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Class Information
Number: 60/231
Name: Power plants > Reaction motor (e.g., motive fluid generator and reaction nozzle, etc.) > With thrust direction modifying means > Jet stream deflecting means > By secondary fluid injection
Description: Apparatus having means whereby a fluid is injected into the motive fluid stream to change the direction of flow of said motive fluid.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7533517 |
Exhaust nozzle for an engine of a flying craft |
May. 19, 2009 |
| 7293401 |
Jet engine noise suppressor |
Nov. 13, 2007 |
| 7234302 |
Housing for a turbocharger |
Jun. 26, 2007 |
| 6996973 |
Method of achieving jet separation of an un-separated flow in a divergent nozzle body of a rocket engine |
Feb. 14, 2006 |
| 6983587 |
Method and apparatus for thrust augmentation for rocket nozzles |
Jan. 10, 2006 |
| 6962044 |
Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle |
Nov. 8, 2005 |
| 6758032 |
System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans |
Jul. 6, 2004 |
| 6701705 |
Gas-walled rocket nozzle |
Mar. 9, 2004 |
| 6679048 |
Apparatus and method for controlling primary fluid flow using secondary fluid flow injection |
Jan. 20, 2004 |
| 6470669 |
Hybrid injection thrust vector control |
Oct. 29, 2002 |
| 6354074 |
Hybrid injection thrust vector control |
Mar. 12, 2002 |
| 6298658 |
Multi-stable thrust vectoring nozzle |
Oct. 9, 2001 |
| 6179251 |
Thin inlet lip design for low drag and reduced nacelle size |
Jan. 30, 2001 |
| 6125627 |
Method and apparatus for spraying fuel within a gas turbine engine |
Oct. 3, 2000 |
| 6112513 |
Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow |
Sep. 5, 2000 |
| 6112512 |
Method and apparatus of pulsed injection for improved nozzle flow control |
Sep. 5, 2000 |
| 6055804 |
Turning vane arrangement for IR suppressors |
May. 2, 2000 |
| 5727381 |
Duct flow control system |
Mar. 17, 1998 |
| 5706650 |
Vectoring nozzle using injected high pressure air |
Jan. 13, 1998 |
| 5694766 |
Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine engine exhaust nozzle using regions of locally separated flow |
Dec. 9, 1997 |
| 5664415 |
After-burning turbo-fan engine with a fixed geometry exhaust nozzle having a variable flow coefficient |
Sep. 9, 1997 |
| 5435489 |
Engine exhaust gas deflection system |
Jul. 25, 1995 |
| 5072891 |
Combination actuator and coolant supply for missile and rocket vector control |
Dec. 17, 1991 |
| 4902254 |
Propulsion device with conditioned inertia |
Feb. 20, 1990 |
| 4686824 |
Gaseous secondary injection thrust vector control device |
Aug. 18, 1987 |
| 4424670 |
Device for piloting the propulsion system of a solid propellant rocket |
Jan. 10, 1984 |
| 4411630 |
Water-jet drive mechanism for the driving of watercraft |
Oct. 25, 1983 |
| 4384694 |
Rocket attitude control apparatus |
May. 24, 1983 |
| 4351479 |
Jet engine with a thrust vector control |
Sep. 28, 1982 |
| 4118930 |
Filter-cooler |
Oct. 10, 1978 |
| 4077572 |
Reduced size altitude insensitive thrust vector control nozzle |
Mar. 7, 1978 |
| 4063685 |
Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle |
Dec. 20, 1977 |
| 4047381 |
Gas turbine engine power plants for aircraft |
Sep. 13, 1977 |
| 4003531 |
Reverse flow reaction control system |
Jan. 18, 1977 |
| 3995662 |
Fluidic switches |
Dec. 7, 1976 |
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