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특허 상세정보

Engine mounting assembly

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-029/02   
미국특허분류(USC) 244/54 ; 248/5
출원번호 US-0534830 (1974-12-20)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 15  인용 특허 : 0
초록

A lightweight engine mounting assembly for attaching an engine to the wing of an airplane includes an outboard beam, an inboard beam, a forward annular stabilizing member and upper and lower, rear stabilizing members. Rearward extensions of the inboard and outboard beams have upper portions that extend rearwardly over the upper airfoil surface of a wing and lower portions that extend rearwardly and under the lower surface of the wing. The rearward extensions of the inboard and outboard beams are attached to the front main spar and to the upper and lower ...

대표
청구항

An assembly for mounting an engine on an aircraft wing having a leading edge, an upper surface, and a lower surface, said engine having a longitudinal dimension and a transverse dimension comprising: an inboard beam having a rearward section and a forward section, said rearward section having an upper portion and a lower portion, said uppeR portion extending in a chordwise direction over the upper surface of said wing and having a bottom edge conforming to the shape of and engaging the upper surface of said wing, said lower portion extending in a chordwi...

이 특허를 인용한 특허 피인용횟수: 15

  1. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing engine and engine nacelle combination. USP1984054449680.
  2. Gratzer Louis B. (Seattle WA) Gillette Walter B. (Issaquah WA). Aerodynamically contoured, low drag wing, engine and engine nacelle combination. USP1984054449681.
  3. Diochon, Lionel; Durand, Jerome. Aircraft engine assembly. USP2010067740200.
  4. Diochon, Lionel; Sarrato, Michael; Chartier, David; Petrissans, Isabelle. Aircraft jet engine pylon suspension attachment. USP2011077971825.
  5. Mayes,Harold G. Closure panel arrangement. USP2007087255307.
  6. Stuhr, Victor K.. Ducted open rotor apparatus and method. USP2010127850116.
  7. Williams,Nicholas A.. Integrated mount duct for use with airborne auxiliary power units and other turbomachines. USP2008097419121.
  8. West, Randall Ray. Intermediate structure for independently de-mountable propulsion components. USP2015129212607.
  9. Todorovic, Predrag. Joint between components. USP20180810054007.
  10. Mauldin, Jack W.; Kwok, David W.; Weidler, John A.; Gonzales, Antonio B.; Lawson, Edward L.; Kulak, Andrew C.. Methods and apparatus for supporting engines and nacelles relative to aircraft wings. USP2016119505499.
  11. Poisson, Mathieu Ange; Bellabal, Francois Robert; Florent, Nicolas. Suspension structure for suspending a turboprop having two unducted propellers from a structural element of an aircraft with rigid fastening of the air intake structure. USP20181010106266.
  12. John Alan Manteiga ; Christopher James Wilusz ; Cornelius Harm Dykhuizen. System for mounting aircraft engines. USP2002066401448.
  13. Tiemon, Jorg Arrien. Systems and methods for mounting a rotatable machine. USP20190210197213.
  14. Howarth,Nicholas; Freeman,Christopher. Turbine engine arrangements. USP2007017165744.
  15. Watson, Bill Russell; Warden, Max. Turbomachine core coupling assembly. USP2014018621874.