AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

Gas Turbine Engine with Third Stream

Gas Turbine Engine with Third Stream

Gas Turbine Engine with Third Stream

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES

GAS TURBINE ENGINE

AIRCRAFT PROPULSION SYSTEM WITH ASYMMETRIC EXHAUST ASSEMBLY

SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR

AIR RECUPERATED ENGINE WITH AIR REINJECTION

TURBOSHAFT ENGINE

PROPULSION ASSEMBLY FOR AN AIRCRAFT

Air recuperated engine with air reinjection

Combustion system

System and method for mitigating bowed rotor in a gas turbine engine

THREE-STREAM GAS TURBINE ENGINE CONTROL

Ambient air environmental control system

Turboshaft engine

Charge Air Cooler Bypass Systems and Methods

Non-axisymmetric secondary duct portion

Turbofan engine comprising a system for blocking the flow path of the bypass stream comprising veils

FLUID FLOW GUIDING DEVICE AND A GAS TURBINE ENGINE

Power withdrawal from a LP body and system for removing debris

Turbofan engine comprising a set of rotatable blades for blocking off the bypass flow duct

Cooling method for a high-temperature radial gas turbine engine

Gas turbine engine with inertial particle separator

Synergistic hybrid propulsion

Compressor apparatus with bleed slot and supplemental flange

Airbreathing engine module with reverse flow arrangement

Turbine engine structure with oxidizer enhanced mode

Three actuator cascade type thrust reverser actuation system

Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve system

Gas turbine engine with compressor bleed valve including at least two open positions

Gas turbine engine power setting

Auxiliary device for three air flow path gas turbine engine

Translating outer cowl flow modulation device and method

Multi-bypass stream gas turbine engine with enlarged bypass flow area

Gas turbine engine with inertial particle separator

Closed cycle heat engine for a gas turbine engine

Three actuator cascade type thrust reverser actuation system

Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines

Compressor apparatus with bleed slot and supplemental flange

Exhaust nozzle control including tapered control effector for a gas turbine engine

Engine for hypersonic aircrafts with supersonic combustor

Deicing nose of an axial turbine engine compressor

Air bypass system for rotor shaft cooling

Harmonic drive for shaft driving multiple stages of vanes via gears

Air intake for turboprop engine

Method and system for modulated turbine cooling as a function of engine health

Method and system for improving structural characteristics of composite component corners

Oil transfer assembly for supplying oil into a rotating and translating tube

Device for fixing blades with variable pitch of a non-streamlined turbomachine propeller

Coanda device for a round exhaust nozzle

Cooled cooling air system for a turbofan engine

Rolling element cage for geared turbofan

Journal bearing for rotating gear carrier

Lubricant delivery system for planetary fan drive gear system

Exhaust nozzle control for a gas turbine engine

HIGH-CYCLE, SHORT RANGE-OF-MOTION LINKAGE APPARATUS FOR GAS TURBINE ENGINE APPLICATIONS

Method to integrate multiple electric circuits into organic matrix composite

Gas turbine engine and an airflow control system

Fan by-pass duct for intercooled turbo fan engines

Air inlet arrangement and method of making the same

GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE TO REDUCE FAN INSTABILITY

Gas turbine engine including a third flowpath exhaust nozzle

Airflow modulation system and method

Flow path routing within a gas turbine engine

Two spool gas generator with improved air porting

Bleed air systems for use with aircraft and related methods

Bleed air systems for use with aircraft and related methods

Auxiliary device for three air flow path gas turbine engine

Multi-bypass stream gas turbine engine with enlarged bypass flow area

Aircraft nozzle with a variable nozzle area of a second flow path

Pivoting blocker door

Translating outer cowl flow modulation device and method

Gas turbine engine with high speed low pressure turbine section

Bleed duct assembly for a gas turbine engine

Gas turbine engine

Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines

Thermal Management for Gas Turbine Engine

System and method for expanding a compressor bleed flow

Turbomachine with bleed valves located at the intermediate case

GEARED TURBOFAN WITH THREE TURBINES WITH HIGH SPEED FAN DRIVE TURBINE

Air-cooled oil cooler for turbofan engine

Aircraft, propulsion system, and inlet with supersonic compression

Aircraft airflow modulation system and method

Gas turbine engine with fan variable area nozzle to reduce fan instability

Nozzle arrangement and method of making the same

Thrust reverser translating sleeve assembly

Air inlet arrangement and method of making the same

Mechanism for turbine engine start from low spool

Mass flow increase at takeoff in supersonic airliner

Load limited actuator

Turbine based combined cycle engine

Movable actuator device for controlling the pitch of fan blades of a turboprop

Device for controlling the pitch of fan blades of a turboprop

Bleed outlet structure for a bleed valve

Method and device to increase thrust and efficiency of jet engine

Jet nozzle mixer

Bypass duct of a turbofan engine

COOLING DEVICE FOR AIRCRAFT PROPELLER

Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines

Aircraft engine inlet having zone of deformation

Exhaust for a gas turbine engine

POWER EXTRACTION METHOD

Integration of a surface heat exchanger to the wall of an aerodynamic flowpath by a structure of reinforcement rods

Airflow modulation for dual mode combined cycle propulsion systems

Non-handed thrust reverser for installation on handed aircraft gas turbine propulsion engines

Active tip clearance control arrangement for gas turbine engine

Thermal protection of rotor blades

TURBO FAN ENGINE

Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle

Inlet particle separator system for a gas turbine engine

Variable slope exhaust nozzle

Thrust reverser for a turbofan gas turbine engine

Method and device to increase thrust and efficiency of jet engine

Methods and systems for supplying air to a vehicle

Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed

Tip turbine engine comprising a nonrotable compartment

Aircraft engine inlet having zone of deformation

Attachment unit of driving shaft with tensioner nut

Jet nozzle mixer

Universal Carnot propulsion systems for turbo rocketry

Internal duct VTOL aircraft propulsion system

Jet nozzle mixer

Jet nozzle mixer

Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system

Airbreathing propulsion engines including rotating detonation and bluff body systems

Gas turbine engine with integral bypass duct

Supplemental thrust system with rotating detonation combustor

Gas turbine engine with axial flow fan with twin stream impeller and variable area bypass nozzle

Variable bypass turbofan engine