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특허 상세정보

Hinge line skin system for an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/06    B64C-003/58   
미국특허분류(USC) 244/131 ; 244/123 ; 244/133 ; 244/213 ; 244/219
출원번호 US-0852870 (1997-05-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Halling
인용정보 피인용 횟수 : 20  인용 특허 : 5
초록

A hinge line system (52) for an aircraft has a structural block (22) attached to a first edge of a hinge line. The structural block (22) has a flange (28) attached to a first end of an elastic sheet (32). A second structural block (24) is attached to a second edge of the hinge line. The second structural block (24) has a second flange (30) attached to a second end of the elastic sheet (32).

대표
청구항

[ What is claimed is:] [1.] A hinge line sock system for an aircraft, comprising:a first stretchable knit fabric;a uniform elastomer skin having a top surface bonded to the stretchable knit fabric;a second stretchable knit fabric bonded to a bottom surface of the elastomer skin;a first rigid structural member attached to a first end of the elastomer skin, the first rigid structural member attached to a control surface of the aircraft and having a shear bonding area; anda second rigid structural member attached to a first end of the elastomer skin, attach...

이 특허를 인용한 특허 피인용횟수: 20

  1. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V.. Apparatus for variation of a wall skin. USP2003076588709.
  2. Glovatsky, Andrew Zachary; Belke, Robert Edward; Baker, Jay DeAvis; Giachino, Joseph Mario; Goenka, Lakhi Nandlal; Lemecha, Myron. Braking assembly and system. USP2003126655504.
  3. Stewart, David Mark. Bridging seal. USP2014118876051.
  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. Geders, Paul F.. Continuous moldline technology (CMT) elastomeric control surface. USP2014088814100.
  7. 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.
  8. Mindermann, Marco; Schwill, Thomas. Covering device for a hinge of an aircraft. USP2010047694915.
  9. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2009087575195.
  10. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2005046877695.
  11. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2012028108980.
  12. Gruensfelder Cynthia Ann ; Brase ; Jr. Lawrence O.. Leading edge for an aircraft. USP2001046213433.
  13. Etling, Keith A.. Morphing control surface transition. USP2013018342447.
  14. Dean Emory Cameron ; Paul Francis Geders ; Michael Watson Geiger ; Dennis Allan Roberts ; Robert Henry Wille. Reinforced elastomer panel. USP2002046375122.
  15. Wilson, James; West, Colin John; Sutton, David Alistair; Hadley, Paul. Seal. USP2016069365283.
  16. Beiermann, Brett A.; Keller, Michael W.; White, Scott R.; Sottos, Nancy R.. Self-healing laminate system. USP2016089415575.
  17. Wigley, Alexander T.. Shape shifting foils. USP2018049944356.
  18. Da Rocha-Schmidt, Luiz. Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts. USP20181210150557.
  19. McCallum, Brent N.; Young, Kendall G.. Subdermally-reinforced elastomeric transitions. USP2003066575407.
  20. Ambrose,David R.. Unitized rotary actuator hinge fitting. USP2007067229049.