REHEAT ASSEMBLY FOR A GAS TURBINE ENGINE

ENTRAINMENT COMPRESSION SYSTEM FOR JET ENGINE

Afterburner strut with integrated fuel feed lines

Turbine engine structure with oxidizer enhanced mode

HIGH SPEED PROPULSION SYSTEM WITH INLET COOLING

Auxiliary device for three air flow path gas turbine engine

Gas turbine engine architecture with nested concentric combustor

Aerospace turbofan engines

REVERSE-FLOW CORE GAS TURBINE ENGINE WITH A PULSE DETONATION SYSTEM

High compressor build clearance reduction

Gas turbine engine including a re-heat combustor and a shaft power transfer arrangement for transferring power between low and high pressure shafts

GAS TURBINE ENGINE

Control scheme using variable area turbine and exhaust nozzle to reduce drag

Reverse-flow core gas turbine engine with a pulse detonation system

High speed propulsion system with inlet cooling

Gas turbine engine with reverse-flow core having a bypass flow splitter

Pre-turbine engine case variable area mixing plane

GAS TURBINE ENGINE AND METHOD OF OPERATING THEREOF

Afterburner chamber for a turbomachine

Duct burning mixed flow turbofan and method of operation

Segmented trapped vortex cavity

Fixed nozzle thrust augmentation system

Dual mode turbo engine

Combustion device

Device for fastening a fluid duct to a turbojet casing

Turbo-jet engine with a protective screen of the fuel manifold of a burner ring, the burner ring and the protective screen

Methods and apparatus for generating gas turbine engine thrust using a pulse detonator

Device for feeding air and fuel to a burner ring in an after-burner chamber

Variably angled propulsion/steering system

Rotating detonation augmentors with adjustable throats for gas turbine engines

Processing vapor exhausted by thermal management systems