• 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:
    An air pressure regulator (16) having a regulator body (40) defining a hollow interior, an air inlet (50) communicating with the hollow interior and adapted to connect to a source of pressurized air, an air outlet (52) in fluid communication with the air inlet (50), and a valve stem (54) located in the air inlet (50) and adapted to regulate the pressure of the air pressurized air for the air outlet (52) due to movement (60) of the valve stem (54) relative to the air inlet (50).
    公开号:FR3040084A1
    申请号:FR1657279
    申请日:2016-07-28
    公开日:2017-02-17
    发明作者:Jerry Dean Hielkema
    申请人:GE Aviation Systems LLC；
    IPC主号:
    专利说明:

    Air pressure regulator
    An air pressure regulator is a type of valve or air restrictor for a pneumatic pressure system, which regulates the flow of a gas at a certain pressure. For example, an air pressure regulator can be used to allow a high pressure gas supply to be reduced to provide lower pressure for later use in various pneumatic pressure system applications. The air pressure regulator can adjust the gas flow rate at the regulator output depending on the gas demand on the pressure system, the gas supply in the regulator, or a combination of both.
    Turbine-powered aircraft may be designed to produce compressed or pressurized air in the compressor section of the engines that can be used to supply pressurized air to various aircraft air pressure systems. The pressurized air, or "bleed air", may also be adjusted by the air pressure regulators described above and be supplied to aircraft pneumatic pressure systems, of which, in no way limiting, means for regulating air supply and cabin pressure, cooling various aircraft or engine components, anti-icing systems, pneumatic cylinders or motors, or waste and water storage systems.
    According to a first aspect, an air pressure regulator comprises a regulator body defining a hollow interior, an air inlet communicating with the hollow interior and adapted to connect to a source of pressurized air, an outlet of air in fluid communication with the air inlet, a valve stem placed in the air inlet and adapted to regulate the pressure of the air under pressure for the air outlet under the effect of the movement of air. the valve stem relative to the air inlet, a retaining member disposed in the hollow interior and assembled with the valve stem so that the valve stem and the retaining member move in concert, the retainer member comprising an electrically conductive sleeve, and a magnet having a magnetic field, mounted on the regulator body, the magnetic field including at least a conductive sleeve portion. The movement of the conductive sleeve with respect to the magnetic field is delayed by eddy currents generated in the conductive sleeve by the movement.
    In another aspect, a pneumatic pressurizing element comprises a housing defining a hollow interior, a retaining element disposed in the hollow interior, having an electrically conductive sleeve, and assembled with a valve stem placed in an air inlet. air and designed to regulate the pressure of air under pressure for an air outlet due to movement of the valve stem relative to the air inlet, the valve stem and the retainer moving together, and a magnet having a magnetic field, mounted in the housing, the magnetic field including at least a portion of the conductive sleeve. The movement of the conductive sleeve with respect to the magnetic field is delayed by eddy currents generated in the conductive sleeve by the movement.
    In yet another aspect, an air pressure regulator includes a limiting member adapted to provide a variable limitation for controlling the pressure of air under pressure at an air inlet for an air outlet, under the effect of the movement of the retaining member with respect to the air inlet, a retaining element assembled with the retaining element and having an electrically conductive sleeve, the limiting member and the retaining element moving concert, and a fixed magnet fixed close to the conductive sleeve and having a magnetic field, the magnetic field including at least a portion of the conductive sleeve, and the conductive sleeve being movable relative to the magnet. The movement of the conductive sleeve with respect to the magnetic field is delayed by eddy currents generated in the conductive sleeve by the movement. The invention will be better understood from the detailed study of some embodiments taken as non-limiting examples and illustrated by the appended drawings in which: FIG. 1 is a schematic top-down view of the architecture of the aircraft and aircraft electronics data network; FIG. 2 is a schematic view of a pressure regulation system; and FIG. 3 is a sectional view of an air pressure regulator.
    Embodiments of the invention described herein relate to an air pressure regulator used in a pneumatic pressure system of an aircraft, but the device described herein can be implemented in any environment using a pressure regulator. air or a pressurizing element of an air pressure regulator for regulating an air pressure from a first pressure at an inlet to a second pressure at an outlet.
    As illustrated in FIG. 1, an aircraft 10 may comprise at least one propulsion engine, represented in the form of a left engine system 12 and a right engine system 14, such as gas turbine engines. The left and right engine systems 12, 14 are shown as schematically including a compressor section 24 designed to produce compressed or pressurized air for combustion in the respective engines 12, 14. The compressor section 24 may further comprise, or be designed to produce "supply air", which is pressurized air not being used for combustion in the respective engines 12, 14, but instead is supplied by the compressor section 24 to send air the air under pressure to various pneumatic pressure systems of the aircraft 10. The aircraft 10 may further comprise a series of pneumatic systems, including, by way of no limitation, means 18 for regulating the supply of air and cabin pressure or pneumatic cylinders or motors 20. Additional pneumatic systems may include, for example, the cooling of various components of the aircraft 10 or engines 12, 14, the anti-icing systems, hydraulic tarpaulins or waste and water storage systems. The pressure regulating means 18 and the pneumatic motors 20 may be in fluid communication with the withdrawal air supplied by the compressor sections 24 via one or more air pressure regulators 16 and a series of pneumatic coupling means such as the pipe 22. The pressure regulators 16 may be designed to regulate a supply air pressure to obtain a predetermined outlet air pressure. The illustrated aircraft 10 is an exemplary embodiment of an aircraft configuration 10 with respect to pneumatic systems. Although the air supply and pressure regulating means 18 are shown near the nose of the aircraft 10 and the pneumatic motors 20 are shown arranged around the periphery of the aircraft 10 and wings, the locations indicated There are no embodiments of the invention and there are contemplated embodiments in which any positioning or location of the pressure regulating means 18 or the respective pneumatic motors 20 is possible. Furthermore, the illustrated embodiment of the aircraft 10 is only a non-limiting example of an aircraft 10 usable in embodiments of the invention described herein. Unless stated otherwise, the features of the illustrated embodiment of the aircraft 10, including relative span, length, number of engines, type of engines and location of various members, do not fall within the scope of the invention. embodiment of the invention.
    Figure 2 schematically illustrates an exemplary operation of a pneumatic pressure system 26 of Figure 1. As shown, a pressure source such as the compressor section 24 of the left and right engine systems 12, 14 generates or produces bleeding air 28 under pressure. The bleed air 28 can be regulated by a set of air pressure regulators 16 to regulate the supply air pressure to obtain outlet air 30 at a predetermined pressure, for example for pneumatic systems 18, 20 of the aircraft 10. The compressor section 24, the set of air pressure regulators 16 and the pneumatic systems 18, 20 are all connected to one another by the pneumatic line 22. Ordinarily, Air pressure regulators 16 are adapted to progressively lower or reduce the supply air supply pressure 28 to obtain a lower pressure of the outlet air 30. Embodiments of the invention are contemplated. wherein an air pressure regulator 16 is designed or adapted with one or more pneumatic systems 18, 20 so that the regulator 16 regulates the pressurized outlet air 30 to a predetermined designed air pressure or For example, the pneumatic systems 18, 20 designed to operate at a common air pressure can be designed to receive the outlet air 30 of a pump. Only one air pressure regulator 16. Alternatively, each pneumatic system 18, 20 may use individual air pressure regulators 16, for example to improve reliability or reduce disturbances in the event of a system failure. In yet another example, a set of cascaded air pressure regulators 16 may gradually lower the supply air pressure 28 as required by the pneumatic systems 18, 20.
    Figure 3 shows a sectional view of an air pressure regulator 16 according to embodiments of the invention. The air pressure regulator 16 comprises a regulator body 40 comprising a first housing 42 and a second housing 44 assembled with each other. The first housing 42 and the second housing 44 may be assembled using known mechanical or fastening means, in particular by means of screws, bolts, glues or the like. The first housing 42 defines a first hollow interior 46 and the second housing defines a second hollow interior 48, the first and second interior 46, 48 not allowing fluid communication between them because they are isolated from each other by least part of a pressure regulating device such as a flexible membrane 49. The flexible membrane 49 may be designed, molded, shaped or otherwise to produce an effect while being stressed or at rest, the membrane 49 being able to generate a reaction or opposition force when it is caused to bend, such that the bias serves to return the membrane 49 to a state or position without bending. The air pressure regulator 16 may be mounted on a manifold under pressure using a number of methods or mounting mechanisms including, by no means limitation, bolts. The methods or mechanisms for mounting the air pressure regulator 16 do not relate to embodiments of the invention.
    The first housing 42 further includes an air inlet 50 adapted to connect to a source of pressurized air and to receive a supply of pressurized supply air. The first housing 42 may also include an air outlet 52 adapted to provide regulated pressurized air, for example to the pneumatic conduit 22 or to a pneumatic system 18, 20. The first housing 42 further comprises a rod 54 valve member positioned in, or slidably received by the first housing 42 in the air inlet 50, the valve stem 54 comprising a valve stem head 56. The valve stem 54 may be supported by a sliding element 58 which, by way of no limitation, a bearing, designed to allow the rod 54 to move back and forth or to be movable in the regulator body 40 (represented by arrows 60). The first housing 42 is further adapted to include, around the valve stem 54, a first channel 62 in fluid communication with, or creating fluid communication between the air inlet 50 and the air outlet 52, and a second channel 64 in fluid communication with or creating fluid communication between the first channel and a pressure chamber 66. The pressure chamber 66 may be defined, for example, by the first interior 46 of the first housing 42 and the membrane 49. In this sense, the pressure chamber 66 is closed so that pressurized air can be supplied only through the air inlet 50 and released only through the air outlet 52. The diaphragm 49 can in addition, be connected to a second end 68 of the valve stem 54 distal to the valve stem head 56. In this sense, the flexible membrane 49 separating the first interior 46 from the second interior 48 may be designed to allow the sliding movement 60 of the valve stem 54 in the first housing 42 while still preventing fluid communication between the first interior 46 and second interior 48.
    The valve stem head 56 is of a size, shape, and configuration for its interaction with the air inlet 50 so that when the valve stem 54 or the valve stem head 56 is fully received in the first housing 42, the valve stem head 56 retains, limits or prevents the supplied air from being received in the air inlet 50. A non-limiting example of a valve stem head 56 may include a poppet valve. For example, as illustrated, the valve stem head 56 may have dimensions such that the head 56 is larger than the opening of the air inlet 50. In this sense, the valve stem head 56 is designed to modify, change or regulate the amount of pressurized air received in the air inlet 50 due to the movement 60 of the valve stem 54 and the valve stem head 56 relative to the inlet of the valve. In this sense, the valve stem head 56 is a limiting member designed to provide variable limitation of the air or pressure of the air received by the air inlet 50. Although the view of Figure 3 does not show the cross section of the valve stem head 56 or the air inlet 50, it is contemplated embodiments of the invention in which the respective shapes of the head 56 and the air inlet 50 are nested, adapted or complementary to one another to provide the restraint, restraint or preventing the receipt of air intake into the air inlet 50 when the head 56 is fully received.
    The regulation of the delivery, at the air outlet 52, of pressurized air received by the air inlet 40 is effected as explained herein. If the valve stem head 56 does not completely limit the receipt of pressurized air at the air inlet 50, a portion of the pressurized air is discharged to the air outlet 52 via the first channel 62. At the same time, another part of the pressurized air received at the air inlet 50 is discharged to the pressure chamber 66 via the first channel 62 and the second channel 64. As explained more high, the pressure chamber 66 is closed so that the pressure in the pressure chamber 66 can be received or released respectively by the air inlet 50 and the air outlet 52. As the pressure of the pressurized air received at the air inlet 50 accumulates in the pressure chamber 55, the flexible membrane 49 bends, which causes an increase in the volume of the chamber 66. The enlargement of the pressure chamber 66 causes in turn a movement 60 of the valve stem 54 and the valve stem head 56 relative to the inlet of the valve stem. As previously explained, the movement of the valve stem head 56 relative to the air inlet 50 limits, inhibits or prevents the receipt of more pressurized air at the air inlet. 50. The air inlet 50 being more or less closed and thus not allowing the previous quantity of pressurized air to pass, the pressure in the pressure chamber 66 decreases as the pressure is released via the outlet of Air 52. The pressure reduction in the pressure chamber 66 in turn causes the flexible membrane 49 and the movement 60 of the valve stem 54 and the resulting valve stem head 56 to move back relative to the inlet. air 50 allows the air inlet 50 to receive more or more air under pressure.
    Thus, the configuration of the air pressure regulator 16 allows the regulation of the pressurized air received at the air inlet 50 in order to obtain pressurized air discharged to the air outlet 52. The membrane 49, the pressure chamber 66, the valve stem 54, the valve stem head 56 and the air inlet 50 can thus be designed and adjusted to allow air at a predetermined pressure to be discharged to the air outlet 52 when it is supplied with pressurized air at an air pressure greater than or equal to the predetermined pressure of the discharged air. When the pressure of the pressurized air supplied to the air inlet 50 has acquired a reliable stability, i.e. the pressure of the air received at the air inlet 50 does not vary , the air pressure regulator 16 can balance, or find a balance between the pressure in the pressure chamber 66, the movement 60 of the valve stem 54 or the valve stem head 56, and therefore the pressure of the air discharged to the outlet 52 of air. When the pressure of the pressurized air supplied to the air inlet 50 is unreliable, or varies with time, the air pressure regulator 16 can react and adjust the amount of pressurized air received at the air inlet 50 and discharged to the air outlet 52, under the effect of the movement 60 of the valve stem 54 or the valve stem head 56, as explained above.
    The second housing 44 may comprise a retaining element 70 or biasing element slidably assembled with the valve stem 54, opposite the first interior 46, the pressure chamber 66 or the membrane 49. In the present description, a "retaining element" 70 or "biasing element" may be any element or set of elements designed to induce or adjust for a predetermined force, pressure or "stress" exerted on the solicitation. The retainer 70 is fixedly mounted on the valve stem 54 so that the retainer 70 accompanies the movement of the valve stem 54. The retainer 70 may be shaped, molded, machined or otherwise from an electrically conductive material such as copper and may include an electrically insulating sleeve 72 surrounding a hollow center 74. As shown, the conductive sleeve 72 and the hollow center 74 are disposed away from the assembly with the valve stem 54, extending axially into the second interior 48 of the second housing 44. Embodiments of the retainer 70 may for example, be mechanically assembled with the valve stem 54, in particular by means of a bolt 76 or a screw. Although a mechanical bolt 76 is shown, any mechanical joining mechanisms, glues or the like can be used to assemble the retainer 70 with the valve stem 54, and the particular assembly mechanism does not no embodiments of the invention. In addition, although the conductive sleeve 72 is described as surrounding the hollow center 74, other possible configurations of cross-sectional shape of the conductive sleeve 72 are contemplated, in which the sleeve 72 includes the center 74. Examples of other cross-sectional shapes may include, by no means limitation, a square, triangular, trapezoidal, hexagonal, etc.
    The second housing 44 may further comprise a fixed magnet 78, fixedly supported by a rear wall 80 of the second housing 44, and whose dimensions allow it to be received in the hollow center 74 of the conductive sleeve 72. magnet 78 may comprise, for example, a permanent magnet or electromagnet and is designed such that magnet 78 has axial magnetization. The magnet 78 and the conductive sleeve 72 are arranged close to each other or to each other so that a first magnetic field path (represented by a magnetic flux 81 in the form of mixed line) generated by the magnet 78 interact with or encompasses at least a portion of the conductive sleeve 72. The magnet 78 or rear wall 80 of the second housing 44 may further include adjusting means 82, such as a screwing interface 84, designed to adjust the position of the magnet 78 relative to the conductive sleeve 72. The adjusting means 82 may, for example, be used to move the magnet 78 in or out respectively into the second inside 48 or in the hollow center 74 of the conductive sleeve 72, in order to adjust the extent of the interaction of the first conductive field or the wrapping by the sleeve 72. Although a screwing interface 84 is shown, other possible mechanisms or setting means may be included.
    The second housing 44 may further include a mechanical retainer such as a mechanical spring 86 located in the second interior 48 between the rear wall 80 and a portion of the retainer 70. The spring 86 may be designed to repel the retaining element 70 away from the rear wall 80 by a mechanical force of a predetermined magnitude. The spring 86 and the membrane 49 (under the effect of the passive bias) may be individually or collectively designed or selected to allow or generate a counterforce to counterbalance, thwart or delay the enlargement of the pressure chamber 66. sense, as air at a higher pressure is received at the air inlet 50 and accumulates pressure in the pressure chamber 66, the spring 86 or the membrane 49 can be chosen to oppose the enlarging the pressure chamber 66 so that the air pressure supplied to the air outlet 52 is regulated to the desired or predetermined outlet air pressure by the movement of the rod 60 54 of the valve and the valve stem head 56. By way of nonlimiting example, the regulator 16 may, during the flight, be subjected to strong external vibrations which may cause an accidental, unexpected or otherwise undesirable movement 60 of the valve stem 54, of the stem head 56 valve, the air inlet 50, the air outlet 52, the first housing 42, the second housing 44 or the membrane 49, producing strong or small temporary variations in the pressure of the supplied air at the air outlet 52. In addition, members possibly connected to the air pressure regulator 16, such as the pipe 22, or structural supports, can also contribute to transmitting vibrations to the regulator 16. In addition, in any embodiment of the air pressure regulator 16 according to the present invention, pulses or variations of the air pressure received at the air inlet 50 can also cause or generate temporary variations in the air pressure regulator 16. crazy air pressure At the air outlet 52, variations in the air pressure supplied to the air outlet 52 may have other subsequent undesirable effects on the pneumatic systems. For example, if the air pressure supplied to the air outlet 52 serves as the reference pressure, a variation of this supplied air pressure can result in instability of a system.
    The conductive sleeve 72 and the magnet 78 may, for example, be configured to further reduce temporary variations in the air pressure supplied to the air outlet 52. air due, in no way limiting, to vibrations and the pressure of the air received at the air inlet 50, the movement 60 of the valve stem 54, of the valve stem head 56 or the membrane 59 can be counteracted, counterbalanced or delayed by the movement of the conductive sleeve 72 relative to the magnet 78 or the first magnetic field. In this sense, the movement of the conductive sleeve 72 around the magnet 78 and the first magnetic field modifies the magnetic flux experienced by the sleeve 72 (eg the intensity of the first magnetic field passing through the sleeve 72) and induces an electric current in the conductive sleeve 72. In turn, the induction of electric current in the conductive sleeve 72 generates in the conductive sleeve 72 eddy currents proportional to the intensity of the first magnetic field, on the surface of the loop of current and the rate of change of the magnetic flux. Thus, the eddy currents are proportional to the magnitude of the movement 60 of the conductive sleeve 72 relative to the magnet 78 or the first magnetic field, and also proportional to the speed of said movement 60.
    The eddy current generated in the conductive sleeve 72 produces a second magnetic field opposite to the first magnetic field produced by the magnet 78. In this sense, the movement 60 of the conductive sleeve 72 relative to the magnet 78 and the first magnetic field produces a second opposing magnetic field that upsets, counterbalances, delays, limits, or attenuates motion 60 itself. In addition, since the second magnetic field is proportional to the magnitude of the movement 60 and the speed of said movement 60, the attenuation of the movement 60 parallel to the movement 60.
    Thus, exemplary embodiments of the invention may be collectively configured to cooperate with the retaining element 70 or biasing element, the spring 86 and the membrane 49, or independently of the aforementioned members 70, 86, 49, to allow or to produce an opposing force for the purpose of counteracting, counteracting or delaying pressure variations of the supplied air at the air outlet 52, as explained above. The counterforce exerted by the retaining member 70 provides variable restraint for regulating the air pressure supplied to the air outlet 52, under the action of the valve stem 54 and the shank head 56. valve.
    One could also consider, for example, the use of an electromagnet instead of the magnet 78. In this example, the electromagnet can be selectively supplied with electricity by a source of electricity. to produce a magnetic field with respect to the conductive sleeve 72 to counteract, upset, attenuate, or delay movement 60 of the retainer 70, valve stem 54, or valve stem head 56, as explained herein . The selective power supply of the electromagnet may further be controlled in response, for example, to movement 60 of the conductive sleeve 72. For example, a sensor such as a position detector, a pressure sensor, an accelerometer or a pressure sensor disposed on the passage of the fluid in the air inlet 50 or the air outlet 52 can detect, measure or provide an indication of when or where, or is likely to occur, a variation of the air pressure supplied to the air outlet 52. The source of electricity can supply electricity to the electromagnet and therefore adjusts the magnetic field to counterbalance the pressure variation of the supplied air. at the air outlet 52 in response to the indication provided by the sensor. This configuration can give magnetic fields more intense than those a permanent magnet could produce alone.
    In another embodiment, at least a portion of the regulator body 40, first housing 42, or second housing 44 may include a thermally conductive cooling circuit thermally coupled to the retaining element 70 or the conductive sleeve 72. this embodiment of the invention, the heat generated in the conductive sleeve 72 under the effect of induced eddy currents can be dissipated through the cooling circuit. In still another embodiment of the invention, the air pressure regulator 16 may be designed such that the magnet 78, the magnetic field and the conductive sleeve 72 can counteract, counteract, attenuate or retard the movement. 60 of the valve stem 54 and the valve stem head 56, without additional mechanical retainers such as the spring 86. In addition, the design and arrangement of the various members can be reworked so that a number different online configurations can be realized.
    As illustrated, an air pressure regulator 16 in which the movement 60 of the conductive sleeve 72 with respect to the magnetic field is delayed by eddy currents generated in the conductive sleeve 72 by the movement 60. This has the technical effect to allow the attenuation of an accidental movement 60 in the air pressure regulator 16 due to pressure fluctuations or vibrations of the regulator 16. A considerable advantage is that it is possible to have a monobloc and self-regulating configuration for regulating a received air pressure and obtaining a regulated supply air pressure, the restraining member reducing or reducing vibration during movement or pressure change experienced by the air pressure regulator. Another advantage may include the absence of additional energy requirements or needs to improve the regulation of air pressure when a permanent magnet is used. Alternatively, in the example where an electromagnet is used, a stronger magnetic field can be used to better mitigate or counteract the variations experienced by the air pressure regulator.
    List of marks 10 Aircraft 12 Left engine system 14 Right engine system 16 Air pressure regulator 18 Air supply and cabin pressure control means 20 Air motor 22 Line 24 Compressor section 26 Pneumatic pressure system 28 Outlet air 30 Outlet air 40 Regulator body 42 First case 44 Second case 46 First inside 48 Second inside 49 Diaphragm 50 Air inlet 52 Air outlet 54 Valve stem 56 Valve stem head 58 Sliding element 60 Movement Valve stem 62 First channel 64 Second channel 66 Pressure chamber 68 Second end 70 Retaining element 72 Conductive sleeve 74 Center 76 Bolt 78 Magnet 80 Rear wall 81 Magnetic flux 82 Adjustment means 84 Screw interface 86 Spring
    权利要求:
    Claims (5)
    [1" id="c-fr-0001]
    An air pressure regulator (16) comprising: a regulator body (40) defining a hollow interior; an air inlet (50) communicating with the hollow interior and adapted to connect to a source of air under pressure ; an air outlet (52) in fluid communication with the air inlet (50); a valve stem (54) disposed in the air inlet (50) and adapted to regulate the pressure of the pressurized air for the air outlet (52) as a result of the movement (60) of the valve stem (54) with respect to the air inlet (50); a retainer (70) disposed in the hollow interior and assembled with the valve stem (54) so that the valve stem (54) and the retainer (70) move in concert, the retainer (70) including an electrically conductive sleeve (72); and a magnet (78) having a magnetic field, mounted on the regulator body (40), the magnetic field including at least one conductive sleeve portion (72); the movement of the conductive sleeve (72) with respect to the magnetic field is delayed by eddy currents generated in the conductive sleeve (72) by the movement (60).
    [2" id="c-fr-0002]
    An air pressure regulator (16) according to claim 1, wherein the retaining element (70) comprises a mechanical retaining element.
    [3" id="c-fr-0003]
    An air pressure regulator (16) according to claim 1, wherein the magnet (78) is a permanent magnet and / or an electromagnet.
    [4" id="c-fr-0004]
    An air pressure regulator (16) according to claim 3, wherein the magnet (78) is fixed relative to the regulator body (40) and includes adjusting means (82) adapted to adjust the position of the the magnet (78) relative to the conductive sleeve (72).
    [5" id="c-fr-0005]
    An air pressure regulator (16) comprising: a limiting member adapted to provide a variable throttle for regulating the pressure of air under pressure in an air inlet (50) for an air outlet (52); ), under the effect of the movement (60) of the restricting element with respect to the air inlet (50), a retaining element (70) assembled with the limiting element and having an electrically conductive sleeve conductor (72), the limiting member and the conductive sleeve (72) moving in concert; and a stationary magnet (78) fixed close to the conductive sleeve (72) and having a magnetic field, the magnetic field including at least a portion of the conductive sleeve (72), and the conductive sleeve (72) being movable relative to the magnet (78); the movement (60) of the conductive sleeve (72) with respect to the magnetic field being delayed by eddy currents generated in the conductive sleeve (72) by the movement (60).
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    同族专利:
    公开号 | 公开日
    BR102016018413A2|2017-02-14|
    US10125880B2|2018-11-13|
    CA2938203A1|2017-02-11|
    CN106438055B|2019-01-15|
    GB2541545B|2020-03-04|
    CA2938203C|2019-09-24|
    GB2541545A|2017-02-22|
    CN106438055A|2017-02-22|
    JP2017037643A|2017-02-16|
    FR3040084B1|2020-01-17|
    JP6401754B2|2018-10-10|
    US20170045149A1|2017-02-16|
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    DE102011108179B4|2011-07-22|2013-09-19|Festo Ag & Co. Kg|valve module|US10598183B2|2016-11-29|2020-03-24|United Technologies Corporation|Aeromechanical identification systems and methods|
    CN107143305B|2017-06-28|2019-12-03|西南石油大学|A kind of shaft bottom self-operated flow regulator|
    DE202017104079U1|2017-07-07|2017-08-21|Samson Ag|Actuator for process valves|
    CN108035807A|2017-11-09|2018-05-15|中国航空工业集团公司金城南京机电液压工程研究中心|A kind of pressure regulation integrating device for air starter|
    CN112178256A|2020-09-29|2021-01-05|中国航发动力股份有限公司|Large-size stable-speed anti-surge air release valve|
    法律状态:
    2017-07-26| PLFP| Fee payment|Year of fee payment: 2 |
    2018-06-21| PLFP| Fee payment|Year of fee payment: 3 |
    2019-06-21| PLFP| Fee payment|Year of fee payment: 4 |
    2020-06-23| PLFP| Fee payment|Year of fee payment: 5 |
    2021-06-23| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    US14/823,345|US10125880B2|2015-08-11|2015-08-11|Air pressure regulator|
    US14823345|2015-08-11|
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