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특허 상세정보

Continuous moldline technology (CMT) elastomeric control surface

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/16   
미국특허분류(USC) 244/215; 244/213
출원번호 US-0451456 (2012-04-19)
등록번호 US-8814100 (2014-08-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ameh IP
인용정보 피인용 횟수 : 2  인용 특허 : 17
초록

A continuous moldline technology elastomeric control surface and methods are presented. A control surface is coupled to a fluid-dynamic body. An elastomer interface is coupled to the control surface and the fluid-dynamic body such that a joint gap caused by movement of the control surface relative to the fluid-dynamic body is filled.

대표
청구항

1. A continuous moldline technology elastomeric control surface, comprising: a first control surface coupled to a fluid-dynamic body; anda first elastomer interface comprising a continuous elastomer surface directly coupled to the first control surface and the fluid-dynamic body such that a first joint gap caused by movement of the first control surface relative to the fluid-dynamic body is filled, the continuous elastomer surface continuous from the fluid-dynamic body to the first control surface, wherein:the fluid-dynamic body comprises a wing, andthe ...

이 특허에 인용된 특허 (17)

  1. Kendall G. Young ; Steven L. Pauletti. Aerodynamic control surface system. USP2002106467733.
  2. Gruensfelder Cynthia Ann ; Geiger Micael Watson ; Jacobs Jack Howard ; Wille Robert Henry. Apparatus for eliminating gaps in an aircraft. USP1999115979828.
  3. Caton John Harold ; Hobey Michael James ; Groeneveld John David ; Jacobs Jack Howard ; Wille Robert Henry ; Brase ; Jr. Lawrence Otto. Control surface for an aircraft. USP2001046209824.
  4. Waldrop ; III John Cleveland,ESX. Elastic ground plane and method. USP2000046048581.
  5. Geiger Michael Watson. Environmental coating for an elastomer panel. USP1999095958803.
  6. Gruensfelder Cynthia Ann ; Wille Robert Henry. Expandable aircraft bay and method. USP1999115975463.
  7. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry. Expandable fuel cell. USP1999075927651.
  8. Cameron Dean Emory. Fairing for an expandable bay. USP1999095947417.
  9. Wille Robert Henry. Hinge line skin system for an aircraft. USP1999085941480.
  10. Geders Paul Francis ; Wille Robert Henry. Interface seal for an aircraft. USP2000076092764.
  11. Pitt, Dale M.; Eckstein, Nicholas Stephen. Moveable leading edge device for a wing. USP2013098534611.
  12. Cameron Dean Emory ; Geders Paul Francis ; Geiger Michael Watson ; Roberts Dennis Allan ; Wille Robert Henry. Reinforced elastomer panel. USP2000026027074.
  13. Dean Emory Cameron ; Paul Francis Geders ; Michael Watson Geiger ; Dennis Allan Roberts ; Robert Henry Wille. Reinforced elastomer panel. USP2002046375122.
  14. Wille Robert Henry. Tail for an aircraft. USP1999095947422.
  15. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA). Variable camber aircraft wing tip. USP1984024429844.
  16. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.
  17. Irving,Jan; Davies,Robert. Wing tip device. USP2007107275722.