VARIABLE FAN NOZZLE THRUST REVERSER ASSEMBLY

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

LINKAGE DAMPER FOR AIRCRAFT COMPONENT

GEARED TURBOFAN WITH OVERSPEED PROTECTION

VARIABLE AREA TURBINE NOZZLE ASSEMBLY

VARIABLE AREA TURBINE NOZZLE ASSEMBLY

SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS

JOINT FOR CONNECTION TO VARIABLE GUIDE VANE OF GAS TURBINE ENGINE

VARIABLE FLOWPATH CASINGS FOR BLADE TIP CLEARANCE CONTROL

FUELDRAULIC ACTUATION

THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGE

THRUST REVERSER COMPRISING FIXED CASCADES AND A SEALING MEMBRANE

VANE ACTUATING ARM FOR A GAS TURBINE, TURBOMACHINE HAVING THE VANE ACTUATING ARM, AND METHOD FOR MOUNTING A VANE ACTUATING ARM FOR A TURBOMACHINE

Locking assembly for an aircraft propulsion system thrust reverser

THRUST REVERSER WITH LOST MOTION DEVICE

LIMITED FLOW THRUST REVERSER ACTUATING

THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGE

THRUST REVERSER WITH BLOCKER DOOR LOCK

Variable guide vane assembly for gas turbine engine

TURBOFAN HAVING MOBILE DEFLECTORS AND A SYSTEM FOR ACTUATING THE DEFLECTORS

System for changing the pitch of the blades of a turbomachine propeller

Turbofan having mobile deflectors and a system for actuating the deflectors

Cascade thrust reverser actuation assembly for a turbofan engine

Variable flowpath casings for blade tip clearance control

Variable guide vane assembly for gas turbine engine

Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing walls

Articulating slider for nacelle

Articulating slider for nacelle

Variable area nozzle assembly and method for operating same

Thrust reverser interspatial blocker system

Device for attaching a connecting rod small end for a thrust reversal cascade flap

Thrust reverser with flaps controlled by a mechanism equipped with aeronautical bellcranks

SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS

Limited flow thrust reverser actuating

Turbine engine compressor variable geometry system with split actuation

Variable nozzle device and variable-displacement type exhaust turbocharger

Bellcrank for a variable adjustment device for a turbomachine

Thrust reverser provided with cable kinematics for scoop flaps

Air inlet duct for a nacelle of an aircraft propulsion assembly

Variable guide vane assembly and vane arms therefor

GEARED TURBOFAN WITH OVERSPEED PROTECTION

Steering rod for turbochargers and method for making it

GAS-TURBINE-ENGINE OVERSPEED PROTECTION SYSTEM

Distributor for a turbomachine radial turbine, turbomachine comprising such a distributor and air conditioning system comprising such a turbomachine

Turbocharger having an actuator-actuated adjusting device and a transmission element with one-part component body

Gas turbine compressor radial door bleed valve

Bypass turbofan engine comprising mobile deflectors

Vane arm torque transfer plate

Nacelle

Over-center thrust reverser primary lock

EXHAUST BYPASS DEVICE AND TURBOCHARGER

Fan module with variable-pitch blades for a turbomachine

Valve for aircraft environmental control system conduit

Retention clip for variable vane arm

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

Geared turbofan with overspeed protection

Linkage assembly preventing axial rotation of the link rod for a gas turbine engine

Bellcrank for a turbomachine

Slat-thrust reverser clearance

Cooling systems for gas turbine engines

Gas turbine engine control system and method for limiting turbine overspeed in case of a shaft failure

Turbocharger

Mechanism for indicating position of a latch mechanism for an aircraft nacelle

Split sleeve hidden door thrust reverser

Translating cascade hidden blocker door thrust reverser

Thrust reverser with displaceable trailing edge body

System including hidden drag link assembly for actuating blocker door of thrust reverser

Target door reverser wit h non-parallel hinge lines

Assembly for controlling variable pitch blades

Variable diffuser having a respective penny for each vane

Variable diffuser having a respective penny for each vane

Nested direct vane angle measurement shaft

Variable vane stabilizer

Control device of an annular row of variable-pitch vanes for an aircraft engine

Profiled bellcrank vane actuation system

SELF-RETAINING VANE ARM ASSEMBLY FOR GAS TURBINE ENGINE

Nacelle of a turbojet engine comprising a thrust-reversing door

Lever connection of a guide vane adjustment for turbomachinery

Nacelle of a turbojet engine comprising an outer thrust-reversing door

Folding and unfolding structure of blade of ceiling fan

Lever with pre-attached self locking nut for a variable turbine geometry turbocharger

Variable turbine geometry vane lever

Impeller shroud with closed form refrigeration system for clearance control in a centrifugal compressor

Hinge mechanism for pivot door thrust reversers

Fan cowl mounted to thrust reverser

Variable vane actuation arrangement

Dual-flow jet engine for an aircraft with an improved aperture

Linkage assembly preventing axial rotation of the link rod

Hidden linkage for a translating cowl thrust reverser

Aircraft propulsion unit having thrust reverser flaps connected to an inter-compressor casing located between the engine compressors

Nacelle

Unison ring assembly

Variable-pitch vane assembly

Thrust reverser system exhibiting limited aerodynamic perturbation

System and method of operating a ducted fan propulsion system during aircraft taxi

Variable-pitch blade control ring for a turbomachine

Split synchronization ring for variable vane assembly

Geared turbofan with overspeed protection

Variable and adaptable diverterless bump inlet

Passively-driven bleed source switching

Variable stator blade operating device

Variable area fan nozzle actuation system

Bellcrank assembly for gas turbine engine and method

Jet engine nacelle having a reverser flap

System for controlling variable-setting blades for a turbine engine

Aircraft thrust reverser system with alternate reverse thrust load path

Over-center thrust reverser primary lock

Sync ring assembly and associated clevis including a rib

Variable geometry turbocharger

Anti-rattle devices and turbocharger wastegate assemblies including the same

Guide vane assembly with compensation device

Propulsion assembly comprising a duct for feeding the gas generator in an inter-duct casing

Thrust vectoring nozzle

Guide vane adjustment device and turbomachine

Dual turn thrust reverser cascade systems and methods

GAS TURBINE ENGINE

Thrust reverser for a nacelle of an aircraft turbojet engine

Hidden thrust reverser blocker door link arm fitting

Hidden thrust reverser blocker door link arm fitting

Floating, non-contact seal with angled beams

AIRCRAFT GAS TURBINE ENGINE NACELLE

Device for the individual adjustment of a plurality of variable-pitch radial stator vanes in a turbomachine

Infrared suppression system in a gas turbine engine

VARIABLE STATOR VANE MECHANISM

Turbine engines with variable area nozzle

Hydraulically Driven Thrust Reverser

Assembly for controlling variable pitch vanes in a turbine engine

Adjustment ring of a variable turbine geometry

System for controlling variable pitch blades for a turbine engine

Self-retaining bushing assembly

Impeller shroud with deflecting outer member for clearance control in a centrifugal compressor

Impeller shroud with pneumatic piston for clearance control in a centrifugal compressor

Segregated impeller shroud for clearance control in a centrifugal compressor

Impeller shroud with thermal actuator for clearance control in a centrifugal compressor

Toothed component optimization for gas turbine engine

Nacelle rear assembly for a turbojet engine comprising a suspension cradle

Nacelle rear assembly for a turbojet engine comprising a cradle for a core-type mast

Sliding nozzle flap assembly

Blocker door link arm and fitting

Nacelle deflection measurement assembly

Method and apparatus for adjusting variable vanes

Link setting assembly and method

Clevis link for toggle mechanism of ram air turbine actuator

Tandem thrust reverser with sliding rails

Variable vane stabilizer

Translating cascade hidden blocker door thrust reverser

Thrust reverser system with translating elements

Compliant shroud for gas turbine engine clearance control

Turbine engine stator vane, fan casing comprising such a vane, thrust reverser system of a turbine engine equipped with such a vane and turbine engine equipped with said vane, said casing or said system

Turbocharger with adjustable vanes

Vibration damping drag link fitting for a thrust reverser

Sandwich structure having hinge assemblies for accommodating differential in-plane expansion of face sheets

Variable nozzle unit and variable geometry turbocharger

System and method for reducing idle thrust in a translating cowl thrust reverser

Turbine shroud assembly and method for loading

System and method for supporting a turbine shroud

Telescoping electrical cable

DETECTION METHOD OF SENSOR IN GAS TURBINE

Thrust reverser apparatus and method

Gas turbine engine rapid response clearance control system

Variable area fan nozzle actuation system

Cooling systems for gas turbine engines

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

Translating cascade hidden blocker door thrust reverser

Slat-thrust reverser clearance

TURBOJET ENGINE NACELLE COMPRISING A UNIT ASSEMBLY CAPABLE OF MOVING ALONG A GUIDE ASSEMBLY

Gas turbine engine and blocker door assembly

Thrust reverser sliding door assembly

Split sleeve hidden door thrust reverser

Thrust reverser with hidden linkage blocker doors

Radial fastening of tubular synchronizing rings

Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle

Turbomachine comprising a plurality of fixed radial blades mounted upstream of the fan

Thrust reverse variable area fan nozzle

Machined vane arm of a variable vane actuation system

Thrust reverser unit having both nested cascades translating linearly and only one cascade rotational

Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system

Rotary actuator for variable vane adjustment system

Single bolting flange arrangement for variable guide vane connection

Vane lever arm for a variable area vane arrangement

Variable stator vane arrangement

Systems and methods for shock load reduction

Thrust reverser for a turbofan engine

Thrust deflecting device and aircraft engine

Sliding nozzle flap assembly

Variable nozzle unit, variable geometry system turbocharger, and power transmission member manufacturing method

Gas turbine cowl

Rod end tensioner and self adjusting rod end

Compact actuation system for flow nozzle

Three stream, variable area, vectorable nozzle

Tandem thrust reverser with multi-point actuation

Tandem thrust reverser with multi-bar linkage

Exhaust-gas turbocharger

Gimbal pin for jet propulsion system

Mounting structure of cooling-fan

Gas turbine engine with a fire wall and an off-take device

Exhaust-gas turbocharger

Apparatus and method for bleeding off compressor air in a jet engine

Blocker door actuation system and apparatus

Adjustable and lockable turnbuckle

Pivot thrust reverser with multi-point actuation

Reverse scissor thrust reverser for a turbine engine

Thrust reverser system with translating-rotating blocker doors and method of operation

Actuating apparatus for a turbine of an exhaust gas turbocharger

Three stream, variable area fixed aperture nozzle with pneumatic actuation

Tandem thrust reverser with sliding rails

Pivot thrust reverser surrounding inner surface of bypass duct

System for changing the pitch of the blades of a propeller

Stopper structure for regulating opening degree of nozzle vane in turbocharger

Turbocharger

Bellcrank for a variable vane assembly

Stator vane adjusting device of a gas turbine

Stroke transmitter for gas turbine

Gas turbine engine synchronizing ring with multi-axis joint

Drive lever arrangement

TOP HAT BEARING RETAINER FOR VARIABLE VANE ACTUATOR

TWO-PIECE DUCT ASSEMBLY

Spherical-link end damper system with near constant engagement

BULB SEAL WITH METAL BACKED FASTENER

Four bar drive mechanism for bleed system

Four bar bracket

Linked ring petal actuation for variable area fan nozzle

Thrust reverser assembly and method of operation

Modular louver system

Compact IGV for turboexpander application

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

Two-surface sandwich structure for accommodating in-plane expansion of one of the surfaces relative to the opposing surface

Bypass duct with angled drag links

ACTUATOR ASSEMBLY

Hydraulic device for changing the pitch of a propeller

Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition

System for transporting turbomachinery

Turbine engine having a stage of variable-pitch stator vanes with independent control

Scissor duct flex joint damper

Fan duct blocker actuation tab seal

Gas turbine engine synchronizing ring bumper

Gas turbine engine synchronizing ring bumper

Reverse thrust device

Fluid Turbine Having Optimized Blade Pitch Profiles

Axial turbomachine having an axially displaceable guide-blade carrier

Bellows type sealing device for partition penetration by a connecting rod of a turboprop fan blade orientation control system

Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine

Variable turbocharger and control method for the same

External flap retaining mechanism

TURBOCHARGER

Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut

Method and apparatus for controlling compressor bleed airflow of a gas turbine engine using a butterfly valve assembly

CONJUGATE CURVE PROFILES FOR VANE ARMS, MAIN-ARMS, AND UNISON RINGS

VARIABLE AREA FAN NOZZLE STIFFENERS AND PLACEMENT

Simplified system for controlling propeller blade pitch in an aircraft turboshaft engine

Simplified system for controlling propeller blade pitch in an aircraft turboshaft engine

BYPASS TURBOJET ENGINE NACELLE

Nozzle adjusting mechanism and method

Variable geometry vane

Turbocharger

Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle

Thrust reverser with grids for jet engine

AN APPARATUS FOR OSCILLATING AND ORIENTING A VANE RELATIVE TO A FLUID

DEVICE FOR MOVING A PLURALITY OF HATCHES IN A GAS TURBINE ENGINE

Tamperproof and calibration device, especially for a turbocharger with a variable nozzle device

Nacelle for double flow engine

Turbo engine

Variable turbo supercharger and method of driving the same

Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle

Gas turbine

Slideable liner link assembly

Turbine blade assembly and steam turbine

Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system

Control device of variable pitch vanes in a turbomachine

Device for pivoting at least one pivotable element in a gas turbine engine

Turbine engine valve assembly and method of assembling the same

Variable turbocharger and control method for the same

Variable turbine vane actuation mechanism having a bumper ring

Pitch control ring for stator vanes of a turbomachine

Supercharger

Single actuator controlled rotational flow balance system

Lever for rotating a turbomachine variable-pitch stator vane about its pivot

Bleed system for a low-pressure compressor of a turbomachine

Leaned high pressure compressor inlet guide vane

Bleed off valve system

Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle

Fan variable area nozzle for a gas turbine engine fan nacelle

Turbomachine stator including a stage of stator vanes actuated by an automatically centered rotary ring

Flexible shaft inline coupler

Adjustable guide device

Methods and apparatus for controlling variable stator vanes

Device for support of an adjusting ring which encompasses at a distance a circular blade carrier

Compressor in an exhaust gas turbocharger of an internal combustion engine and method for operating the compressor

Turbocharger compressor with an auxiliary rotor wheel and magnetic clutch

Methods and apparatus for rotary machinery inspection

Device for moving at least one moveable element in a gas turbine

System for controlling stages of variable-pitch stator vanes in a turbomachine

Variable geometry turbocharger

Rotary actuator

Exhaust-gas turbocharger, regulating device for an exhaust-gas turbocharger and vane lever for a regulating device

Fast start-up combined cycle power plant

Variable vane arm/unison ring attachment system

Axial divergent section slot nozzle

Dual retention vane arm