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Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-027/00
출원번호 US-0663660 (1984-10-22)
발명자 / 주소
  • Buxton John A. (Westminister CA)
출원인 / 주소
  • Lockheed Corporation (Burbank CA 02)
인용정보 피인용 횟수 : 39  인용 특허 : 2

초록

The invention is a counterbalanced bifurcated cowling assembly for a pylon-mounted engine and nacelle therefor, the pylon 16 extending, generally, horizontally from the fuselage 15 of the aircraft 10. The assembly comprises a first cowling section 18 pivotally attached to the pylon 16 which is rotat

대표청구항

A counterbalanced bifurcated cowling assembly for a pylon-mounted engine and nacelle therefor, the pylon extending horizontally from the fuselage of an aircraft comprising: a first cowling section pivotally mounted to the pylon and rotatable from a closed position extending partially about the top o

이 특허에 인용된 특허 (2)

  1. Moorehead James R. (Bellevue WA), Nacelle assembly and mounting structures for a turbofan jet propulsion engine.
  2. Crudden Eric H. (Mercer Island WA) Jessen P. Jay (Snohomish WA), Power opening system for engine cowl doors.

이 특허를 인용한 특허 (39)

  1. Anderson Robert E. (Huntington Station NY), Advanced composite aircraft cowl.
  2. Jones,Emlyn; Stretton,Richard G, Aeroengine nacelle.
  3. Fournier, Alain; Laboure, Bernard, Aeroengine nacelle afterbodies.
  4. Klamka Andrew ; Parham Dean Leon, Aircraft engine and associated aircraft engine cowl.
  5. Bonneau, Florent; Lezerac, Julien, Aircraft nacelle comprising a spacing system which is intended to maintain the two cowls spaced apart.
  6. McEvoy, Finbarr, Aircraft propulsive power unit.
  7. Thornock, Russel L.; Sangwin, Michael L.; Hsiao, Entsung, Aircraft systems including cascade thrust reversers.
  8. Beljambe, Ceddric; Dautreppe, Frederic; Robin, Noel, Case structure interposed between the engine and the nacelle with jointed ferrule segments.
  9. Mayes,Harold G, Closure panel arrangement.
  10. Soulier, Pascal-Marie Paul Marcel; De Sorbay, Aurelie, Coupling device intended to connect first and second elements which can move relative to one another.
  11. Garcia Alain (Aussonne FRX) Tchavdarov Jean-Claude (Castelmaurou FRX) Porte Alain (Colomiers FRX), Ducted fan turbine engine.
  12. Regard, Sebastien, Fairing device for nacelle of an aircraft propulsion power unit.
  13. Langston, Todd A.; Johnson, Andrew T.; Ahrendt, Terry J., Gearless electric thrust reverser actuators and actuation system incorporating same.
  14. Layland, Michael J.; James, Norman J.; Forsey, David; Soria, Christian, Hybrid hinge and latch beam.
  15. Mercier, Claude, Latching actuation mechanism for nacelle mounted latching system.
  16. Burnett, John L.; Hackler, David W.; Wilson, Timothy C.; Welch, John M.; Popp, Thomas D.; Sawyer, Christopher S.; Hoadley, Leo B.; Fulbright, Leroy J.; Granger, Mitchel B.; Craig, Barry B.; Kenney, Phillip E., Mandrel for fabrication of a monolithic composite nacelle panel.
  17. Ahrendt, Terry, Method for controlling the deployment of jet engine thrust reversers.
  18. Wollenweber, Gary C., Methods and apparatus for exhausting gases from gas turbine engines.
  19. Stewart, Timothy; Tweedie, Alan; Hatrick, Michael, Nacelle with hinged cowl doors enabling access to the engine.
  20. Hammer, Mike, Non-handed engine cowl doors for fuselage mounted turbine engines.
  21. Vauchel, Guy Bernard; Cazuc, Xavier, Side-opening jet engine nacelle.
  22. Ahrendt, Terry, System and method for controlling the deployment of jet engine thrust reversers.
  23. Ahrendt, Terry J.; Johnson, Andrew T.; Chakkera, Kevin K., System and method for controlling the movement of an aircraft engine cowl door.
  24. Ahrendt, Terry, System and method for controlling the stowage of jet engine thrust reversers.
  25. Terry J. Ahrendt, System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system.
  26. Vauchel, Guy Bernard, Thrust reverser for a jet engine.
  27. Johnson, Andrew T., Thrust reverser position determination system and method.
  28. Welch, John Michael; Sawyer, Christopher Steven, Thrust reverser translating sleeve assembly.
  29. Soria, Christian; Chiou, Song; Layland, Michael J.; Hubert, Claude, Thrust reverser-integrated track beam and inner fixed structure.
  30. Strunk,John T.; Gabel,Bruce, Thrust reversers including latching mechanisms and methods for manufacturing such thrust reversers.
  31. Harrison, Geoffrey E.; Sternberger, Joe E.; Lallement, Michael K.; Strunk, John T.; Byrd, William S.; Jundt, Darrell C., Thrust reversers including locking assemblies for inhibiting deflection.
  32. Sternberger, Joe E., Thrust reversers including support members for inhibiting deflection.
  33. Lozano, Raphael; Strong, Kevin I.; Hoang, Andrew Mai-Tuan; Schrell, Johann S.; Soria, Christian, Track mounted hold open rod.
  34. Cloft, Thomas G.; Gukeisen, Robert L., Translatable cascade thrust reverser.
  35. Adamson Arthur P. (Cincinnati OH), Turbofan engine having a split cowl.
  36. Beutin,Bruno; Yvon,Didier; Mazeaud,Georges; Burdin,Fabien, Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position.
  37. Joret, Jean-Philippe; Segat, Peter; Vauchel, Guy Bernard; Bouret, Georges Alain, Turbojet engine nacelle including a device for absorbing circumferential stresses.
  38. Royer Wilson M. ; Gucker Mark J., Vent valve with pressure relief.
  39. Clausen Charles C. (Seattle WA) Johnson Ronald C. (Fall City WA) Chee Wan T. (Bellevue WA) Schmidt Warren E. (Erie PA), Vibration isolating engine mount.
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