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특허 상세정보

Staggered channel wing-type aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/06   
미국특허분류(USC) 244/13 ; 244/45R
출원번호 US-0393220 (1973-08-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 24  인용 특허 : 0
초록

Disclosed is a staggered channel wing-type aircraft comprising a reverse staggard lower and upper wing which relates to aircraft of the type generally described as a short takeoff and landing vehicle (STOL) and more particularly to an improved version thereof having superior low speed handling characteristics in both takeoff and landing and an economical high speed cruise configuration. Also having an improved gliding characteristic and easy storage because the wingspan is reduced to a minimum but keeping still rather large wing area.

대표
청구항

A staggered channel wing type aircraft comprising: a fuselage with a nose and a passenger section; a pusher type propulsion means mounted behind said passenger section, said fuselage being free of any tail structure; a lower pair of wings swept rearward from said fuselage; an upper pair of wings rigidly attached at the wing tips of said lower pair and swept back, inward and upward from said tips and secured together to form a triangular pyramid-like configuration with the upper wings being free from the fuselage and from vertical fins and both upper and ...

이 특허를 인용한 특허 피인용횟수: 24

  1. Breitsamter, Christian; Allen, Alexander. Aerodynamic element and wing with aerodynamic element, actuator-activation module, computer, computer program and method of influencing wake eddies. USP2013038387922.
  2. Adam ; Jr. George F. ; Knudsen John C. ; Shaw David ; Hatfield Daniel ; Rutan Burt. Aircraft. USP200108D446182.
  3. Wilding, Joe; Olcott, Dennis D.; Cole, Greg. Aircraft. USP200501D500981.
  4. Wilding, Joe; Olcott, Dennis D.; Cole, Greg. Aircraft. USP200501D500729.
  5. Cazals, Olivier; Genty de la Sagne, Jaime. Aircraft presenting two pairs of wings and fuel tanks in fluid communication. USP2013058439310.
  6. McGinnis, John William. Aircraft stability and efficient control through induced drag reduction. USP2017019545993.
  7. Peters ; Jr. Spence E.. Aircraft structure to improve directional stability. USP2000086098923.
  8. Zimmer ; Herbert. Airplane with two superposed wings. USP1978054090681.
  9. Rado,Kenneth S.. Amphibian delta wing jet aircraft. USP2006067063291.
  10. James R. Lohse ; James G. Hutton. Amphibious aircraft. USP2002046367737.
  11. Lohse James R. ; Hutton James G.. Amphibious aircraft. USP2000096113028.
  12. August, Henry. Arch wing and forward steering for an advanced air vehicle. USP2003126659396.
  13. Fink, Axel; Blacha, Martin. Compound rotorcraft. USP20181110131424.
  14. Hernadi, Andras. Decagonal box-wing aircraft. USP201904D844538.
  15. Hernadi, Andras. Decagonal boxed-wing for aircraft. USP201903D843920.
  16. McGinnis, John William. Efficient control and stall prevention in advanced configuration aircraft. USP2014028657226.
  17. Suokas, Aki. Flying device and a wing construction for the same. USP2016049308984.
  18. Brzack Jeffrey A. (140 Maumee Trail Lake Orion MI 48035). Glider. USP1981074280673.
  19. Brzack Jeffrey A. (140 Maumee Trail Lake Orion MI 48035). Glider. USP1982084345401.
  20. Garreau, Oliver F.. Joined-wing tilt-wing aircraft. USP201503D724001.
  21. Jerry E. Carlow. Mobius-like joining structure for fluid dynamic foils. USP2002116474604.
  22. Wenzel Harold A. (Phoeniz AZ). Multi-winged lifting body aircraft. USP1979034146199.
  23. August, Henry. Survivable and reusable launch vehicle. USP2004066749153.
  24. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.