• 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:
    Method and equipment for converting thermal energy to mechanical energy by means of a thermal power machine (1). A member of metal alloy contained in the thermal power machine is heated to a certain temperature, whereat its physical properties are changed. This physical change is used as the mechanical drive power of the thermal power machine. The metal allow member of the thermal power machine (1) is heated by means of heat which is transferred by means of one or several heat pumps (6) from an external medium (9) that contains heat. The heat pump is operated by means of part of the mechanical energy generated by the thermal power machine (1), and the rest of this mechanical energy is used for other purposes, for example for moving a vessel (8).
    公开号:SU1386039A3
    申请号:SU853856874
    申请日:1985-02-01
    公开日:1988-03-30
    发明作者:Т.Арвола Илка；Кайамаа Яакко
    申请人:Илка-Т.Арвола и Яакко Кайамаа (FI)；
    IPC主号:
    专利说明:

    WITH
    00 00
    about: about
    00
    ;about
     s
    fzg.V
    two parts installed with the possibility of contact with elements from two sides. Rotors 2 and 3 m. They are made in the form of crankshafts 20, which are located symmetrically next to each other, and the elements are connected to them by articulated arms attached to their ends. The element is heated by means of the heat of the environment transferred by means of one or several heat pumps 26, while the heat pump is driven by a part of the mechanical energy generated by the engine. Instead of the auxiliary engine start m. implemented by means of an auxiliary heater, running on electricity or fuel; the energy received may be used to move the vessel. The structures in the devices according to the invention are made light and in them can be. used materials such as nylon, fiberglass, etc. The operating temperature of the device may be 40 ° C. The engine may be. constructed so that it is most suitable for certain t-bary conditions. The invention provides the possibility of using the minimum difference t-p surfaces 8 and 9. In this case, the heat loss will be minimal in absolute value. It is also possible to use several motors connected in series in such a way that each engine operates at a lower phase transition temperature of the material of its elements relative to the previous engine. 2 sec. and 4 hp f-ly 11 ill. .
    one
    The invention relates to converting low-grade thermal energy into mechanical energy during thermal deformations of metal alloy elements with a thermomechanical memory of their shortened length when heated and can be used to obtain work due to thermal aHep of the environment.
    The aim of the invention is to increase the heating and cooling efficiency and reduce the resistance to movement of the metal alloy elements.
    FIG. 1 is a diagram of the operating cycle of the engine when implementing the proposed method; FIG. 2 is a schematic diagram of a heat engine for implementing the method using a known ring element of a metal alloy; FIG. 3 is a structural diagram of an apparatus for implementing a method using the proposed engine as a ship engine; in fig. 4 - a heat engine for the implementation of the proposed method with elements of a metal alloy in the form of arcuate spring yarns, alternately heated I
    in the tank with coolant, in axonometry; in fig. 5 - engine, cross section; in fig. 6 - a variant of the proposed engine, in perspective; in fig. 7 - nitinol wire used in the motor, cross section; in fig. 8 - engine, cross section; in fig. 9 - section
    A-A in FIG. eight; in fig. 10 - details of the connection of metal alloy elements with rotors; in fig. t1 is a cross-section of a solid of means for heating and cooling a metal alloy element in the form of a tape shown in FIG. 10, in an embodiment of each of these bodies of two movable parts.
    Warm engine (see figure 4-9)
    contains one, two or more elongated elements 1 made of a metal alloy, for example, nitinol, capable of changing their length at a certain temperature by a certain
    value relative to the original length and relatively easy to stretch at lower temperatures. Elements 1 are parallel to each other and are eccentrically pivotally connected at one end to the first rotor 2, and at the other end to the second
    rotor 3. Both rotors 2 and 3 are installed with the possibility of rotation around shaft 4 and 5, perpendicular to elements 1, during compression and stretching of elements 1 from a metal alloy. The engine also contains means for heating and cooling elements 1 in the form of solids 6 and 7, respectively, with heating and cooling surfaces 8 and 9. Bodies 6 and 7 are installed with the possibility of their alternate contact of surfaces 8 and 9 with elements 1 when moving the latter and rotors 2 and 3.
    The solids 6 and 7 of the heating and cooling means can each be made in the form of two parts 10, 11 and 12, 13, respectively (see FIG. 11 installed in contact with the elements 1 from two sides, with parts 10, 11 and 12, 13 of these bodies are made with the possibility of controlled movement to tight contact of their surfaces 8.9 with elements 1 and in the opposite direction. Parts 10, 11 and 12, 13 bodies 6 and 7 of the heating and cooling means are connected to the frame (not shown) by means of hinges 14. At the maximum approximation of parts 10, 11 and 12.13, bodies 6 or 7 between their opposite The heat exchange surfaces 8 or 9 have a gap, the width of which corresponds to the thickness of the nitinol element 1, made in the form of a strip (see Fig. 10. Bodies 6 and 7 are located along the entire length of the element 1. Inside parts 10, 11 and 12, 13 bodies 6 and 7 pass the channels for the supply of coolants, and parts 10, 11 and 12, 13 are spring-loaded to keep them at a distance from each other in all phases except phase and contact with element 1 (not shown In the embodiment shown in FIG. 10, the elements 1 are connected to the rotors 2 and 3 by means of 1 tons of 15 fixed to the ends and connecting rods 16 connected to each other by means of hinges 17, and rotors 2 and 3 by means of hinges 18. There are stops 19 on both sides of the tons 17, the distance between which is less than the diameter of the motion path of the rotors 2 and 3, to control the transfer
    Placement of parts 10, 11 and 12, 13



    respiratory bodies 6 and 7 means of heating and cooling. Element 1 is made in the form of a nitinol strip, the side is long
    15
    20
    five
    i- Q
    0
    five
    0
    five
    0
    the cross section of which is arranged vertically (in Fig. 10 one end of the strip of element 1 is shown).
    According to the embodiment shown in FIG. 6-8, the rotors 2 and 3 are made in the form of crankshafts 20 arranged symmetrically adjacent to each other, and each element 1 in the form of a flat section nitinol wire, hinged to the cranks 21 of the shafts located opposite each other 20. Solid The bodies 6 and 7 of the heating and cooling means are located between the knees and shafts 20 one below the other and face each other with metal heat exchange surfaces 8 and 9, the distance between which is equal to or less than the diameter of the movement path of the necks of the cranks of the shafts 21 20. Inside 6 and 7 are parallel channels 22 for supplying coolants (see Fig. 9), and grooves 23 are made on their surfaces 8 and 9 for the filament wires of elements 1. Surfaces 8 and 9 are preferably convex toward each other and the distance between them in the middle part is less than the diameter of the crankshaft 20. Between surfaces 8 and 9: there is an insulation layer 24 in which vertical slots (not shown) are made parallel to the grooves 23. It is preferable that the insulation layer 24 covers all sides of the body 7. The device is enclosed in steel This vacuum casing 25. The channels 22 of the bodies 6 and 7 are connected to a heat pump 26 for transferring heat from the body 7 of the cooling element 1 to either the environment or the body 6 of the heating means. The body 6 of the heating means may also be connected directly to an external heat source 27, for example, waste heat of cooling water discharged from the nuclear power plant (with a temperature of approximately 50 ° C).
    According to the embodiment shown in FIG. 10 and 11, several parallel elements 1 in the form of strips can also be used. In this case, each strip has its own bodies 6 and 7 of the means for heating and cooling. The supports 19 can be filled, for example, fork-shaped, thanks to which the load can be 15, the end of which can be
    51386039
    located between two vertical rods of the plug (not shown), securely retains its position.
    Alternatively, the stops 19 and the hinges 17 can be omitted. In this case, instead of stops 19, limit switches are used, which actuate the relays, closing parts 10, 11 or 12, 13 of body 6 or 7 (not shown). In this case, it is advisable to provide an elastic mount bodies 6 and. 7, for example, by means of compression springs mounted on the side of the hinges 14, whereby the bodies 6 and 7 can move together with the elements 1 while in the closed position.
    Parts 10, 11 and 12, 13 tel 6 and 7
    change as the driving force of the heat engine, and the deformed element 1 is returned to its original longitudinally compressed form. In process a, the temperature of element 1 is reduced to a level below the phase transition temperature, after which the described cycle is repeated.
    The heating of element 1 in process C-d is carried out by means of the heat of the environment transferred by means of one or several heat pumps 26, while the heat pump 15 26 is driven by a part of the mechanical energy generated by the engine.
    The proposed method can be pe10
    For example, in the heat engine, it can be installed with the possibility of a 20 gatele shown in FIG. 2, co-moving towards each other and vice versa so that their heat exchange surfaces 8, 9 always remain parallel. One of the parts or both parts 10, 11 and 12 13 25 of the bodies 6 and 7 can be made movable. The stroke of the parts 10, 11 and 12, 13 may be very small, sufficient only to release the element 1 from the clamp between parts 10, 11 and 12, 13 of the bodies 6 and 7.
    Elements 1 can also be made of round wire, while on the heat exchange por30
    The field contains two rotors 2 and 3 in the form of wheels, the axes of which are parallel and on which one or several annular nitinol elements 1 are mounted. The wheel of the rotor 3 of smaller diameter is placed in a tank 28 with a heated medium covered with heat insulation The tank 28 is heated by the heat pump 26. The heat pump 26 is connected by means of a suitable transmission (not shown) to the shaft 4 of the wheel of the large rotor 2 of the heat engine. In addition, an auxiliary engine can be connected to the heat pump 26, which can be either an internal combustion engine or an electric motor (not shown).
    The surfaces 8 and 9 of parts 10, 11 and 12, 13 of bodies 6 and 7 should be made recesses corresponding to the cross section of the wire of elements 1. For effective operation of the device it is also important that contact heat transfer surfaces 8 and 9 of bodies 6 and 7 be as smooth as possible. and evenly heated.
    The working cycle of the heat engine during the inspection of the proposed method is shown in FIG. 1 in coordinates, the elongation of the element 1 is the stress in it, respectively, along the axes X and Y. In the process, a S element 1 is deformed (stretched) at a temperature below the phase transition temperature of its material. In the process, the element 1 is heated to a certain phase transition temperature of its material, at which the property of a thermomechanical memory manifests and its physical properties change, in particular its elastic modulus increases. In the process g, this change is used as the driving force of the heat engine, and the deformed element 1 is returned to its original longitudinally compressed form. In process a, the temperature of element 1 is reduced to a level below the phase transition temperature, after which the described cycle is repeated.
    The heating of element 1 in process C-d is carried out by means of the heat of the environment transferred by means of one or several heat pumps 26, while the heat pump 26 is driven by a portion of the mechanical energy generated by the engine.
    The proposed method can be re
    For example, in a heat engine, shown in FIG. 2, 5
    0
    The field contains two rotors 2 and 3 in the form of wheels, the axes of which are parallel and on which one or several annular nitinol elements 1 are mounted. The wheel of the rotor 3 of smaller diameter is placed in a tank 28 with a heated medium covered with heat insulation The tank 28 is heated by the heat pump 26. The heat pump 26 is connected by means of a suitable transmission (not shown) to the shaft 4 of the wheel of the large rotor 2 of the heat engine. In addition, an auxiliary engine can be connected to the heat pump 26, which can be either an internal combustion engine or an electric motor (not shown).
    When starting the heat pump 26 by means of an auxiliary engine, the pump 26 transfers heat from the environment to the environment, is located in the reservoir 28. In the latter, heat is transferred from the medium to the rotor wheel 3 of the heat engine and to that part of the ring nitinol element 1, which covers the rotor wheel 3. When the temperature of the nitinol element 1 reaches the phase transition temperature of its material, for example 50 ° C, the ring element 1, as it straightens, starts to rotate the rotor wheel 3. The motion is transmitted rotor wheel 2, a shaft 4 5 that produce the PTO. A part of the power obtained on shaft 4 is used to drive the heat pump 26 (all power
    0
    five
    0
    fie is required for this purpose). The remaining power can be used for other purposes.
    Instead of the auxiliary engine, the start-up can be carried out by means of an auxiliary heater operating, for example, on electricity or fuel (not shown). In this case, the medium in the tank 28 is first heated to the phase transition temperature by means of an auxiliary heater, which can then be turned off,
    FIG. 3 shows the application of the mechanical energy obtained by the proposed motor 29 for moving the vessel 30. The heat engine 29 and the heat pump 26 are mounted on the vessel. Heat pump 26 transfers heat from environment 31 - water through a system 32 of pipelines to a water tank 28 connected to a heat engine 29, maintaining the temperature of water in it, for example about 50 ° C. Some of the energy generated by the heat engine 29, spend on the drive of the heat pump 26, and another part - on the drive of the screw 33 of the vessel 30. Thus, by means of a part of the mechanical energy created by the heat engine 29, the vessel 30 is moved, and as the environment 31, the heat of which is transferred to element 1 of a metal alloy, those that use the water surrounding the vessel 30.
    FIG. 4 and 5 show a variant of a heat engine 29 containing a reservoir 28 with a heated medium, a heat carrier, between the side walls of which is fixed by means of springs 34 several elements 1 in the form of arcuate nitinol bands. The strips of elements 1 are bent up and down alternately. A connecting rod 35 is attached to the middle part of each strip of element 1, the opposite end of which is rotatably attached to a crankshaft 20 with alternating oppositely directed crank elbows 21,
    When the temperature in the tank 28 reaches the phase transition temperature of the material of the nitinol strips of the elements 1, the downward curved bands of the elements 1 begin to reclaim, tend to take the shape given to them during the heat treatment, as a result
    Q
    , 2 25 5
    0
    five
    thirty
    0
    The rods 35 begin to rotate the crankshaft 20. The strips of elements 1, straightening out, move away from the medium in reservoir 28, and the heat energy of the hot source — medium 31 — is no longer transferred to them. When cooled down, they again become flexible, while the crank 35 forces them to curve upwards. During the strip of elements 1, which are initially bent upwards, they are forced to curve downward, as a result of which they come into contact with the medium in the reservoir 28. Then Again, some of the thermal energy of the medium is converted into kinetic energy.
    The transfer of heat to the nitinol bands of the elements 1 in the device shown in FIG. 4-5, can be generated either from the medium 31 as a liquid with a low surface tension, or from contact surfaces 8, 9, or as a pulse of any other thermal energy, for example, generated by electricity, heat radiation or a laser. The stiffness of the springs 34 can be selected from the condition of providing a resonance of their oscillations during rotation of the shaft 20.
    ; The structures in the devices are made light, they can be used, for example, materials such as nylon, fiberglass, etc. The operating temperature of the device may, for example, be 40 ° C. The motor may be designed to be most suitable for certain temperature conditions. The environment 31, from which energy is transferred by means of the heat pump 26, may be, for example, earth, water or air.
    The engine shown in fig.b-9, works in the implementation of the proposed method in the following way. When the heat exchange surface 8 is heated, the nitinol wires of the elements 1 in contact with it are heated to the phase transition temperature of their material. Reaching the phase transition temperature, the nitinol wires of the elements 1 are reduced and the crankshaft 21 of the crankshafts 20 with the elements 1 wires attached to them are in the lowest position, while the wires of the elements 1
    1 rise and begin to cool. At the same time, the nitinol wires of the elements 1 attached to the cranks 21 of the crankshafts 20, which are in the upper position, are cooled in contact with the surface 9 of the cooling means body 7, and as a result of the rotation of the crankshafts 20 in opposite directions they stretch. The movement continues and the wires of the elements 1, which in the initial position were in contact with the heating surface 8, come into contact with the cooling surface 9 and are effectively cooled.
    After starting the device, crankshafts 20 perform a continuous symmetrical rotation in opposite directions, with the nitinol wires of the elements 1 alternately reducing, coming into contact with the surface 8, then after cooling in contact with the surface 9 lengthening due to elongation by the crankshafts 20.
    The power outputs of the shafts 20 can be combined by means of a common load shaft (not shown). A part of the combined output power can be used to drive the heat pump 26, and the remaining useful power can be used for other purposes.
    With Heo6xoAiiMOCTH, the position of the crankshafts 20 can be adjusted by displacing them in the W and Z directions (Fig. 8). The device can operate in such a way that its lower surface 8 is cooling and the upper surface 9 - heating. In this case, the crankshafts 20 rotate in opposite directions. The device can be installed so that the wires of the elements 1 are not in the horizontal direction.
    FIG. 8 schematically shows that the liquid cooled in the evaporator of the heat pump 26 is first passed through the channels 22 (FIG. 9) of the cooling means body 7 supplied by the cooling surface 9, which is efficiently cooled. Jlimb thereafter, the fluid is passed through nycKajoT through the medium 31 used as the heat source, in which the temperature of the fluid rises
    to the level of medium temperature 31. After that, the liquid is sent back to the evaporator of the heat pump 26, where it gives off heat.
    The fluid passed through the body 6 of the heating means, provided with a heating surface 8, circulates through the heat pump capacitor, where it is heated, whereby the temperature of the heating surface 8 is kept sufficiently high.
    The device depicted in figure 10
    g and 11, in the implementation, the proposed method works as follows.
    When moving the nitinol band of element 1 from top to bottom together with
    0 a crankshaft of 20 tons gi 15 at its ends comes into contact with lower stops 19. A result of a relay (not shown) connected to stop 19 causes parts 10, 11 of the body 6 of the medium,
    5, the heat moves, overcoming the action of springs (not shown) towards each other and comes into close contact with the nitinol strip of element 1 on both sides. At the same time, the strip of element 1 quickly heats up to the phase transition temperature of its material and tends to shrink. The crankshafts of the crankshafts 20 are rotated in opposite directions until the thrust rod 15 starts moving away from the lower stop 19. At the same time, due to the joint 17 connecting the connecting rod 16 and the stud 15, the position of the nitinol strip of the element 1 does not change in the vertical direction, At the same time, when the pull rod 15 departs from the lower stop 19, the relay releases parts 10, 11 of body 6 and allows them to move apart, with the result that the strip of element 1 is able to rise.
    Upon further movement of the rod 15, it comes into contact with the upper stop 19, which causes the parts 12, 13 of the cooling means body 7 to come closer towards the strip of the element 1. At the same time, the cooling surfaces 9 come into contact with the strip of the element 1 and efficiently and quickly cool it. Then, the lane of the element 1 extended by the crankshaft 20 is elongated again, after which the described sequence of movements is repeated.
    0
    five
    0
    five
    0
    The invention provides the possibility of using the minimum temperature difference between surfaces 8 and 9. In this case, the heat loss is minimal in absolute value.
    It is also possible to use several heat engines 29 connected in series so that each engine 29 operates at a slightly lower temperature of the phase transition of the material of its elements 1 with respect to the previous engine 29. In this case, the temperature difference between adjacent temperature ranges can be very small. . You can also use only part of such a group of series-connected engines 29.
    权利要求:
    Claims (6)
    [1]
    1. A heat engine containing one, two or more elongated metal alloy elements arranged parallel to each other, capable of varying its length at a certain temperature by a certain amount relative to the original length and relatively easy to stretch at lower temperatures. The metal alloy elements are hinged and eccentric connected. one end with the first rotor, and the other end with the other rotor, both rotors mounted for rotation around the shafts of the perpendicular metal alloy elements to obtain rotation during compression of metal alloy elements and stretching the latter during subsequent rotation of the rotors
    as well as heating and cooling means installed with the possibility of their alternate contact with metal alloy elements when moving the latter and the rotors, from the fact that, in order to increase the heating and cooling efficiency and reduce the resistance to movement of the metal alloy elements, heating and cooling are made in the form of solid bodies, respectively, with heating and cooling surfaces.
    [2]
    2. The engine according to claim 1, about tl and - - due to the fact that the solids of the heating and cooling means are executed in two parts, mouth
    Yu
    0
    five
    0
    five
    0
    0
    five
    contact with elements from a metal alloy on both sides, and parts of these bodies are made with the possibility of controlled movement of one to another until intimate contact of their surfaces with elements of a metal alloy and in the opposite direction.
    [3]
    3. The engine for PP. 1 or 2, which is characterized by the fact that the rotors are made in the form of crankshafts arranged mutually symmetrical in a row, and each metal alloy element is connected to crankshafts cranks located opposite each other.
    [4]
    4. The engine of PP. 1-3, characterized in that the metal alloy elements are connected to the rotors by means of articulated joints attached to the ends of the elements, on both sides of the latter stops are installed, the distance between which is smaller than the diameter of the rotor movement path, heating and cooling.
    [5]
    5. A method of converting thermal energy into mechanical energy by means of a heat engine by heating.
    ; a metal-made element to a certain temperature at which its physical properties, in particular, the elastic modulus, change, and using this change as the driving force of the heat engine, is due to the fact that the metal alloy element was heated by means of one or more heat pumps of ambient heat, and the heat pump is driven by a portion of the mechanical energy generated by the engine.
    [6]
    6. The method according to claim 5, characterized in that by means of a part of the mechanical energy created by the engine, the vessel on which the engine is installed is moved, and water is used as an environment, the heat of which is transferred to the metal alloy element, surrounding the vessel.
    Priority points: 06/03/83 yr) nn. 5 and 6. 02.12.83 on PP. 1-4.
    3Z7
    , 28
    ABOUT
    FIG. 2
    26
    7
    Phie, 3
    26
    2f
    21
    Jj
     PUQ.
    FIG. five
    0i / e. 7
    i
    Phases, //
    类似技术:
    公开号 | 公开日 | 专利标题
    US4086769A|1978-05-02|Compound memory engine
    SU1386039A3|1988-03-30|Heat engine and method of converting heat energy into mechanical energy by means of heat engine
    US3971230A|1976-07-27|Stirling cycle engine and refrigeration systems
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    US4415171A|1983-11-15|Control system and shaft seal for Stirling cycle machine
    US4235075A|1980-11-25|Method and apparatus for converting relatively low temperature heat energy into useful work
    US4257231A|1981-03-24|Heat engine
    US4423596A|1984-01-03|Thermal engine
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    US5878571A|1999-03-09|Device for amplifying the output of a driven machine
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    US4503676A|1985-03-12|Apparatus for directly converting thermal to rotational energy
    US374123A|1887-11-29|hopkins
    WO2010097637A2|2010-09-02|Apparatus for the utilisation of thermal radiation
    SU1315649A1|1987-06-07|Heat martensite engine
    SU1268793A1|1986-11-07|Thermal engine
    FI75402C|1988-06-09|VAERMEKRAFTMASKIN FOER OEVERFOERING AV VAERMEENERGI TILL MEKANISK ENERGI.
    CA1261636A|1989-09-26|Method and equipment for converting thermal energy to mechanical energy
    RU2099595C1|1997-12-20|Heat engine | and thermoelement
    US20110247332A1|2011-10-13|External Combustion Engine
    SU1057706A1|1983-11-30|Heat engine
    同族专利:
    公开号 | 公开日
    DE3481075D1|1990-02-22|
    FI76405B|1988-06-30|
    FI834438A0|1983-12-02|
    EP0144406B1|1990-01-17|
    AU3015484A|1985-01-04|
    FI834438A|1984-12-04|
    US4800722A|1989-01-31|
    FI76405C|1988-10-10|
    US4756158A|1988-07-12|
    WO1984004947A1|1984-12-20|
    EP0144406A1|1985-06-19|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    DE1476719A1|1964-08-05|1969-03-27|Taylor John Edward|Thermal machine|
    US4175390A|1974-12-27|1979-11-27|George Koslow|Solid stress motor|
    US4086769A|1975-05-19|1978-05-02|The United States Of America As Represented By The Secretary Of The Navy|Compound memory engine|
    US4150544A|1976-10-14|1979-04-24|Pachter John J|Engine|
    US4117680A|1976-12-07|1978-10-03|Solergy, Inc.|Continuous loop shape memory effect heat engine|
    DE2756093A1|1977-12-16|1979-06-21|Dieter Knauer|Mechanical engine driven by heat pump - has hydraulic drive between thermal engine and mechanical output|
    US4275561A|1978-08-03|1981-06-30|Wang Frederick E|Energy conversion system|
    US4246754A|1979-03-12|1981-01-27|University Of Illinois Foundation|Solid state thermal engine|
    DE2933199A1|1979-08-16|1981-03-26|Bernd Dipl.-Ing. 8000 München Hahn|Engine converting heat into mechanical energy - has rotor with thermally sensitive strips to shift centre of gravity when heated|
    GB2072756B|1980-03-18|1984-08-15|Sharp Kk|Shape memory effect heat engine|
    FR2502253A1|1981-03-20|1982-09-24|Souteyrat Joseph|Heat powered rotary engine - has rotor with radial arms heated to displace weight and cause rotation of output shaft|
    US4397151A|1982-03-22|1983-08-09|Houlton Samuel S|Heat engine|
    SU1134778A1|1983-04-07|1985-01-15|Trotsenko Ivan V|Heat engine|RU2213256C2|2002-11-21|2003-09-27|Умаров Георгий Рамазанович|Method of conversion of thermal energy into useful work|
    US8857174B2|2009-11-20|2014-10-14|GM Global Technology Operations LLC|Vehicle energy harvesting device having discrete sections of shape memory alloy|
    US8299637B2|2009-12-16|2012-10-30|GM Global Technology Operations LLC|Shape-memory alloy-driven power plant and method|
    US8938965B1|2011-05-27|2015-01-27|The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration|Thermal powered reciprocating-force motor|
    CN110529348B|2019-09-27|2021-11-26|大连大学|Heat engine device for realizing heat energy-mechanical energy conversion by utilizing shape memory alloy|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    FI832016A|FI832016A0|1983-06-03|1983-06-03|OVER ANCHORING OF OIL CHARGING AV MECHANICAL ENERGY|
    FI834438A|FI76405C|1983-06-03|1983-12-02|FOERFARANDE FOER OMVANDLING AV VAERME-ENERGI TILL MEKANISK ENERGI.|
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