157488 ⎘
Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow; Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative position; adjustable, e.g. self-adjusting
SYSTEM AND METHOD HAVING ISOTHERMAL COMBUSTION ALONG SET OF TURBINE BLADES VIA VARYING FLUID INJECTION ALONG SET OF TURBINE VANES
#2Adjustable gaseous fuel injector
#3Dual-mode ramjet engine with variable fuel injection
#4System and method having flame stabilizers for isothermal expansion in turbine stage of gas turbine engine
#5SYSTEM AND METHOD HAVING FLAME STABILIZERS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE
#6Self-adapting gas turbine firebox with variable geometry
#7Jet engine, flying object, and operation method of jet engine
#8Variable geometry thruster
#9COMBUSTION CHAMBER
#10HELMHOLTZ DAMPER FOR A GAS TURBINE AND GAS TURBINE WITH SUCH HELMHOLTZ DAMPER
#11Jet engine, flying object and method of operating jet engine
#12Annular combustion chamber in a turbine engine
#13Jet engine, flying object, and method of operating jet engine
#14Fuel injection device for gas turbine
#15Pivoting stowable spray bar
#16Multi-stage combustor with a linear actuator controlling a variable air bypass
#17Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
#18Compact swirl augmented afterburners for gas turbine engines
#19Compact lightweight ramjet engines incorporating swirl augmented combustion with improved performance
#20Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
#21Adjustable gaseous fuel injector
#22System and method having flame stabilizers for isothermal expansion in turbine stage of gas turbine engine