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특허 상세정보

Mounting system for a thrust generating engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/20    B64D-027/16   
미국특허분류(USC) 60/200R ; 60/3931 ; 244/54 ; 248/5
출원번호 US-0572647 (1975-04-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 18  인용 특허 : 0
초록

An improvement in a mounting system for mounting a thrust generating engine to an aircraft wherein force generating means are operatively connected to a casing surrounding and supporting the engine for applying a variable force to the casing for maintaining the engine in a predetermined position relative to said aircraft.

대표
청구항

In a system for mounting a thrust generating engine to an aircraft wherein the engine includes a casing for enclosing and supporting at least some of the thrust generating elements of the engine and said mounting system includes means connecting the casing to the aircraft for retaining said engine against rotational, axial, vertical and side movement relative to said aircraft, the improvement comprising: force generating means operatively connected to said casing for generating a variable force for application to said casing for maintaining said engine i...

이 특허를 인용한 특허 피인용횟수: 18

  1. Stretton,Richard G; Beardsley,Peter K; Beaven,David M. Aircraft engine mounting assembly. USP2007117296414.
  2. Brantley, James W.. Aircraft gas turbine engine backbone deflection control. USP1994065319922.
  3. Whitmer,Brett D.; Rockwell,Glen C.; Tanner,Richard B.. Apparatuses and methods for attaching engines and other structures to aircraft wings. USP2006087083143.
  4. Balk, Wouter. Attachment of a multiflow turbojet engine to an aircraft. USP2012078215580.
  5. Greenberg Paul B. (Manchester CT) Lenkeit C. Heinz (South Windsor CT) Seibert Willard J. (Manchester CT). Case deflection control in aircraft gas turbine engines. USP1984014428189.
  6. Edgley John K. (Elsworth GB2). Ducted propeller aircraft. USP1983024371133.
  7. Hodgkinson Carl (Derby GB2). Engine mount including engine mount failure indicator. USP1991034997145.
  8. Erdmann Hermann (Weyhe DEX) Rahm Heiko (Hamburg DEX). Gas generator. USP1987124710359.
  9. Williamson Willie (Derby GB2). Gas turbine engine casing. USP1985014492078.
  10. Bower Charles R. (Middletown CT) Fowler Frank L. (Guilford CT). Load sharing for engine nacelle. USP1987044658579.
  11. Sargisson Donald F. (Cincinnati OH). Long duct mixed flow gas turbine engine. USP1979044147029.
  12. 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.
  13. 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.
  14. Smith Michael A. (Tacoma WA). Strut supported inlet. USP1984074458863.
  15. Alexander, Eric J.. System and method for aft mount of gas turbine engine. USP2018069988155.
  16. White John L. (Bellevue WA). System for mounting a jet engine. USP1986084603821.
  17. Herbst Paul T. (Lord Corporation ; 2000 W. Grandview Blvd ; P.O. Box 10038 Erie PA 16514-0038). Turbine engine mounting bracket assembly. USP1989024805851.
  18. Watson, Bill Russell; Warden, Max. Turbomachine core coupling assembly. USP2014018621874.