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특허 상세정보

Engine mounting structure interposed between an aircraft wing system and said engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/054; 248/554
출원번호 US-0065837 (2006-09-26)
등록번호 US7967242 (2011-06-15)
우선권정보 FR-2005-5 52900(2005-09-27)
국제출원번호 PCT/EP2006/066736 (2006-09-26)
§371/§102 date 20080305 (20080305)
국제공개번호 WO07/036519 (2007-04-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
인용정보 피인용 횟수 : 3  인용 특허 : 12
초록

A device for suspension of an engine, configured to be inserted between an aircraft wing and the engine. The device includes a rigid structure and a forward aerodynamic structure mounted fixed on the structure through a suspension mechanism. The forward aerodynamic structure is configured to carry engine fan casings and to be inserted between the rigid structure and the wing. The suspension mechanism includes at least one adjustable length connecting rod of which one end is mounted on the rigid structure, and the other end is mounted on the forward aerod...

대표
청구항

The invention claimed is: 1. A suspension device for suspension of an engine, configured to be inserted between an aircraft wing and the engine, the suspension device comprising:a rigid structure; anda forward aerodynamic structure coupled to the rigid structure through suspension means, the forward aerodynamic structure being configured to carry an engine fan casing and to be inserted between the rigid structure and the wing,wherein the suspension means includes at least one adjustable length connecting rod of which one end is mounted on the rigid struc...

이 특허에 인용된 특허 (12)

  1. Cohen Mordehy (Rockford IL). Deployment mechanism for a ram air turbine. USP1987064676458.
  2. MacGee Andrew (Cincinnati OH). Duct support assembly. USP1992025088279.
  3. Olivier J-F Cazenave GB. Gas turbine engine mounting arrangement. USP2002116474597.
  4. Seaquist John D. ; Culbertson Chris. Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon. USP2000106126110.
  5. 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.
  6. Marche,Herve. Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft. USP2007067232091.
  7. 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.
  8. 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.
  9. Parkinson, Colin C. A.; Kinnerly, Anthony G.. Power plant attachment arrangements for aircraft wings. USP1985124560122.
  10. Chee Wan T. (Bellevue WA). Pylon and engine installation for ultra-high by-pass turbo-fan engines. USP1995115467941.
  11. Cohen Mordehy (Rockford IL) Kezar David A. (Loves Park IL). Ram air turbine indexing mechanism. USP1988014717095.
  12. Bhatia Kumar G. (Mercer Island WA) Backus Walter E. (Kent WA) Hagelin Jack S. (Seattle WA). Vibration damping aircraft engine attachment. USP1991115065959.