$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Aircraft undercarriage lock mechanism

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-025/10   
미국특허분류(USC) 244/102SL ; 244/102R
출원번호 US-0486435 (2000-02-28)
우선권정보 GB0003353 (1999-02-16)
국제출원번호 PCT/GB00/00292 (2000-02-02)
§371/§102 date 20000228 (20000228)
국제공개번호 WO-0048903 (2000-08-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Nixon & Vanderhye P.C.
인용정보 피인용 횟수 : 10  인용 특허 : 6
초록

An aircraft undercarriage mechanism 20 comprising a first lock member 22 mounted on the undercarriage 14, the first lock member being engageable with a second lock member 24 mounted on a wing 10 of the aircraft. The first lock member 22 comprises a pivotable arm 26 which carries a roller 36. The roller 36 is rotatable and slidable on the arm 26 and is engageable with a catch 48 on the second lock member 24. The provision of the pivotable arm 26 and slidable roller 36 permits relative movement between the lock members 22, 24 when the undercarriage 14 is r...

대표
청구항

[ What is claimed is:] [1.]1. An aircraft undercarriage mechanism comprising a first lock member for mounting on the undercarriage, said first lock member being engageable with a second lock member for mounting on a support part of the aircraft, one of said lock members including means which permits relative movement in more than one direction between said lock members when the undercarriage is retracted with said lock members interengaged to minimise transmission of forces created by wing deflection from one lock member to the other.

이 특허를 인용한 특허 피인용횟수: 10

  1. Schmidt, Robert Kyle. Aircraft landing gear assembly. USP20190210196132.
  2. La Commara, Domenico; Faure, Thibault. Aircraft landing gear provided with an adjustable roller. USP2017129834302.
  3. Franklin, III, Walter M.; Morgenstern, John M.; Lee, Howard; Quayle, Brian; Hajic, Ken; Scarcello, John; Arslan, Alan E.. Aircraft tail configuration for sonic boom reduction. USP2004116824092.
  4. Quayle, Brian. Forward inboard retracting main landing gear. USP2005096942182.
  5. Collet, Olivier; Felemez, Eric; Liegeois, Pierre-Yves; Fremiot, Sébastien; Perathoner, Dominique. Latch device, in particular for latching an airplane landing gear or an airplane landing gear hatch. USP2004116811118.
  6. Collet, Olivier; Felemez, Eric; Liegeois, Pierre-Yves; Fremiot, Sébastien; Perathoner, Dominique. Latch device, in particular for latching an airplane landing gear or an airplane landing gear hatch, and a method of operating said device. USP2004106802476.
  7. Tran, Hai H.. Locking mechanism with bi-modal actuator. USP2014088814094.
  8. Lafitte, Arnaud; Balducci, Gérard. Selective force transmission device and an undercarriage consisting of an application thereof. USP2014098833693.
  9. Chang, Ming; Meza, Victor; Morgenstern, John M.; Arslan, Alan E.. Supersonic aircraft with channel relief control. USP2005076921045.
  10. Quayle,Brian; Morgenstern,John M.; Arslan,Alan E.. Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction. USP2007057216830.