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Aircraft propulsive power unit assembly having a leading edge lipskin and intake barrel

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-029/08
출원번호 US-0649609 (1996-05-24)
우선권정보 GB-0007632 (1994-04-18)
국제출원번호 PCT/GB95/00830 (1995-04-12)
§371/§102 date 19960524 (19960524)
국제공개번호 WO-9528318 (1995-10-26)
발명자 / 주소
  • Sherry Philip David,GBX
  • Welsh Robert,GBX
  • Johnson Kenneth Henry,GBX
출원인 / 주소
  • Short Brothers PLC, IEX
대리인 / 주소
    Fish & Richardson P.C.
인용정보 피인용 횟수 : 39  인용 특허 : 6

초록

An aircraft propulsive power unit comprises an engine, a nacelle structure which houses the engine and which includes displaceable nacelle portions which form a forward part of the nacelle structure and which take up operational positions in which a forward end of each nacelle portion forms part of

대표청구항

[ We claim:] [1.] An aircraft propulsive power unit comprising an engine, a nacelle structure which houses the engine and which includes a displaceable nacelle portion which forms a forward part of the nacelle structure and which takes up an operational position in which a forward end thereof forms

이 특허에 인용된 특허 (6)

  1. Cole Derek (Bangor IEX) Sherry Philip D. (Larne IEX) Blair Alan J. (Holywood IEX), Aircraft propulsive power unit.
  2. Vetter Earl E. (Mercer Island WA), Common pod for housing a plurality of different turbofan jet propulsion engines.
  3. Armstrong Norman (Newtownards GB5), Ducted fan turbine engine nozzle assembly.
  4. Carlin Robert N. (Nottingham GB2) Deighton Andrew W. (Derby GB2), Mounting arrangement for a gas turbine engine.
  5. Bart Jacques R. (Evry FRX), Pod for a turbofan aero engine of the forward contrafan type having a very high bypass ratio.
  6. Crudden Eric H. (Mercer Island WA) Jessen P. Jay (Snohomish WA), Power opening system for engine cowl doors.

이 특허를 인용한 특허 (39)

  1. Suciu, Gabriel L.; Chandler, Jesse M., ATR axial V-groove.
  2. Suciu, Gabriel L.; Chandler, Jesse M., ATR full ring sliding nacelle.
  3. Suciu, Gabriel L.; Chandler, Jesse M., ATR guide pins for sliding nacelle.
  4. Chiou, Song; Yu, Jia; Hubert, Claude; Layland, Michael, Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers.
  5. Fournier, Alain; Laboure, Bernard, Aeroengine nacelle afterbodies.
  6. Joret, Jean-Philippe; Baillard, André, Air inlet structure for a turbojet engine nacelle of laminar type.
  7. Chaumeret,Michel; Mazeaud,Georges, Air input device for a turboprop engine.
  8. Klamka Andrew ; Parham Dean Leon, Aircraft engine and associated aircraft engine cowl.
  9. Shutrump, Jeffrey D., Aircraft engine inlet having zone of deformation.
  10. Shutrump, Jeffrey D., Aircraft engine inlet having zone of deformation.
  11. Alain Porte FR, Aircraft propulsion unit fan cowls equipped with maintaining and positioning safety elements.
  12. Etling, Keith A., Apparatus and method for sealing surfaces.
  13. Tsou, Chi-Ling Michael; Holdren, Carl Francis; Bailey, William Andrew; Lenahan, Dean Thomas, Baffle seal for gas turbine engine thrust reverser.
  14. Stuart, Alan Roy; Fehrmann, John Robert, Clamping system and method for thrust reverser attachment.
  15. Andre, Robert; Dussol, Loic; Ridray, Frederic, Closing system for an aircraft fan shroud.
  16. Stretton, Richard G; Udall, Kenneth F, Cowl structure for a gas turbine engine.
  17. Stretton,Richard G; Udall,Kenneth F, Cowl structure for a gas turbine engine.
  18. Liston Laurence D. N. ; Schoepf Joseph L. ; Royalty Charles Michael, Detachable integral aircraft tailcone and power assembly.
  19. Rolt, Andrew M, Engine.
  20. Cloft, Thomas G., Gas turbine engine assembly including accessory components within the nacelle.
  21. Riou, Georges Jean Xavier; Verseux, Philippe, Inner wall for a turbomachine nacelle.
  22. Suciu, Gabriel L.; Chandler, Jesse M., Integrated nozzle and plug.
  23. Porte, Alain; Lalane, Jacques, Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together.
  24. Mercier, Claude; Cloft, Thomas G., Nacelle inner flow structure leading edge latching system.
  25. Stewart, Timothy; Tweedie, Alan; Hatrick, Michael, Nacelle with hinged cowl doors enabling access to the engine.
  26. James, Norman John, Nacelle with longitudinal translating cowling and rotatable sleeves.
  27. Allford, Peter, Panel assembly including deformable seal.
  28. Suciu, Gabriel L.; Chandler, Jesse M.; Bomzer, T. David, Pivot thrust reverser surrounding inner surface of bypass duct.
  29. Suciu, Gabriel L.; Chandler, Jesse M., Pivot thrust reverser with multi-point actuation.
  30. Chiou, Song; Yu, Jia; Hubert, Claude; Layland, Michael, Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure.
  31. Vauchel, Guy Bernard; Epherre-Iriart, Serge, Removable air intake structure for a turbofan engine nacelle.
  32. Pierce, David, Set of latches with identical components for nacelle doors.
  33. Gleason, Michael P.; Pulcher, Daniel Eugene; Roberts, Anthony C.; Keyes, William John; Arrowsmith, Michael Allan; Kauffman, Elizabeth Kay; Lambrecht, Amoret Margaret; Tegeler, Alan F.; Gipperich, Robert A.; Coffman, Mathew Albert, Surface sealing system.
  34. Chandler, Jesse M.; Suciu, Gabriel L., Tandem thrust reverser with multi-bar linkage.
  35. Suciu, Gabriel L.; Chandler, Jesse M., Tandem thrust reverser with multi-point actuation.
  36. Chandler, Jesse M.; Suciu, Gabriel L., Tandem thrust reverser with sliding rails.
  37. Chandler, Jesse M.; Suciu, Gabriel L., Tandem thrust reverser with sliding rails.
  38. Maguire, Alan R; Udall, Kenneth F; Stretton, Richard G, Thrust reverser mounting structure.
  39. Fournier, Alain; Laboure, Bernard; Standish, Robert, Turboprop unit for aircraft with improved aerodynamic installation.
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