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특허 상세정보

Tail for an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/14    B64C-003/50    B64C-009/00   
미국특허분류(USC) 244/219 ; 244/214 ; 244/215 ; 244/087
출원번호 US-0841732 (1997-04-29)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Halling
인용정보 피인용 횟수 : 31  인용 특허 : 8
초록

A tail (14) for an aircraft (10) has a center member (20) pivotally attached to the aircraft (10). A leading edge flap (22) extends along a length of the center member (20). An elastomeric skin (30) is connected between an exterior surface (26) of the center member (20) and an adjacent exterior surface (28) of the leading edge flap (22).

대표
청구항

[ What is claimed is:] [1.] A tail for an aircraft, comprising:a center member pivotally attached to the aircraft;a leading edge flap extending along a length of the center member and having a single pivot;a trailing edge flap extending along a length of the center member and having a single pivot;a worm drive that actuates the leading edge flap and the trailing edge flap simultaneously; anda reinforced elastomeric panel connected between an exterior surface of the center member and an adjacent exterior surface of the leading edge flap, the reinforced el...

이 특허를 인용한 특허 피인용횟수: 31

  1. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V.. Apparatus for variation of a wall skin. USP2003076588709.
  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. 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. John Cleveland Waldrop, III ES. Elastic ground plane. USP2002016337294.
  9. Gruensfelder Cynthia Ann. Folding wing for an aircraft. USP2000066076766.
  10. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2009087575195.
  11. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2005046877695.
  12. Eveker, James V.; Young, Roger K.. Hinge cover integration into door seal edges. USP2012028108980.
  13. Geders Paul Francis ; Wille Robert Henry. Interface seal for an aircraft. USP2000076092764.
  14. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  15. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  16. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  17. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  18. Gruensfelder Cynthia Ann ; Brase ; Jr. Lawrence O.. Leading edge for an aircraft. USP2001046213433.
  19. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  20. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  21. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  22. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  23. Gruensfelder Cynthia Ann ; Wille Robert Henry. Mission adaptive inlet. USP2000076089505.
  24. Gruensfelder Cynthia Ann ; Wille Robert Henry. Mission adaptive inlet. USP2001076260567.
  25. Dean Emory Cameron ; Paul Francis Geders ; Michael Watson Geiger ; Dennis Allan Roberts ; Robert Henry Wille. Reinforced elastomer panel. USP2002046375122.
  26. Wilson, James; West, Colin John; Sutton, David Alistair; Hadley, Paul. Seal. USP2016069365283.
  27. Wigley, Alexander T.. Shape shifting foils. USP2018049944356.
  28. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  29. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  30. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  31. Underwood Fred R. ; Scholtz Richard ; Claxton Ray J.. Vane actuator. USP2001096289787.