INJECTOR WITH TANGENTIAL FEED CONDUITS FOR HYDROGEN-DRIVEN GAS TURBINE ENGINE

Air turbine starter with shaped vanes

Cartridge tip for turbomachine combustor

Air turbine starter with shaped vanes

Device for ventilation of a turbomachine turbine casing

Airflow straightening assembly having improved aerodynamic performances

Method and system for modulated turbine cooling

Gas turbine engine with high speed and temperature spool cooling system

Gas turbine engine component with conformal fillet cooling path

Apparatus for mounting a component in a gas turbine engine

Airfoil cooling apparatus

Root lightening holes with slot

Air exhaust tube holder in a turbomachine

Turbine blade

Combustor transition duct assembly with inner liner

Cooled turbine blades for a gas-turbine engine

Turbofan mounting arrangement

Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine

Assembly for directing combustion gas

Axial turbine

Modular transvane assembly

Turbine seal assembly

Canted outlet for transition in a gas turbine engine

MULTI-TUBE, CAN-ANNULAR PULSE DETONATION COMBUSTOR BASED ENGINE WITH TANGENTIALLY AND LONGITUDINALLY ANGLED PULSE DETONATION COMBUSTORS

Rocket engine nozzle system

Axial turbine

Out-flow margin protection for a gas turbine engine

Axial turbine

Combustion transition duct providing stage 1 tangential turning for turbine engines

Support system for transition ducts

Blade and disk radial pre-swirlers

Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine

Coverplate deflectors for redirecting a fluid flow

Axial turbine

Gas turbine gas path contour

Exhaust turbocharger