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특허 상세정보

Engine mounting assembly

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/054; 244/053.0R; 248/554; 248/555; 248/556
출원번호 UP-0187943 (2005-07-25)
등록번호 US-7806363 (2010-10-26)
우선권정보 GB-0418454.5(2004-08-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Melcher, Jeffrey S.
인용정보 피인용 횟수 : 17  인용 특허 : 17
초록

An engine mounting assembly for an engine, e.g. a gas turbine engine comprises a plurality of carrying arrangements. Each carrying arrangement comprises a rear load absorbing assembly. Each load absorbing assembly provides a rear mounting point for an engine carrier. Each carrying arrangement further comprises first and second stabilising members extending forwardly from the rear mounting point of the rear load absorbing assembly to first and second spaced forward mounting points for an engine carrier.

대표
청구항

We claim: 1. A gas turbine engine mounting assembly connecting a gas turbine engine to a pylon, the engine comprising: a fan casing; and a a core casing, the mounting assembly comprising: a front beam mount connecting the fan casing to the pylon, the front beam mount carrying vertical load, side load and torque during operation of the engine; and a plurality of carrying arrangements carrying thrust, lateral and vertical loads during operation of the engine, each carrying arrangement comprising a rear load absorbing assembly connected to the core casing,...

이 특허에 인용된 특허 (17)

  1. Lymons Dennis E. ; Aten Michael R.. Actuator and safety lock system for pivoting door thrust reverser for aircraft jet engine. USP1998105826823.
  2. Dunstan Kent W.. Aircraft engine thrust mount. USP1999025873547.
  3. O\Brien Michael T. (Cincinnati OH) Bobo ; deceased Melvin (late of Cincinnati OH by Beatrice L. Bobo ; executor). Aircraft gas turbine engine sideways mount. USP1995085443229.
  4. Freid Wilbert B. (Bridgton ME). Aircraft gas turbine engine thrust mount. USP1995095452575.
  5. Breitbach Elmar J.,DEX ; Grutzmacher Torsten,DEX. Engine mount, particularly for a propeller-driven aircraft, comprising a tubular frame structure. USP2000096123293.
  6. Seaquist John D. ; Culbertson Chris. Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon. USP2000106126110.
  7. Brefort, François; Huet, Patrick; Pasquer, Félix. Jet engine suspension. USP2004076758438.
  8. Kumata Hirotaka,JPX ; Katahira Kiyoshi,JPX ; Wakita Shuichi,JPX ; Nishikawa Toshihiro,JPX. Method for reducing wave resistance in airplane. USP2000086102328.
  9. Nightingale Douglas John (Bristol EN). Mounting bypass gas turbines engines on aircraft. USP1977034013246.
  10. Rodgers Leonard J.,GB2 ; Newton Arnold C.,GB2 ; Berry James P.,GB2 ; Farrar Peter G. G.,GB2 ; Udall Kenneth F.,GB2. Mounting for coupling a turbofan gas turbine engine to an aircraft structure. USP1998055746391.
  11. Marche,Herv챕. Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft. USP2006067063290.
  12. Brodell Robert F. (Marlborough CT) Hovan Edward J. (Manchester CT) Selfors Steven T. (Somerville MA) Loffredo Constantino V. (Newington CT) Duesler Paul W. (Manchester CT). Nacelle and mounting arrangement for an aircraft engine. USP1996065524847.
  13. Smith Michael A. (Tacoma WA). Strut supported inlet. USP1984074458863.
  14. White John L. (Bellevue WA). System for mounting a jet engine. USP1986084603821.
  15. John Alan Manteiga ; Christopher James Wilusz ; Cornelius Harm Dykhuizen. System for mounting aircraft engines. USP2002066401448.
  16. Standish Robert R.,FRX. Thrust reverser for high bypass fan engine. USP1999015863014.
  17. Lair Jean-Pierre (8023 Vantage ; Suite 1450 San Antonio TX 78230). Thrust reverser integrating a variable exhaust area nozzle. USP1993015181676.

이 특허를 인용한 특허 피인용횟수: 17

  1. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. AFT engine nacelle shape for an aircraft. USP2017119815560.
  2. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP2017119821917.
  3. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP20180710017270.
  4. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David. Aft engine for an aircraft. USP2018059957055.
  5. Journade, Frédéric; Jalbert, Delphine. Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine. USP2014058733693.
  6. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Aircraft having an aft engine. USP2017059637217.
  7. Vauchel, Guy Bernard. Deformable structural framework for a turbofan nacelle. USP2014038668441.
  8. Kupiszewski, Thomas; Miller, Brandon Wayne; Vondrell, Randy M.. Electric propulsion system. USP20181010093428.
  9. Miller, Brandon Wayne; Vondrell, Randy M.; Marrinan, Patrick Michael; Gemin, Paul Robert; Moore, Nicholas Taylor. Electric propulsion system for an aircraft. USP20181110137981.
  10. Kupiszewski, Thomas; Miller, Brandon Wayne; Vondrell, Randy M.; Gemin, Paul Robert. Embedded electric machine. USP20180910071811.
  11. Hamel, Jeffrey Anthony; Murrow, Kurt David. Gas-electric propulsion system for an aircraft. USP20180610000293.
  12. Clemen, Carsten. Jet engine device with a bypass duct. USP2015129206766.
  13. Glover, Anthony R.. Lightweight engine mounting. USP2015099145047.
  14. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Non-axis symmetric aft engine. USP2018029884687.
  15. Niergarth, Daniel Alan; Vondrell, Randy M.; Miller, Brandon Wayne; Marrinan, Patrick Michael. Propulsion engine for an aircraft. USP20190410252810.
  16. Vondrell, Randy M.; Polakowski, Matthew Ryan; Murrow, Kurt David; Crabtree, Glenn. Propulsion system for an aircraft. USP2017099764848.
  17. Vauchel, Guy Bernard; Gibouin, Anne-Laure; Fassier, Regis; Joret, Jean-Philippe; Collier, Jerome; Lefort, Guillaume; Chouard, Pierre-Alain. Structural nacelle. USP2014068739552.