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특허 상세정보

Span loaded flying wing control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/20    B64C-009/32    B64C-009/00   
미국특허분류(USC) 244/90A ; 244/113 ; 244/87 ; 244/215
출원번호 US-0211517 (1980-12-01)
발명자 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 1
초록

A flying wing aircraft control for angle of attack and direction thereof, comprising retractile controlling surfaces rearward of the center of lift and along the trailing edges and extensible over the top and bottom cambers of the wing in spaced relation to the trailing portions thereof and with variable angular dispositions with respect to air flow over the cambers so as to establish the desired moment arm with respect to the lift center of the flying wing to control the same into and out of a nose-up attitude with respect to the line of flight and with...

대표
청구항

A flying wing aircraft control for inducing angle of attack and controlling the line of flight, and including; a wing having upper and lower cambered surfaces and a center of lift substantially forward of a trailing edge establishing a moment arm therebetween, upper and lower trailing edge pitch control surfaces aft of the center of lift and retractile substantially coincidental with the upper and lower cambered surfaces of the wing, lever means to space said upper and lower pitch control surfaces into the air stream above and below said upper and lower ...

이 특허를 인용한 특허 피인용횟수: 21

  1. Jennifer Phillips Whitlock ; Blaine K. Rawdon ; Sean R. Wakayama. AFT egress and control device for an aircraft. USP2002056382562.
  2. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torisionally flexible wing. USP2015099120555.
  3. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torsionally flexible wing. USP2017099764819.
  4. Oyama, Hiroki. Aerodynamic braking device for aircraft. USP2012078231079.
  5. Cazals, Olivier; Druot, Thierry. Aerodynamic flight control surface said of crocodile style for aircraft. USP2013128613409.
  6. Omeara, Sean C.; Geppert, Brian E.; Konings, Christopher Andrew; Amorosi, Stephen Roger; Vijgen, Paul M.; Johnsen, Kevin Mark; Santini, Gregory M.. Aerodynamic structures having lower surface spoilers. USP20181210144502.
  7. Okabe, Yoshinori; Ishihara, Kenya; Sugawara, Zenta. Aircraft. USP20180710017240.
  8. Cox, Earl C.; Swanson, Kyle D.. Aircraft control method. USP2005086931247.
  9. Kendall, Greg T.; Morgan, Walter R.. Aircraft control system. USP2010097802756.
  10. Lisoski,Derek L.; Kendall,Greg T.. Aircraft control system. USP2007047198225.
  11. Shental,Gad; Shental,Nir; Shental,Ran; Pessachis,Lev. Aircraft wing structure and a method for decreasing flight speed of the aircraft. USP2007127311288.
  12. Clark, Walter Dennis. Aircraft with forward opening inlay spoilers for yaw control. USP2005056892982.
  13. Cazals, Olivier; Druot, Thierry. Aircraft with yaw control by differential drag. USP2014118876044.
  14. Saiz Manuel Munoz,ESX. Automatic flap. USP1999045895015.
  15. Bushnell, Glenn S.. Deployable aerodynamic devices with reduced actuator loads. USP2014028646729.
  16. Mahmoudi, Amirhossein; Alizadeh Salimi, Firouz. Flap device. USP2011027891612.
  17. Weston Paul H.. High efficiency combination wing aircraft. USP2001076264136.
  18. Funck, Stephen H.. Multi wing aircraft. USP2012108282036.
  19. Jacobson Clayton. Surface effect craft. USP2000016014940.
  20. Fevergeon, Matthew D M; Kordel, Jan A.. Trailing edge device with bell crank mechanism. USP2017129840320.
  21. William Blake. Wing mounted aircraft yaw control device. USP2002126491261.