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Class Information
Number: 239/265.17
Name: Fluid sprinkling, spraying, and diffusing > Reaction motor discharge nozzle > With addition of secondary fluid upstream of outlet
Description: Apparatus comprising a means for delivering an auxiliary or secondary fluid into the main fluid stream at a point in the system prior to discharge through the distributor outlet.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7607306 |
Infrared suppressor apparatus and method |
Oct. 27, 2009 |
| 7607305 |
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Oct. 27, 2009 |
| 7509797 |
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Mar. 31, 2009 |
| 7506501 |
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Mar. 24, 2009 |
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Mar. 10, 2009 |
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Self powdered missile turbojet |
Nov. 11, 2008 |
| 7401682 |
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Jul. 22, 2008 |
| 7392651 |
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Jul. 1, 2008 |
| 7377099 |
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May. 27, 2008 |
| 7310939 |
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Dec. 25, 2007 |
| 7311175 |
Acoustic liner with bypass cooling |
Dec. 25, 2007 |
| 7296397 |
Ventilation system for a convergent divergent exhaust nozzle |
Nov. 20, 2007 |
| 7293401 |
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Nov. 13, 2007 |
| 7246481 |
Methods and apparatus for operating gas turbine engines |
Jul. 24, 2007 |
| 7111448 |
Jet nozzle mixer |
Sep. 26, 2006 |
| 7055329 |
Method and apparatus for noise attenuation for gas turbine engines using at least one synthetic jet actuator for injecting air |
Jun. 6, 2006 |
| 7043898 |
Combined exhaust duct and mixer for a gas turbine engine |
May. 16, 2006 |
| 7017332 |
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Mar. 28, 2006 |
| 6996973 |
Method of achieving jet separation of an un-separated flow in a divergent nozzle body of a rocket engine |
Feb. 14, 2006 |
| 6962044 |
Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle |
Nov. 8, 2005 |
| 6854260 |
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Feb. 15, 2005 |
| 6837038 |
Variable cycle boost propulsor |
Jan. 4, 2005 |
| 6804948 |
Lobe mixer for jet engine |
Oct. 19, 2004 |
| 6804947 |
Device for cooling the common nozzle of a turbojet pod |
Oct. 19, 2004 |
| 6792748 |
Cooling system for a gas turbine engine post-combustion jet nozzle |
Sep. 21, 2004 |
| 6786037 |
Segmented mixing device having chevrons for exhaust noise reduction in jet engines |
Sep. 7, 2004 |
| 6742721 |
Shock wave aerosolization method and apparatus |
Jun. 1, 2004 |
| 6640537 |
Aero-engine exhaust jet noise reduction assembly |
Nov. 4, 2003 |
| 6629416 |
Afterburning aerospike rocket nozzle |
Oct. 7, 2003 |
| 6612106 |
Segmented mixing device having chevrons for exhaust noise reduction in jet engines |
Sep. 2, 2003 |
| 6578355 |
Bloom mixer for a turbofan engine |
Jun. 17, 2003 |
| 6568171 |
Rocket vehicle thrust augmentation within divergent section of nozzle |
May. 27, 2003 |
| 6381950 |
Engine nozzle arrangement for an aircraft |
May. 7, 2002 |
| 6360528 |
Chevron exhaust nozzle for a gas turbine engine |
Mar. 26, 2002 |
| 6345935 |
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Feb. 12, 2002 |
| 6336319 |
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Jan. 8, 2002 |
| 6308898 |
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Oct. 30, 2001 |
| 6298658 |
Multi-stable thrust vectoring nozzle |
Oct. 9, 2001 |
| 6295805 |
Exhaust induced ejector nozzle system and method |
Oct. 2, 2001 |
| 6253540 |
Removable baffle infrared suppressor |
Jul. 3, 2001 |
| 6182440 |
Infrared radiation coanda suppressor |
Feb. 6, 2001 |
| 6179225 |
Turbo jet engine exhaust nozzle with masked gas jet |
Jan. 30, 2001 |
| 6178742 |
Rear mixer ejector for a turbomachine |
Jan. 30, 2001 |
| 6164059 |
Multi-expansion ejector nozzle with diverging walls |
Dec. 26, 2000 |
| 6148607 |
Thrust reverser with lock-status display |
Nov. 21, 2000 |
| 6134879 |
Suppression system for a gas turbine engine |
Oct. 24, 2000 |
| 6123170 |
Noise reducing connection assembly for aircraft turbine housings |
Sep. 26, 2000 |
| 6122907 |
IR suppressor |
Sep. 26, 2000 |
| 6112512 |
Method and apparatus of pulsed injection for improved nozzle flow control |
Sep. 5, 2000 |
| 6112513 |
Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow |
Sep. 5, 2000 |
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