Matches 51 - 86 out of 86 < 1 2
Match Document Document Title
3750402 MIXED FLOW AUGMENTATION SYSTEM  
1. In an axial flow reaction engine a mixed flow augmentation system comprising: A first plurality of motive fluid flow passages; A second plurality of motive fluid flow passages, the passages of...
3747345 SHORTENED AFTERBURNER CONSTRUCTION FOR TURBINE ENGINE  
An afterburner construction for a turbine engine, such as a turbofan engine, which is foreshortened by using a construction which utilizes swirl flow phenomena to rapidly mix the engine products of...
3648460 GAS TURBINE ENGINE FUEL CONTROL SYSTEM  
The invention concerns a gas turbine engine fuel control system comprising a first burner supply conduit and at least one second burner supply conduit, a fuel pump which communicates with both said...
3636712 LIQUID ROCKET ENGINE AND METHOD OF OPERATING SAME  
1. In a liquid propellant rocket engine including ante-combustion chamber means, main combustion chamber means, means for supplying fuel and oxidizer to the ante-combustion chamber means for...
3633362 REHEAT COMBUSTION APPARATUS FOR BYPASS GAS TURBINE ENGINES  
A reheat system for a bypass gas turbine jet propulsion engine comprises a device at the downstream end of the bypass duct which both mixes the bypass air with the hot gas stream and provides a...
3540216 TWO-FLOW GAS TURBINE JET ENGINE  
3528250 BYPASS ENGINE WITH AFTERBURNING AND COMPRESSOR BLEED AIR HEAT EXCHANGER IN BYPASS DUCT  
3514954 GAS TURBINE BY-PASS ENGINE  
3465525 GAS TURBINE BYPASS ENGINES  
3398538 Combustion apparatus  
3387457 Combined turbojet and turboprop engine  
3366373 Apparatus for adding heat to gas turbine exhaust  
3352112 Bleed control in mixing valve for a turbofan engine  
3330117 By-pass gas turbine jet engine  
3279186 Thrust variation and vectoring nozzle  
3150484 Gas turbine by-pass engine  
3128598 Afterburner fuel control  
3087301 Leading edge fuel manifold  
3054423 Close-open and diverter valve  
3043101 By-pass gas turbine engine employing reheat combustion  
3030769 Ramjet variable area exit nozzle  
2999672 Fluid mixing apparatus  
2987873 Method and apparatus for using ammonia to increase the air specific impulse of a two-stage compressor turbojet engine  
2979900 Ducted fan flameholder  
2978865 Turbo fan exhaust mixing device  
2978868 Concentric combustion system with cooled dividing partition  
2974478 Fluid flow energy transformer  
2974486 Afterburner mixture and flame control baffle  
2966141 Pneumatic displacement amplifier  
2946185 Fuel-air manifold for an afterburner  
2944388 Air atomizing spray bar  
2939275 Solid-fuel rocket type motor assemblies  
2929203 Afterburning bypass aviation turbojet engine  
2910828 Convergent-divergent variable area propulsion nozzle  
2834181 Jet propulsion unit comprising pulse jet units having ejector tubes within a ramjet unit  
2834183 Composite ramjet-pulsejet engine  
Matches 51 - 86 out of 86 < 1 2