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특허 상세정보

Ducted fan gas turbine power plant mounting

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/04    F02C-007/20   
미국특허분류(USC) 60/2261 ; 60/3932
출원번호 US-0035815 (1987-04-03)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 49  인용 특허 : 2
초록

A ducted fan gas turbine powerplant is mounted to aircraft structure via a single plane mounting which comprises a single peripheral array of struts which connect the core gas generator, the fan cowl and the aircraft structure. The structure which connects the struts to the core gas generator is extended downstream of the array of struts and terminates in a plain bearing. A downstream portion of the core gas generator includes a cylindrical portion which is in sliding engagement with the plain bearing, so that radial forces generated by the movement arm,...

대표
청구항

A ducted fan gas turbine powerlant including a unitary structure comprising a plurality of mounting struts affixed by their radially inner ends to an annular strengthened outer casing portion of a core gas generator of the powerplant in peripheral alignment thereon and extending radially across the fan duct, a box structure which incorporates the radially outer ends of the struts and is fastened to aircraft structure so as to transmit powerplant loads via said struts to said aircraft structure and wherein the improvement comprises an annular portion of t...

이 특허를 인용한 특허 피인용횟수: 49

  1. Forbes, Alistair; Cox, Kenneth. Aircraft engine pylon attachment. USP2012118308105.
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  4. Wery, Xavier; Derclaye, Alain; Penalver Castro, Enrique. Architecture of a compressor rectifier. USP2014048708649.
  5. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian. Axial compressor for tip turbine engine. USP2010127845157.
  6. Nordeen, Craig A.; Suciu, Gabriel L.. Balanced turbine rotor fan blade for a tip turbine engine. USP2014088807936.
  7. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian. Cantilevered tip turbine engine. USP2011108033094.
  8. Suciu, Gabriel L.; Nordeen, Craig A.; Kramer, Stephen. Combustor for turbine engine. USP2011098024931.
  9. Merry, Brian; Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Counter-rotating compressor case and assembly method for tip turbine engine. USP2011118061968.
  10. Suciu, Gabriel; Merry, Brian; McCune, Michael E.. Counter-rotating gearbox for tip turbine engine. USP2015028950171.
  11. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Diffuser aspiration for a tip turbine engine. USP2013068468795.
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  16. Nordeen, Craig A.; Norris, James W.. Individual inlet guide vane control for tip turbine engine. USP2015038967945.
  17. Suciu, Gabriel L.; Portlock, Lawrence E.; Merry, Brian. Inflatable bleed valve for a turbine engine. USP2011077976272.
  18. Clemen, Carsten. Jet engine device with a bypass duct. USP2015129206766.
  19. Suciu, Gabriel L.; Merry, Brian. Modular tip turbine engine. USP2009127631480.
  20. Suciu, Gabriel; Roberge, Gary D.; Merry, Brian. Particle separator for tip turbine engine. USP2015049003759.
  21. Norris, James W.; Nordeen, Craig A.. Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method. USP2014028641367.
  22. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Regenerative turbine blade and vane cooling for a tip turbine engine. USP2009107607286.
  23. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.; Merry, Brian. Seal assembly for a fan rotor of a tip turbine engine. USP2011027883315.
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  25. Suciu, Gabriel L.; Roberge, Gary D.; Merry, Brian. Stacked annular components for turbine engines. USP2012018087885.
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  28. Norris, James W.; Nordeen, Craig A.. Tip turbine engine and operating method with reverse core airflow. USP2012018096753.
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  31. Suciu, Gabriel L.; Norris, James W.; Nordeen, Craig A.. Tip turbine engine comprising turbine blade clusters and method of assembly. USP2011017874802.
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  38. Norris, James W.; Nordeen, Craig A.. Tip turbine engine with reverse core airflow. USP2017019541092.
  39. Suciu, Gabriel L.; Norris, James W.; Merry, Brian. Tip turbine single plane mount. USP2015089109537.
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  49. Roberge, Gary D.. Vectoring transition duct for turbine engine. USP2010127854112.