    US20090310731A1|2008-06-13|2009-12-17|Burke Robert J|Single-pass, heavy ion fusion, systems and method|
    US9082517B2|2008-06-18|2015-07-14|Joel Guild Rogers|Modular apparatus for confining a plasma|
    EP2308273A4|2008-07-31|2015-07-22|Jiddtek Pty Ltd|Neutral particle generator|
    US20100046688A1|2008-08-25|2010-02-25|Kotschenreuther Michael T|Magnetic confinement device|
    NZ614346A|2008-08-28|2015-03-27|Advanced Fusion Systems Llc|Inertially compressing a fusion fuel pellet with temporally spaced x-ray pulses|
    US8279994B2|2008-10-10|2012-10-02|Board Of Regents, The University Of Texas System|Tokamak reactor for treating fertile material or waste nuclear by-products|
    US20110200153A1|2008-10-16|2011-08-18|Ferreira Jr Moacir L|Magnetic and electrostatic nuclear fusion reactor|
    KR100985611B1|2008-12-15|2010-10-05|한국원자력연구원|Blanket using lithum nanofluid and fusion reactor havning the same|
    US20100202580A1|2009-01-28|2010-08-12|Los Alamos National Security, Llc|Method and apparatus for neutron generation using liquid targets|
    WO2010089670A1|2009-02-04|2010-08-12|General Fusion, Inc.|Systems and methods for compressing plasma|
    PL2396792T3|2009-02-12|2016-06-30|Msnw Llc|Method and apparatus for the generation, heating and/or compression of plasmoids and/or recovery of energy therefrom|
    US9560734B2|2009-02-20|2017-01-31|Lawrence Livermore National Security, Llc|Dense plasma focus accelerated non radio isotopic radiological source|
    US20110075783A1|2009-04-30|2011-03-31|Mcgervey Donald L|Economical Method to Ignite a Nuclear Fusion Reaction and Generate Energy|
    US20110007860A1|2009-07-09|2011-01-13|Nathan Scott Sanders|Method and apparatus for reduction of neutron flux and or neutron containment, to facilitate nuclear-fusion|
    US20120014491A1|2009-07-13|2012-01-19|Mike Deeth|Nuclear fusion power plant having a liquid reactor core of molten glass that is made laseractive and functions as a tritium breeding blanket which is capable of acousticly compressing/confining fuel so that it radiates and triggers outgoing laser cascades that will reflect from the blast chamber's spherical inside wall and return like photonic Tsunamis, crushing, heating, and causing thermonuclear ignition of the fuel so that heat engines and piezoelectric harvesters can convert the released energy into electricity|
    US8837661B2|2009-07-24|2014-09-16|The Regents Of The University Of California|Radionuclide production using a Z-pinch neutron source|
    US8891719B2|2009-07-29|2014-11-18|General Fusion, Inc.|Systems and methods for plasma compression with recycling of projectiles|
    NZ598493A|2009-09-17|2013-10-25|Advanced Fusion Systems Llc|Advanced fusion fuel|
    WO2010114360A1|2009-09-24|2010-10-07|Bernard Jozef Reits|Apparatus for fusing nuclei of hydrogen isotopes|
    WO2011044495A1|2009-10-09|2011-04-14|Fpgeneration, Inc.|Systems and methods for magnetically assisted inertial electrostatic confinement fusion|
    US20110142185A1|2009-12-16|2011-06-16|Woodruff Scientific, Inc.|Device for compressing a compact toroidal plasma for use as a neutron source and fusion reactor|
    JP6097563B2|2010-01-08|2017-03-15|トライ アルファ エナジー， インコーポレイテッド|Energy conversion from high energy photons to electricity|
    US20110216866A1|2010-03-08|2011-09-08|Timothy Raymond Pearson|Method and apparatus for the production of nuclear fusion|
    US9025717B2|2010-03-18|2015-05-05|Brent Freeze|Method and apparatus for compressing plasma to a high energy state|
    US8436271B2|2010-04-14|2013-05-07|Baruch Boris Gutman|Thermal nucleus fusion torch method|
    US8576971B2|2010-04-23|2013-11-05|Lawrence Livermore National Security, Llc|Laser fusion neutron source employing compression with short pulse lasers|
    US20110261918A1|2010-04-26|2011-10-27|Schmidt Willard H|Neutron and multi-neutron generator|
    US20110274228A1|2010-05-04|2011-11-10|Lopez Jose E|Nuclear fusion using electrostatic cage and electro-magnetic field|
    US9287011B2|2010-05-17|2016-03-15|Innoven Energy Llc|High-yield ICF containment chambers and power reactors|
    DE102010023339A1|2010-06-10|2011-12-15|Siemens Aktiengesellschaft|Accelerator for two particle beams to create a collision|
    GB201009768D0|2010-06-11|2010-07-21|Tokamak Solutions Uk Ltd|Compact fusion reactor|
    AU2011274383B2|2010-07-01|2014-12-04|Advanced Fusion Systems Llc|Method of inducing chemical reactions|
    US20120008728A1|2010-07-09|2012-01-12|Ray R. Fleming|Resonant Vacuum Arc Discharge Apparatus for Nuclear Fusion|
    US20120033775A1|2010-08-09|2012-02-09|Highfuels, Inc.|Method and apparatus for intermediate controlled fusion processes|
    WO2012021537A1|2010-08-09|2012-02-16|Msnw Llc|Apparatus, systems and methods for establishing plasma and using plasma in a rotating magnetic field|
    US20120039431A1|2010-08-12|2012-02-16|Schmidt Willard H|Process for fused neutron nuclear chain reactions|
    US20120057665A1|2010-09-08|2012-03-08|Lawrence Livermore National Security, Llc|Three Wavelength Coupling for Fusion Capsule Hohlraums|
    WO2012037488A1|2010-09-16|2012-03-22|Intelligent Power Corp|Systems, apparatuses and methods for the implementaton of an energy system|
    US20120076253A1|2010-09-23|2012-03-29|Mr. & Mrs. Fred E. Howard, JR., Family Living Revocable Trust|Scalable high efficiency nuclear fusion energy source|
    US8466429B2|2010-10-06|2013-06-18|Lawrence Livermore National Security, Llc|Particle beam injector system and method|
    US20120086364A1|2010-10-06|2012-04-12|Lawrence Livermore National Security, Llc|Particle beam coupling system and method|
    WO2012064668A1|2010-11-08|2012-05-18|Lawrence Livermore National Security, Llc|Indirect drive targets for fusion power|
    JP2014508289A|2011-01-28|2014-04-03|ローレンスリバモアナショナルセキュリティー，エルエルシー|Adjustable fusion blanket for load following and tritium production|
    BR112013021793B1|2011-02-25|2020-02-27|General Fusion, Inc.|PRESSURE WAVE GENERATOR WITH MOBILE CONTROL ROD TO GENERATE A PRESSURE WAVE IN A MEDIUM|US20060198486A1|2005-03-04|2006-09-07|Laberge Michel G|Pressure wave generator and controller for generating a pressure wave in a fusion reactor|
    WO2010089670A1|2009-02-04|2010-08-12|General Fusion, Inc.|Systems and methods for compressing plasma|
    US8891719B2|2009-07-29|2014-11-18|General Fusion, Inc.|Systems and methods for plasma compression with recycling of projectiles|
    KR101663032B1|2010-09-10|2016-10-06|삼성전자주식회사|Process monitoring device and semiconductor process apparatus with the same, and process monitoring method|
    BR112013021793B1|2011-02-25|2020-02-27|General Fusion, Inc.|PRESSURE WAVE GENERATOR WITH MOBILE CONTROL ROD TO GENERATE A PRESSURE WAVE IN A MEDIUM|
    US10201070B2|2012-01-10|2019-02-05|Electron Power Systems, Inc.|Systems and methods for generating electron spiral toroids|
    KR101615063B1|2012-04-04|2016-04-22|제너럴 퓨전 아이엔씨.|Jet control devices and methods|
    US9596745B2|2012-08-29|2017-03-14|General Fusion Inc.|Apparatus for accelerating and compressing plasma|
    KR101235597B1|2012-11-28|2013-02-21|국방과학연구소|Accelerator using electromagnetic force|
    WO2014121401A1|2013-02-08|2014-08-14|General Fusion, Inc.|Pressure wave generator with a sabot launched piston|
    US9655221B2|2013-08-19|2017-05-16|Eagle Harbor Technologies, Inc.|High frequency, repetitive, compact toroid-generation for radiation production|
    CA2958399C|2014-08-19|2017-07-04|General Fusion Inc.|System and method for controlling plasma magnetic field|
    US9406405B2|2014-09-28|2016-08-02|Joel Guild Rogers|Fusion energy device with internal ion source|
    RU2590893C1|2014-12-18|2016-07-10|Открытое акционерное общество "Научно-исследовательский институт оптико-электронного приборостроения" |Method for producing impact-compressed plasma layer and device for its implementation|
    RU2670424C2|2016-03-21|2018-10-23|Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом"|Device for attachment of blanket module on vacuum housing of thermonuclear reactor|
    IT201600089129A1|2016-09-02|2018-03-02|Paolo Sangermano|FLUID COMPRESSED GENERATOR DEVICE|
    KR101819921B1|2016-10-10|2018-01-18|삼성전자주식회사|Valve shutter|
    RU2661345C1|2017-03-06|2018-07-16|АКЦИОНЕРНОЕ ОБЩЕСТВО "Научно-исследовательский институт оптико-электронного приборостроения" |Method for simulation of a shock-compressed layer in arc discharge conditions|
    US10798808B2|2017-05-01|2020-10-06|General Fusion Inc.|Methods and systems for forming a liquid liner of a cavity|
    EP3635748A4|2017-06-07|2021-03-10|University of Washington|Plasma confinement system and methods for use|
    US10811144B2|2017-11-06|2020-10-20|General Fusion Inc.|System and method for plasma generation and compression|
    JP2021518034A|2018-02-28|2021-07-29|ジェネラル フュージョン インコーポレイテッド|Systems and methods for generating plasma and sustaining the plasma magnetic field|
    法律状态:
    2019-01-15| B06F| Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]|
    2019-07-09| B06T| Formal requirements before examination [chapter 6.20 patent gazette]|
    2020-10-20| B09A| Decision: intention to grant [chapter 9.1 patent gazette]|
    2020-12-22| B16A| Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]|Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 22/12/2020, OBSERVADAS AS CONDICOES LEGAIS. |
    优先权:
    申请号 | 申请日 | 专利标题
    US22935509P| true| 2009-07-29|2009-07-29|
    US61/229,355|2009-07-29|
    PCT/US2010/043587|WO2011014577A1|2009-07-29|2010-07-28|Systems and methods for plasma compression with recycling of projectiles|
    [返回顶部]