System and method for reconfiguring a bleed system

THRUST REVERSER FOR TURBOFAN PROPULSION SYSTEM OF AN AIRCRAFT AND THRUST REVERSAL METHOD

Gas turbine compressor radial door bleed valve

Turbofan comprising a system comprising a screen for closing off the bypass duct

Divided volute turbocharger having vane ring with plurality of vanes having asymmetric vane pattern and system including the same

Wastegate for turbine

Self retained linkage and system including the self retained linkage for a gas turbine engine

Thrust reverser for an aircraft engine nacelle, comprising a panel for avoiding a movable slat of the wing, and nacelle associated therewith

Fan drive gear system mechanical controller

Variable diffuser having a respective penny for each vane

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

Two-dimensional supersonic nozzle thrust vectoring using staggered ramps

Dual function air diverter and variable area fan nozzle

Discourager for discouraging flow through flow path gaps

Oil tank mount arrangement on a geared turbofan engine

Rotary adjustable orifice plate valve

Aero loading shroud sealing

Variable vane apparatus

Particle separator

Gas turbine engine dual sealing cylindrical variable bleed valve

Solid propellant rocket motor

CHEVRON NOZZLE

Propulsive force vectoring

Belly band seal with anti-rotation structure

Fan drive gear system mechanical controller

Gas turbine engine accessory architecture

Turboprop engine with compressor turbine shroud

Oil tank mount arrangement on a geared turbofan engine

Particle separating fluid intake

Gas turbine engine having section with thermally isolated area

Gas turbine engine and blocker door assembly

Hub of an intermediate casing for an aircraft turbojet engine comprising doors with contoured geometry

Turbofan engine with variable exhaust cooling

Rotary hydraulic motor driven hybrid thrust reverser actuation system with end-of-stroke snubbing

Turbocharger with an annular rotary bypass valve

Dual function air diverter and variable area fan nozzle

Aircraft propulsion system fan case comprising thrust reversing assembly

Compact actuation system for flow nozzle

Three stream, variable area, vectorable nozzle

Turbocharger with an annular rotary bypass valve

Three stream, variable area fixed aperture nozzle with pneumatic actuation

Device for pivoting a rotor of a turbomachine from a first position into a second position

Turboprop engine with compressor turbine shroud

Stationary blade ring, assembly method and turbomachine

Door for thrust reverser of an aircraft nacelle

Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device

Start system for gas turbine engines

Gas turbine engine duct blocker that includes a duct blocker rotor with a plurality of roller elements

Gas turbine engine duct blocker with rotatable vane segments

Fan duct blocker actuation tab seal

System for mounting combustor transition piece to frame of gas turbine engine

Gas turbine compressor last stage rotor blades with axial retention

Industrial plant with noise attenuation hood

Turbocharger with divided turbine housing and annular rotary bypass valve for the turbine

Turbine assembly and method for securing a closure bucket

Turbojet engine with an element of the nacelle attached to the intermediate casing

Aggregate vane assembly

Turbocharger with turbine nozzle vanes and an annular rotary bypass valve

DOOR WITH MOVABLE SPOILER FOR DOOR-TYPE THRUST REVERSER

Connecting device, driving device and charging device

GAS TURBINE TRANSITION PIECE AIR BYPASS BAND ASSEMBLY

Gas turbine engine air valve assembly

Turbocharger with annular rotary bypass valve for the turbine

Spool support structure for a multi-spool gas turbine engine

Remote pitch controller for a variable pitch propeller

Variable area turbine vane arrangement

Variable geometry vane

Inlet particle separator system for a gas turbine engine

VARIABLE GEOMETRY TURBOCHARGER

Turbocharger

GAS TURBINE ENGINE WITH ROTATIONALLY OVERLAPPED FAN VARIABLE AREA NOZZLE

Fresh gas system swirl generator

Integral thrust vector and roll control system

Variable geometry turbine having intermeshing control and guide blades

Pintle-controlled propulsion system with external ring actuator

Annulus filler

Variable turbine vane actuation mechanism having a bumper ring

Pitch control ring for stator vanes of a turbomachine

Gas turbine engine systems involving rotatable annular supports

Gas turbine engine air valve assembly

Variable-vane assembly having fixed axial-radial guides and fixed radial-only guides for unison ring

Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit

Rotary metering valve arrangement

Adjustable turbine exhaust flow guide and bearing cone assemblies

Device for adjusting the centring of a turbo-engine pivoting vane control synchronization ring

Nozzles with rotatable sections for variable thrust

Bushing for thermally independent bypass air metering valve

Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps

Method and system for rotating a turbine stator ring

Vernier duct blocker

Vectorable nozzle with sideways pivotable ramp

Variable position intake for an aircraft mounted gas turbine engine

Actuation assembly for variable geometry turbochargers

Split vane flow blocker

Variable geometry turbocharger