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Actuation system for use on a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/075
출원번호 US-0252687 (1981-04-09)
발명자 / 주소
  • Nash Dudley O. (Cincinnati OH) Clayton Thomas S. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 37  인용 특허 : 3

초록

An actuation system is provided for transferring axial motion into an interior of a gas turbine engine at a number of locations around an outer casing of the engine, with one synchronous movement. An external hydraulic actuator activates the system by rotating one outer crank which, in turn, rotates

대표청구항

An actuation system for axially actuating an annular translating member internally mounted within a cylindrical outer casing of a gas turbine engine through which airflow passes, wherein said actuation system comprises: a plurality of circumferentially spaced crankshafts extending through said casin

이 특허에 인용된 특허 (3)

  1. Nash Dudley O. (Forest Park OH), Apparatus and method for controlling fan duct flow in a gas turbine engine.
  2. Young John Herman (South Windsor CT) Salisbury Charles Edward (Glastonbury CT), High ratio actuation linkage.
  3. Wagenknecht Conrad D. (West Chester OH) Faust Guy K. (West Chester OH), Individual bypass injector valves for a double bypass variable cycle turbofan engine.

이 특허를 인용한 특허 (37)

  1. Zsurka, Mark, Aerodynamic track fairing for a gas turbine engine fan nacelle.
  2. Craig Alfred C.,GB2, Aircraft engines with a controllable outer casing.
  3. Makowski, Maciej D.; Vasquez, David A., Articulated diffuser and door for submerged ram air turbine power and cooling control.
  4. Koshoffer,John Michael, Augmenter swirler pilot.
  5. Cadieux, Michel, Bleed off valve system.
  6. Eleftheriou, Andreas; Ivakitch, Richard; Denis, David, Bleed valve.
  7. Smith, J. Walter, Controlled fan stream flow bypass.
  8. Regunath,Shane, Controlling a plurality of devices.
  9. Schwarz, Frederick M., Cooling exchanger duct.
  10. Schwarz, Frederick M., Cooling exchanger duct.
  11. Schwarz, Frederick M.; Glahn, Jorn A., Cooling exchanger ducts.
  12. Beutin Bruno Albert,FRX ; Brossier Pascal Noel,FRX ; Franchet Michel Fran.cedilla.ois Raymond,FRX ; Lecordix Jean-Loic Herve,FRX ; Loubet Marc Georges,FRX, Cooling system for a turbomachine speed reducer.
  13. Mandet Gerard M. F. (Fericy FRX) Mouchel Jacques H. (Paris FRX), Device for varying the fluid passage area between adjacent turbine stator vanes.
  14. Baran, Kenneth C., Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system.
  15. Izquierdo, Felix; Bush, Robert H.; McAlice, Timothy J., Flow control device for a three stream turbofan engine.
  16. LeBlanc, Ryan Edward; Cummings, Kevin J., Four bar drive mechanism for bleed system.
  17. Jones, James; Maurer, John H.; Ward, Eric J.; Bursey, Jr., Roger W., Gas turbine engine duct blocker that includes a duct blocker rotor with a plurality of roller elements.
  18. Jones, James; Bursey, Jr., Roger W.; Maurer, John H.; Hawke, Larry B.; Clawson, Ronald T.; Olech, Andrew P., Gas turbine engine duct blocker with rotatable vane segments.
  19. Do, Logan H.; Krystowski, Edward A., Gas turbine engine with variable area fan nozzle.
  20. Zamora, Sean P.; Murphy, Michael Joseph, Gas turbine engine with variable area fan nozzle.
  21. Christopherson, Charles Kammer, Gas turbine engine with variable pressure ratio fan system.
  22. Scavo Steven, Integrated fluidic CD nozzle for gas turbine engine.
  23. Ruthemeyer, Michael Anthony, Integrated variable geometry flow restrictor and heat exchanger.
  24. Corsmeier, Donald Michael; Perveiler, David Andrew; Johnson, George Joseph, Method and apparatus for regulating fluid flow through a turbine engine.
  25. Bachelder, Kenneth Alan; Welty, Donald James, Methods and apparatus for supporting variable bypass valve systems.
  26. Eleftheriou, Andreas; Bruno, Vittorio; Chandler, Ian William, Pneumatic compressor bleed valve.
  27. Swanson, Timothy A.; Elving, Carl T.; Brooks, Robert T., Single actuator controlled rotational flow balance system.
  28. Harrold, Michael Charles, Stator vane actuator in gas turbine engine.
  29. Ress, Jr., Robert A., Three spool gas turbine engine having a clutch and compressor bypass.
  30. Corsmeier, Donald Michael; Dawson, David Lynn, Turbine engine valve assembly and method of assembling the same.
  31. Orlando, Robert Joseph; Moniz, Thomas Ory; Seda, Jorge Francisco, Turbofan engine cowl assembly and method of operating the same.
  32. Giffin ; III Rollin G. ; Johnson James E. ; Crall David W. ; Salvage John W. ; Szucs Peter N., Turbofan engine with a core driven supercharged bypass duct.
  33. Schirtzinger, Gary A., Valve system for a gas turbine engine.
  34. Schwark, Jr., Fred W.; Atassi, Oliver V.; Owen, William D., Variable area fan nozzle bearing track.
  35. Hubbard, Adrian Alexander, Variable mode jet engine--compact.
  36. Copeland, Andy; Ohlsson, Linnea; Freeman, Ted, Variable vane actuation system.
  37. Wong, Albert; Perez, Lucas; Tommasone, Anthony F., Variable vane actuation system.
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