$\require{mediawiki-texvc}$
  • 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 fore structure

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/00   
미국특허분류(USC) 244/119 ; 244/102R
출원번호 US-0245842 (1999-02-08)
우선권정보 FR0010550 (1998-08-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Burns, Doane, Swecker & Mathis, LLP
인용정보 피인용 횟수 : 21  인용 특허 : 1
초록

An aircraft fore-structure for wide- and very-wide body freight aircraft that is characterized by the presence of a unpressurized landing gear compartment in the lower fore end section. The landing gear compartment is formed by a ceiling at the top, that is preferably domed, and by a partition towards the rear. A door that is provided in the partition provides access through the landing gear compartment to the pressurized compartment located behind said partition. An opening in the fore of the landing gear compartment also provides access to the radar ch...

대표
청구항

[ What is claimed is:] [1.]1. An aircraft fore structure comprising:a pressurized compartment; andan unpressurized landing gear compartment that is suitable to house fore landing gear in the retracted position, in which the unpressurized landing gear compartment constitutes a lower fore end section of the fore structure, and the unpressurized landing gear compartment is separated from the pressurized compartment by a ceiling and a rear partition, wherein the landing gear compartment comprises an extension towards the rear, beyond said rear partition, the...

이 특허를 인용한 특허 피인용횟수: 21

  1. Guering, Bernard. Aircraft comprising a landing gear compartment permitting better integration of the landing gear. USP2011027891606.
  2. Wood, Jeffrey H.; Ngo, Lamvien H.. Aircraft nose landing gear enclosure. USP2010017641146.
  3. Gallant, Guillaume; Biennes, Herve. Aircraft nose provided with a connecting frame between the landing gear housing and the outer skin of the fuselage. USP2017129840321.
  4. Bernadet, Philippe; Lieven, Patrick; Dugerie, Marc; Mialhe, Christophe; Delahaye, Romain. Aircraft nose structure with landing gear compartment. USP2014128905352.
  5. Dazet,Francis; Maurens,No��l. Aircraft nose with shield. USP2008067384015.
  6. Cazals, Olivier; Genty de la Sagne, Jaime. Aircraft with retracted front landing gear. USP2013108550400.
  7. Müller, Markus; Fiedler, Lars. Airframe structure of an aircraft or spacecraft. USP2011098016234.
  8. Guering, Bernard; Guering, Jonathan. Casing and front landing gear assembly for an aircraft. USP2012098262020.
  9. Perez Sanchez,Juan. Closure system for a support structure. USP2009037503523.
  10. Alby, Sebastien; Gauthie, Laurent; Bernadet, Philippe. Composite internal beam for reinforcing the structure of an aircraft. USP2010107810756.
  11. Guering, Bernard; Guering, Jonathan. Front aircraft part comprising a flat partition between a pressurised zone and a non-pressurised zone housing landing gear. USP2010087784736.
  12. Durand, Yves; Guerring, Bernard. Front aircraft sealed bottom comprising recesses for housing cockpit equipment. USP2016069376200.
  13. Loupias, Thierry; Gouarderes, Patrick. Front part of an aircraft fuselage incorporating a bay for stowing landing gear. USP2014098840066.
  14. Lieven, Patrick; Chaumel, Pascal. Front structure of an aircraft fuselage comprising landing gear. USP2014098840063.
  15. Retz, Kevin M.; Voogt, Nicholaas; Friend, Michael G.; Holtorf, Christopher R.; Wallace, Mannon L.; Sones, Andrew. Integrated aircraft windshields and associated methods. USP2004116817571.
  16. De Ruffray, Paul; Morel, Rodolphe. Landing gear casing provided with a dissociated structure. USP2012128336819.
  17. Briancourt,Stephen P. Landing gear door assembly. USP2007107287726.
  18. Wood, Jeffrey H.. Landing gear system and load distribution. USP2010097798444.
  19. Gleyze, Gilbert. Method for adjusting the doors of a landing gear bay, and associated door. USP2015089096311.
  20. Thomas, Grant Brian; Dopker, Bernhard; Johnson, Robert Wayne. Pressure panels. USP2015129199713.
  21. Guering, Bernard. Storage compartment for the nose gear of an aircraft. USP2012028118259.