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특허 상세정보

Power plant attachment arrangements for aircraft wings

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/054; 248/554
출원번호 US-0569896 (1984-01-11)
우선권정보 GB-19830000748 (1983-01-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cushman, Darby & Cushman
인용정보 피인용 횟수 : 18  인용 특허 : 2
초록

An attachment arrangement for connecting a jet propulsion power plant to an aircraft wing, the power plant lying generally forward and below the wing, wherein the engine is not only anchored in the vertical, lateral and fore-and-aft senses against bodily displacement with reference to the wing, but is anchored against angular movement in its pitch, roll and yaw senses in the event of partial or total failure of any one element of the attachment arrangement.

대표
청구항

1. A power plant attachment arrangement for an engine lying generally forward and below an aircraft wing, including a fore-and-aft extending engine-carrying beam member, a spanwise extending wing structural member, and means interconnecting the two, the interconnecting means including a forward element, pin means pinning respective ends of the forward element to the wing structural member and to the beam member such that the forward element extends downwardly and forwardly with respect to the aircraft wing, a rearward element of A-shape in plan, pin mean...

이 특허를 인용한 특허 피인용횟수: 18

  1. Lafont, Laurent; Journade, Frederic; Renaud, Eric. Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins. USP2014088794568.
  2. Hager Thomas R. (Bothell WA) Lakin Gerald C. (Bellevue WA) Rogers John T. (Snohomish WA). Apparatus and methods for reducing aircraft lifting surface flutter. USP1990044917331.
  3. Lafont, Laurent. Assembly for aircraft comprising a wing system element as well as an attachment mast. USP2011087997527.
  4. Marche, Jacques Herve; Raison, Fabien. Engine attachment pylon comprising means of fastening spars and panels located outside the inner space in the box. USP2013078474750.
  5. Chee Wan T. (Bellevue WA). Engine mounting assembly. USP1989084854525.
  6. Combes, Stephane; Lafont, Laurent. Engine mounting structure interposed between an aircraft wing system and said engine. USP2011067967242.
  7. Machado,Stephane; Cassagne,Jerome; Del Blanco,Anthony; Martin,Yvon; Chambreuil,Arnaud. Engine mounting structure under an aircraft wing. USP2008117451947.
  8. Marche, Herv?. Hooking strut of an engine under the wing unit of an aircraft. USP2005096938855.
  9. Duesler Paul W.. Mounting arrangement for a gas turbine engine. USP1998075775638.
  10. West, Randall Ray. Pylon arrangement for open structure. USP2015059027875.
  11. Teulou, Olivier; Diochon, Lionel; Petrissans Lloveras, Isabelle. Pylon for attaching an aircraft turbine engine comprising aligned front wing ties. USP2014088814079.
  12. Demouzon Fran.cedilla.is Michel,FRX ; Fer Rene Pierre,FRX ; Huet Patrick Jean Alibert,FRX ; Marnas Laurent Pierre Elysee Gaston,FRX. Redundant front suspension system for a turboshaft engine. USP1999025871176.
  13. Demouzon Francis Michel,FRX ; Fer Rene Pierre,FRX ; Alibert Huet Patrick Jean,FRX ; Marnas Laurent Pierre Elysee Gaston,FRX. Redundant front suspension system for a turboshaft engine. USP1999025871175.
  14. Demouzon Francis Michel,FRX ; Fer Rene Pierre,FRX ; Huet Patrick Jean Alibert,FRX ; Marnas Laurent Pierre Elysee Gaston,FRX. Redundant front suspension system for a turboshaft engine. USP1999025871177.
  15. Powell Donald T.. Strut-wing interface having dual upper links. USP2000086095456.
  16. Guillou, Pierrot. Suspension for a turbine engine. USP2016079394057.
  17. Howarth,Nicholas; Freeman,Christopher. Turbine engine arrangements. USP2007017165744.
  18. Herbst Paul T. (Lord Corporation ; 2000 W. Grandview Blvd ; P.O. Box 10038 Erie PA 16514-0038). Turbine engine mounting bracket assembly. USP1989024805851.