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Reinforced elastomer panel

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-039/00   
미국특허분류(USC) 244/133; 244/123
출원번호 US-0294443 (1998-08-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Harness Dickey & Pierce P.L.C.
인용정보 피인용 횟수 : 7  인용 특허 : 17
초록

A reinforced elastomer panel (100) has a first rigid member (104) with an edge (116) attached to a first end of an elastomer panel (114). The first rigid member (104) has a removable plate (106) that provides access to a cavity (108). Attached to the first rigid member (104) is a reinforcing member (102) that extends through the elastomer panel (114). A second ridge member (118) has an edge attached to a second end of the elastomer panel (114).

대표
청구항

1. A reinforced elastomer plate, comprising:a structural body; a flexible rib having a first end inside the structural block; an elastomer panel encapsulating a portion of the flexible rib and attached to an edge of the structural block; a second structural block having an edge attached to the elastomer panel and having a sleeve extending into the second structural block.

이 특허에 인용된 특허 (17)

  1. Maclean Brian J. (Daniel WY) Carpenter Bernard F. (Littleton CO) Misra Mohan S. (Golden CO). Adaptive control surface using antagonistic shape memory alloy tendons. USP1997095662294.
  2. Gruensfelder Cynthia Ann ; Geiger Micael Watson ; Jacobs Jack Howard ; Wille Robert Henry. Apparatus for eliminating gaps in an aircraft. USP1999115979828.
  3. Burbridge Thomas Edward ; Tomko Harvey John ; Wille Robert Henry. Blade seal for an aircraft. USP1999065913494.
  4. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223. Continuous moldline technology system. USP1998095810291.
  5. Waldrop ; III John Cleveland,ESX. Elastic ground plane and method. USP2000046048581.
  6. Geiger Michael Watson. Environmental coating for an elastomer panel. USP1999095958803.
  7. Gruensfelder Cynthia Ann ; Wille Robert Henry. Expandable aircraft bay and method. USP1999115975463.
  8. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry. Expandable fuel cell. USP1999075927651.
  9. Cameron Dean Emory. Fairing for an expandable bay. USP1999095947417.
  10. Wille Robert Henry. Hinge line skin system for an aircraft. USP1999085941480.
  11. Covey James H. (Snohomish WA). Method for plating one side of a woven fabric sheet. USP1990014892626.
  12. Meyerhoefer Carl E.. Optical fiber strain relief system. USP1999045892877.
  13. Cameron Dean Emory ; Geders Paul Francis ; Geiger Michael Watson ; Roberts Dennis Allan ; Wille Robert Henry. Reinforced elastomer panel. USP2000026027074.
  14. Beier Theodor Harry ; Haake John Martin ; Wille Robert Henry ; Jacobs Jack Howard. Reinforced elastomer panel with embedded strain and pressure sensors. USP1999045896191.
  15. Wille Robert Henry. Tail for an aircraft. USP1999095947422.
  16. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA). Variable camber aircraft wing tip. USP1984024429844.
  17. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.

이 특허를 인용한 특허 피인용횟수: 7

  1. Geders, Paul F.. Continuous moldline technology (CMT) elastomeric control surface. USP2014088814100.
  2. Arata, Allen A.. Elastomeric transition. USP2018059975623.
  3. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2009087575195.
  4. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2005046877695.
  5. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2012028108980.
  6. Stephan, Andreas. Method for producing a composite skin in the field of aeronautics and astronautics. USP2016049314875.
  7. Etling, Keith A.. Morphing control surface transition. USP2013018342447.

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