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특허 상세정보

System and method for mounting an aircraft engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/054; 244/053R; 060/797; 248/554
출원번호 US-0487666 (2012-06-04)
등록번호 US-8727269 (2014-05-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Andes, William Scott
인용정보 피인용 횟수 : 7  인용 특허 : 11
초록

A mounting system and method capable of reducing backbone deflection in a high-bypass turbofan engine. The system includes a rigid structure and a linkage mechanism having at least first and second links that are each pivotally connected to the rigid structure and adapted to be pivotally connected to an engine support structure of the aircraft. The first and second links are configured to define a focal point thereof at a location that is a distance from a centerline of the engine of not more than 15% of an inlet diameter at an inlet of the engine, and i...

대표
청구항

1. A system for mounting an engine to an engine support structure of an aircraft, the engine being a turbomachine having an inlet diameter at an inlet thereof, the system comprising a rigid structure and a linkage mechanism having at least first and second links that are each pivotally connected to the rigid structure and adapted to be pivotally connected to the engine support structure, the first and second links being configured to define a focal point thereof at a location that is a distance of not more than 15% of the inlet diameter from a centerline...

이 특허에 인용된 특허 (11)

  1. Brantley, James W.. Aircraft gas turbine engine backbone deflection control. USP1994065319922.
  2. Barron Michael L. (Loveland OH) Brantley James W. (Fairfield OH) Wakeman Thomas G. (Lawrenceburg IN). Aircraft gas turbine engine backbone deflection thermal control. USP1995015385013.
  3. Stuart, Alan Roy; Fehrmann, John Robert. Clamping system and method for thrust reverser attachment. USP2013078479491.
  4. Chee Wan T. (Bellevue WA). Engine mounting assembly. USP1989084854525.
  5. Chee Wan T. (Bellevue WA). Engine mounting assembly. USP1991115064144.
  6. Manteiga, John Alan; Wilusz, Christopher James; Dykhuizen, Cornelius Harm. Fail-safe aircraft engine mounting system. USP2005016843449.
  7. Moorehead James R. (Bellevue WA). Integrated power plant installation system. USP1984034437627.
  8. Manteiga John Alan ; Dykhuizen Cornelius Harm ; Joseph Thomas Peter ; Wilusz Christopher James ; Troup Robert Eugene ; Boger Ethan ; Franceschelli Anthony John. Link component for aircraft engine mounting systems. USP2001126330985.
  9. 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.
  10. 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.
  11. Schilling Jan C. (Middletown OH). Structure for eliminating lift load bending in engine core of turbofan. USP1992125174525.