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