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특허 상세정보

Method for operating a landing gear assembly with a breaker strut

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-025/10    B64C-025/20   
미국특허분류(USC) 244/102A; 244/100R; 244/102R
출원번호 US-0376160 (2010-06-03)
등록번호 US-8602352 (2013-12-10)
우선권정보 FR-09 02721 (2009-06-05)
국제출원번호 PCT/EP2010/057778 (2010-06-03)
§371/§102 date 20111202 (20111202)
국제공개번호 WO2010/139756 (2010-12-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sughrue Mion, PLLC
인용정보 피인용 횟수 : 14  인용 특허 : 5
초록

A method of operating an aircraft landing gear between a deployed position and a retracted position. The landing gear comprises a leg hinged to the aircraft, the leg being stabilized in the deployed position by a folding strut comprising two hinged-together links, the strut being held in an aligned position by a stabilizer member comprising two hinged-together links themselves held in alignment by a locking member. The method comprises the steps of arranging the strut (2; 102) and the stabilizer member (4; 104) in such a manner that at least one of the l...

대표
청구항

1. An aircraft landing gear comprising: a leg hinged to the aircraft and operable between a deployed position and a retracted position, the leg being stabilized in the deployed position by a folding strut comprising two hinged-together links, the strut being held in an aligned position by a stabilizer member comprising two hinged-together links, the links of the strut being held in alignment by a locking member,wherein the strut and the stabilizer member are arranged in such a manner that at least one of the links of the stabilizer member moves continuou...

이 특허를 인용한 특허 피인용횟수: 14

  1. Guering, Bernard. Center pedestal for aircraft cockpit and aircraft comprising such a pedestal. USP2017089731823.
  2. Guering, Bernard. Compact improved aircraft landing gear. USP2016039272775.
  3. Ducos, Dominique. Device for unlocking an undercarriage in a deployed position, and an undercarriage fitted with such a device. USP2015099145204.
  4. Evans, Royston; Tierney, Malcolm. Electrical actuator incorporating a free play mechanism to eliminate force fighting. USP2015049004401.
  5. Ditzler, Adam J.. Electrically powered downlock actuation system. USP20181010086928.
  6. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Szulyk, Zenon P.. Rotary piston actuator anti-rotation configurations. USP2017049631645.
  7. Kim, Joseph H.; O Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP2016019234535.
  8. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator. USP20180710030679.
  9. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017079709078.
  10. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2017119816537.
  11. Kim, Joseph H; O'Hara, Robert P; Hydari, Shahbaz H; Sobolewski, Pawel A.. Rotary piston type actuator with a central actuation assembly. USP2015109163648.
  12. Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.; Sobolewski, Pawel A.; Szulyk, Zenon P.. Rotary piston type actuator with hydraulic supply. USP2017039593696.
  13. Sobolewski, Pawel A.; Kim, Joseph H.; Szulyk, Zenon P.. Rotary piston type actuator with modular housing. USP2016109476434.
  14. Sobolewski, Pawel A.; Kim, Joseph H.; O'Hara, Robert P.; Hydari, Shahbaz H.. Rotary piston type actuator with pin retention features. USP2015028955425.