$\require{mediawiki-texvc}$
  • 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

Umbrella seal for aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/12   
미국특허분류(USC) 244/132 ; 244/121 ; 244/123
출원번호 US-0475060 (1990-02-05)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 0
초록

An improved seal assembly positionable to cover a gap between aircraft panels. The seal assembly includes an umbrella seal and primary nodes extending therefrom into the gap. The seal assembly also includes secondary nodes in the gaps secured with respect to the panels and positioned between the primary nodes. The primary and secondary nodes having apertures aligned along a common axis. An elongated pin extends through the apertures of the primary and secondary nodes. The assembly further includes a cross seal positionable with its ends secured over ends...

대표
청구항

A seal assembly positionable to cover a gap between aircraft panels, the seal assembly including an umbrella seal of length and width to cover the gap and contact the exterior faces of associated aircraft panels and primary nodes extending therefrom into the gap, the seal assembly also including secondary nodes in the gaps secured with respect to the panels and positioned between the primary nodes, the primary and secondary nodes having apertures aligned along a common axis and an elongated pin removably extending through the apertures of the primary and...

이 특허를 인용한 특허 피인용횟수: 14

  1. Wille Robert Henry. Aircraft hinge. USP2001086276026.
  2. McBroom, Geoffrey Peter. Aircraft wing. USP2013128602355.
  3. Ambite Iglesias,Juan Carlos; Martin Prieto,Fernando; Calero Gallardo,Miguel Angel; Cala Romero,Antonio. Elastic pre-deformed fairings for aircrafts. USP2009037510144.
  4. Nolte, Bert. Envelope with an adhesive closure and method and device for producing the same. USP2004056732494.
  5. Delort, Pierre. Method of forming a panel assembly of a ventral fairing of an aircraft. USP2013108544176.
  6. Fisher, David; Abbas, Raja S.; Robbens, John S.; Wood, Stan. Method of sealing a panel to an aircraft structure. USP2005076915987.
  7. Sarh, Branko; Oberoi, Harinder Singh; Blanch, Alfredo Jose Gerosa; Barrick, Kevin Marion; Holden, Ray Lanier. Positioning system for electromagnetic riveting. USP2017059656319.
  8. Martín Hernández, Agustin Mariano. Reinforced cover for cut-outs in an aerodynamic contour. USP2010107815147.
  9. Martín Hernández, Agustín Mariano. Reinforced cover for gaps in an aerodynamic contour. USP2010037669800.
  10. Harris, Todd M.; Swanstrom, Frederick Marvin; Miller, Melinda Dae; Blanch, Jeffrey David. Ribbed caul plate for attaching a strip to a panel structure and method for use. USP2017119821538.
  11. Digmann, Charles J.; Droullard, Jack T.; Schmidt, Timothy J.. Seal for dock leveler lip hinge. USP2015028943630.
  12. Schulz, Alexander. Seal for sealing a component opening in a component. USP2009077556220.
  13. Parikh, Pradip Girish; Koppelman, Henry John; Harris, Todd Matthew; Swanstrom, Frederick M.. Skin panel joint for improved airflow. USP2012108282042.
  14. Parikh, Pradip Girish; Koppelman, Henry John; Harris, Todd Matthew; Swanstrom, Frederick M.. Skin panel joint for improved airflow. USP2013038393578.