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특허 상세정보

Aircraft with jet flap propulsion

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/16   
미국특허분류(USC) 244/013 ; 244/207 ; 244/215 ; 244/216 ; 244/045A
출원번호 US-0043712 (1998-03-23)
국제출원번호 PCT/IB95/00818 (1995-09-29)
§371/§102 date 19980323 (19980323)
국제공개번호 WO-9712804 (1997-04-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Jones & Askew
인용정보 피인용 횟수 : 14  인용 특허 : 2
초록

The airfoil profile has maximum thickness just forward of the control surface device (12) which has large included trailing edge angle and large leading edge radius. The control surface device hinge (17) is positioned close to the mean line (19) of the plane, and air slots (10) in the plane are blowing the control surface device.

대표
청구항

[ I claim:] [1.] Aircraft (1) with at least one engine (6) and at least one blower (5), air intakes (2) for the blower and at least one plane (18) with at least one control surface device (12) having surfaces including a top surface (20) and airduct means (9,10) from the blower to the plane for producing jet flap propulsion in combination with the control surface device, characterized ina) that the plane (18) has a profile with thickness increasing to the rear of the plane;b) that the control surface device (12) is hinged with a hinge (17) just aft of th...

이 특허를 인용한 특허 피인용횟수: 14

  1. Reckzeh, Daniel; Dyke, Adrian R.. Aircraft wing, method for operating an aircraft wing, and use of a pivotable trailing edge on a main wing of an aircraft, for adjusting the shape and width of an air gap. USP2009047520471.
  2. Phillips, Warren F.. Apparatus and method for reducing induced drag on aircraft and other vehicles. USP2005116970773.
  3. Phillips, Warren F.. Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles. USP2011027883060.
  4. Cordy, Jr.,Clifford B. Better balanced canard airplane with forward engine. USP2006107121503.
  5. Schwetzler, Detlev; May, Peter. Flap arrangement for varying the aerodynamic lift generated by an aerodynamic element of an aircraft. USP2003116641089.
  6. Becker, Juergen. Flight control device for improving the longitudinal stability of an automatically controlled airplane and method of operating same. USP2004056729579.
  7. Evulet, Andrei. Fluidic propulsive system and thrust and lift generator for aerial vehicles. USP20190210207812.
  8. Westra, Bryan Wayne; Sato, Roxanne Marie; Shultz, Douglas Ellwood; Kerswell, James Franklin; Petersen, Perry Bruce; Collins, Scott Walter. Flying wing aircraft. USP2012068191820.
  9. Westra, Bryan Wayne; Sato, Roxanne Marie; Shultz, Douglas Ellwood; Kerswell, James Franklin; Petersen, Perry Bruce; Collins, Scott Walter. Flying wing aircraft with modular missionized elements. USP2012108292220.
  10. Libby, John. High lift longitudinal axis control system. USP2010027661630.
  11. Libby,John. High lift longitudinal axis control system. USP2008057367532.
  12. Hirai, Makoto; Maeda, Ichiro. High-lift device, wing, and noise reduction structure for high-lift device. USP2013068469316.
  13. Hirai, Makoto; Maeda, Ichiro. High-lift device, wing, and noise reduction structure for high-lift device. USP2015049010692.
  14. Arata,Allen A.. Rechargeable compressed air system and method for supplemental aircraft thrust. USP2006097104499.