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Engine mount 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-027/18
출원번호 US-0592440 (1975-07-02)
발명자 / 주소
  • Boris Paul A. (Ellington CT) Marx Jon A. (Manchester CT)
출원인 / 주소
  • United Technologies Corporation (Hartford CT 02)
인용정보 피인용 횟수 : 55  인용 특허 : 0

초록

The loads manifested by and imposed on the engine are transmitted through a mounting formed on a single plane with a three point attachment permitting the engine to be cantilever mounted although not limited thereto, and allows for the engine to project considerably forward of an airfoil section to

대표청구항

A support system to mount a turbine type power plant to aircraft structure wherein the power plant includes an outer case having a given annular portion adapted to receive the support system, a yoke for partially receiving said annular portion of said power plant case, a first pin at the bottom of s

이 특허를 인용한 특허 (55)

  1. Sandy, David F; Zheng, Zhijun, Adjustable engine mount.
  2. Diochon, Lionel; Durand, Jerome, Aircraft engine assembly.
  3. Diochon, Lionel; Sarrato, Michael; Chartier, David; Petrissans, Isabelle, Aircraft jet engine pylon suspension attachment.
  4. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  5. Suciu, Gabriel L.; Norris, James W; Nordeen, Craig A.; Merry, Brian, Annular turbine ring rotor.
  6. Goodro, Jerry B.; Higgs, Thomas W., Apparatus for load transfer between aerospace vehicle components, aerospace vehicles including same, and method of attachment of aerospace vehicle components.
  7. Legrand Paul J. (Vaux le Penil FRX) Notheaux Andre R. (Palaiseau FRX) Pachomoff Guy R. (Corbeil-Essonnes FRX) Romanoff Alexis M. G. (Cesson FRX), Apparatus for the installation of a jet engine in an aircraft compartment.
  8. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian, Axial compressor for tip turbine engine.
  9. Nordeen, Craig A.; Suciu, Gabriel L., Balanced turbine rotor fan blade for a tip turbine engine.
  10. Larrochelle, Jean; Peyruseigt, François, Ball slide bearing and connecting device associated with a mast for hooking a gas turbine engine under an aircraft wing comprising such a bearing.
  11. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian, Cantilevered tip turbine engine.
  12. Suciu, Gabriel L.; Nordeen, Craig A.; Kramer, Stephen, Combustor for turbine engine.
  13. Merry, Brian; Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Counter-rotating compressor case and assembly method for tip turbine engine.
  14. Suciu, Gabriel; Merry, Brian; McCune, Michael E., Counter-rotating gearbox for tip turbine engine.
  15. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Diffuser aspiration for a tip turbine engine.
  16. Godbersen Byron L. (710 Circle Dr. Ida Grove IA), Ducted fan unit.
  17. Suciu, Gabriel L.; Roberge, Gary D., Ejector cooling of outer case for tip turbine engine.
  18. Diochon, Lionel; El Hammami, Samir; Le Louvetel-Poilly, Julie; Dumas, Jean-Baptiste; Koenig, Nicolas, Engine assembly for aircraft comprising an engine and a mounting device for such an engine.
  19. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine.
  20. Nordeen, Craig A.; Norris, James W., Individual inlet guide vane control for tip turbine engine.
  21. Suciu, Gabriel L.; Portlock, Lawrence E.; Merry, Brian, Inflatable bleed valve for a turbine engine.
  22. Williams,Nicholas A., Integrated mount duct for use with airborne auxiliary power units and other turbomachines.
  23. Kumar, Avinash; Brockett, Theodore; Chinthapally, Srinivas; Kumbham, Krishna Mohan; Khare, Milind; Ganji, Venkatarao; Kandula, Rama Sateesh Venkata, Method and apparatus for reducing high transient mount load in aircraft engine mounting systems.
  24. Suciu, Gabriel L.; Merry, Brian, Modular tip turbine engine.
  25. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian, Particle separator for tip turbine engine.
  26. Norris, James W.; Nordeen, Craig A., Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method.
  27. Coraboeuf, Yohann; Dutheil, Jean-Philippe, Propulsion unit for reusable launch vehicle.
  28. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Regenerative turbine blade and vane cooling for a tip turbine engine.
  29. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Seal assembly for a fan rotor of a tip turbine engine.
  30. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Seal assembly for a fan-turbine rotor of a tip turbine engine.
  31. Penda, Allan R.; Merry, Brian D.; Suciu, Gabriel L.; Dye, Christopher M., Single plane mount system for gas turbine engine.
  32. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian, Stacked annular components for turbine engines.
  33. Merry, Brian; Webb, Scot Adams; McCune, Michael, Starter generator system for a tip turbine engine.
  34. Suciu, Gabriel L.; Alvanos, Ioannis, TEC mount redundant fastening.
  35. Norris, James W.; Nordeen, Craig A., Tip turbine engine and operating method with reverse core airflow.
  36. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine engine composite tailcone.
  37. Suciu, Gabriel L.; Merry, Brian; Portlock, Lawrence, Tip turbine engine comprising a nonrotable compartment.
  38. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Tip turbine engine comprising turbine blade clusters and method of assembly.
  39. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A., Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor.
  40. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine engine integral case, vane, mount and mixer.
  41. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian, Tip turbine engine integral fan, combustor, and turbine case.
  42. Suciu, Gabriel L.; Merry, Brian, Tip turbine engine support structure.
  43. Suciu, Gabriel L.; Merry, Brian, Tip turbine engine with a heat exchanger.
  44. Norris, James W.; Nordeen, Craig A.; Roberge, Gary, Tip turbine engine with multiple fan and turbine stages.
  45. Norris, James W.; Nordeen, Craig A., Tip turbine engine with reverse core airflow.
  46. Suciu, Gabriel L.; Norris, James W.; Merry, Brian, Tip turbine single plane mount.
  47. Roberge, Gary D., Turbine blow down starter for turbine engine.
  48. Suciu, Gabriel L.; Alvanos, Ioannis; Merry, Brian, Turbine engine case mount and dismount.
  49. Soloy Joe I. (Centralia WA), Turbine engine drive and mounting assembly for fixed wing aircraft.
  50. Suciu, Gabriel L.; Pagluica, Gino J.; Duong, Loc Quang; Portlock, Lawrence E., Turbine engine with differential gear driven fan and compressor.
  51. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly for gas turbine engine.
  52. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method.
  53. Suciu, Gabriel L.; Merry, Brian; Norris, James W.; Sirica, Steven J., Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method.
  54. Roberge, Gary D., Vectoring transition duct for turbine engine.
  55. Lardellier Alain M. J. (Melun FRX), Wing mounting nacelle for a very high by-pass ratio turbojet aero-engine.
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