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Conformable weapons platform

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/30   
미국특허분류(USC) 244/129.5 ; 244/129.4 ; 244/118.1 ; 244/119 ; 89/011 ; 89/015.1
출원번호 US-0885255 (1997-06-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Halling
인용정보 피인용 횟수 : 11  인용 특허 : 8
초록

A conformable weapons platform (52) has a cavity (60) in a skin of an aircraft. A weapon launching system (62) is contained in the cavity (60). A pair of elastomer doors (56, 58) are attached to a perimeter of the cavity.

대표
청구항

[ What is claimed is:] [1.] A conformable weapons platform comprising:a cavity in a skin of an aircraft;a weapon launching system contained in the cavity; anda pair of elastomer doors attached to a perimeter of the cavity and having a closed position that conforms to the moldline of the aircraft and a weapons loaded position wherein the pair of elastomer doors cover a portion of a weapon.

이 특허에 인용된 특허 (8)

  1. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  2. Ellis James R. ; Diller Joseph B.. Expandable aircraft section. USP1998095803405.
  3. Hardy Richard (Seattle WA) Neumann Frank D. (Bellevue WA) Ruzicka Dennis E. (Enumclaw WA). Fighter aircraft having low aerodynamic drag and low radar signature configuration. USP1996065522566.
  4. Jensen Duane Lowell. Inflatable conformable fuel tank. USP1998125845879.
  5. Klestadt Ralph H. (Sherman Oaks CA) Finn Richard R. (Palmdale CA). Multiple missile ejection system. USP1994085333528.
  6. Pinson George T. (Huntsville AL). Resiliently deployable fairing for sealing an airframe cavity. USP1989064838502.
  7. August Henry (Chatsworth CA). Technique and apparatus for rearward launch of a missile. USP1994015279199.
  8. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.

이 특허를 인용한 특허 피인용횟수: 11

  1. Gerard, Ludovic; Gutiérrez García, Alejandro; Maldonado, Julián. Aircraft landing gear. USP2016029248905.
  2. Gruensfelder Cynthia Ann. Auxiliary inlet for a jet engine. USP2000066079667.
  3. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Braking assembly and system. USP2003126655504.
  4. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Concealed air vents. USP2003066571820.
  5. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Container holder that utilizes moldline structures. USP2003046547117.
  6. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2009087575195.
  7. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2005046877695.
  8. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2012028108980.
  9. Geders Paul Francis ; Wille Robert Henry. Interface seal for an aircraft. USP2000076092764.
  10. Conway, Jr., George Louis; Young, Kendall G.; Stroud, Ron L.. Single aperture conformal aircraft bays. USP2003036536711.
  11. McCallum, Brent N.; Young, Kendall G.. Subdermally-reinforced elastomeric transitions. USP2003066575407.

IPC 상위 출원인