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특허 상세정보

Combination lift thrust device

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-015/00   
미국특허분류(USC) 244/121 ; 244/209 ; 244/15 ; 244/55
출원번호 US-0757387 (1985-07-22)
발명자 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 1
초록

A combination lift and thrust device for increasing the performance of an aircraft by simultaneously reducing drag and augmenting the thrust of a turbojet engine carried within the device. The device comprises a wing of generally airfoil shape having numerous geometrically spaced apertures penetrating its surface, a turbojet engine carried within the wing, an elongated exhaust plenum attached to the turbojet having a number of strategically positioned exhaust nozzles, and a mixing chamber having a forward opening and a rear nozzle also carried within the...

대표
청구항

An improved combination lift and thrust device for use in aircraft application, comprising: (a) a wing of general airfoil shape for providing lift as the device is moved forwardly through the air, said wing including a forward opening and a membrane having a plurality of spaced apart apertures therethrough so constructed and arranged as to permit a flow of substantial amounts of air through said membrane; (b) a turbojet engine carried within said wing, said engine having an exhaust duct for the exhaustion of the gases of combustion from said engine and a...

이 특허를 인용한 특허 피인용횟수: 19

  1. Zhu, Xiaoyi. Aircraft generating a lift from an interior thereof. USP2013058448892.
  2. Zhu, Xiaoyi. Aircraft generating a lift from an interior thereof. USP2014128910903.
  3. Rolling, August J; Heiser, William H; Wisniewski, Charles F. Augmented propulsion system with boundary layer suction and wake blowing. USP2017039587585.
  4. Reissig, Mark A.. Ejector driven flow control for reducing velocity deficit profile downstream of an aerodynamic body. USP2014048690106.
  5. Gerber, Martin; Schrauf, Geza. Flow body, in particular for aircraft. USP2014048702042.
  6. Evulet, Andrei. Fluidic propulsive system and thrust and lift generator for aerial vehicles. USP20190210207812.
  7. Burns David Johnston,GB3. Flying craft and a thruster engine suitable for use in such a craft. USP1998115836542.
  8. Billman, Garrett M.; O'Neil, Patrick J.. Forebody vortex alleviation device. USP2003096612524.
  9. Ouellette,Richard P; Kutzmann,Aaron J; Cummings,Darold B. Horizontal augmented thrust system and method for creating augmented thrust. USP2006127150432.
  10. Anderson, Jack H.. Jet nozzle mixer. USP2005026854260.
  11. Anderson,Jack H. Jet nozzle mixer. USP2007087251927.
  12. Anderson,Jack H.. Jet nozzle mixer. USP2006097111448.
  13. Anderson,Jack H.. Jet nozzle mixer. USP2006037017331.
  14. Prat, Damien; Negulescu, Camil; Barrois, Frederic; Caruelle, Bastien. Streamlined profile reducing the speed deficit in its wake. USP2013128596574.
  15. Reckzeh, Daniel; Goelling, Burkhard; Lengers, Matthias. Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element. USP2016039272772.
  16. Howarth,Nicholas; Freeman,Christopher. Turbine engine arrangements. USP2007017165744.
  17. Willis Mark T. (San Diego CA). Venturi enhanced airfoil. USP1991055016837.
  18. Reckzeh, Daniel; Goelling, Burkhard; Lengers, Matthias. Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift. USP2016039278753.
  19. Wood, Norman. Wing leading edge venting. USP2016119487287.