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특허 상세정보

Elastomeric transition

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/06    B64C-009/02   
출원번호 US-0064366 (2016-03-08)
등록번호 US-9975623 (2018-05-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Tarolli, Sundheim, Covell & Tummino LLP
인용정보 피인용 횟수 : 0  인용 특허 : 21
초록

An elastomeric transition for spanning a gap between first and second surfaces on an aircraft includes an elastomeric skin. A first skin edge is configured for attachment to the first surface and a second skin edge is configured for attachment to the second surface. The elastomeric skin has a longitudinal dimension, coincident with the gap, which is significantly longer than a distance between laterally corresponding points on the first and second skin edges. At least one continuous rod is coupled at one end to a selected first point on the first surface...

대표
청구항

1. An elastomeric transition for spanning a gap between first and second surfaces on an aircraft, the elastomeric transition comprising: an elastomeric skin, a first edge of the skin attached to the first surface and a second edge of the skin attached to the second surface, the elastomeric skin having a longitudinal dimension, coincident with the gap, which is longer than a distance between laterally corresponding points on the first and second edges of the skin; andat least one continuous rod coupled at one end to a selected first point on the first sur...

이 특허에 인용된 특허 (21)

  1. Geiger Michael Watson ; Gruensfelder Cynthia Ann ; Jacobs Jack Howard. Active reinforced elastomer system. USP1999085931422.
  2. Kendall G. Young ; Steven L. Pauletti. Aerodynamic control surface system. USP2002106467733.
  3. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V.. Apparatus for variation of a wall skin. USP2003076588709.
  4. Geders, Paul F.. Continuous moldline technology (CMT) elastomeric control surface. USP2014088814100.
  5. 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.
  6. John Harold Caton ; Michael James Hobey ; John David Groeneveld ; Jack Howard Jacobs ; Robert Henry Wille ; Lawrence Otto. Brase, Jr.. Control surface for an aircraft. USP2002026349903.
  7. John Cleveland Waldrop, III ES. Elastic ground plane. USP2002016337294.
  8. Waldrop ; III John Cleveland,ESX. Elastic ground plane and method. USP2000046048581.
  9. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP2000116145791.
  10. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  11. Geiger Michael Watson. Environmental coating for an elastomer panel. USP1999095958803.
  12. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry. Expandable fuel cell. USP1999075927651.
  13. Charron,Richard. Flexible airfoils and method. USP2006037007889.
  14. Gruensfelder Cynthia Ann. Folding wing for an aircraft. USP2000066076766.
  15. Greenhalgh Samuel (Doylestown PA). Lift enhancement device. USP1994085335886.
  16. Cameron Dean Emory ; Geders Paul Francis ; Geiger Michael Watson ; Roberts Dennis Allan ; Wille Robert Henry. Reinforced elastomer panel. USP2000026027074.
  17. Dean Emory Cameron ; Paul Francis Geders ; Michael Watson Geiger ; Dennis Allan Roberts ; Robert Henry Wille. Reinforced elastomer panel. USP2002046375122.
  18. Madsen, Casey Lyn. Shape memory alloy rods for actuation of continuous surfaces. USP2015119174723.
  19. Arata Allen A.. Single surface multi axis aircraft control. USP2000056068219.
  20. McCallum, Brent N.; Young, Kendall G.. Subdermally-reinforced elastomeric transitions. USP2003066575407.
  21. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.