JET NOZZLE EFFECTIVE AREA CONTROL SYSTEM FOR GAS TURBINE ENGINE

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

Exhaust Area and Flow Turning Control

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

ACTUATION MECHANISM

ACTUATION MECHANISM

FLUID CONTROL VALVE

EXHAUST NOZZLE AND A METHOD OF OPERATING AN EXHAUST NOZZLE

Engine mount system for a gas turbine engine

TELESCOPIC BALLSCREW ACTUATOR

Aircraft propulsion system exhaust nozzle with ejector passage(s)

Method for coupling a hydroelectric power plant to the grid comprising at least two hydroelectric units

Drive system for translating structure

Method and system for monitoring a system for actuating a component of a turbomachine

Variable three dimensional convergent-divergent nozzle

Telescopic ballscrew actuator

Engine mount system for a gas turbine engine

Variable area nozzle exhaust system with integrated thrust reverser

Gas turbine engine bifurcation located fan variable area nozzle

Drive system for translating structure

PROPULSION SYSTEM FOR AN AIRCRAFT AND METHOD OF MANUFACTURING A PROPULSION SYSTEM FOR AN AIRCRAFT

Multi-nozzle jet propulsor

VARYING THE BYPASS RATIO OF A TURBOFAN ENGINE

Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement

Variable area fan nozzle with wall thickness distribution

Translating outer cowl flow modulation device and method

Supersonic aircraft turbofan

Multi-actuation control system with pressure balancing plumbing

Telescopic ballscrew actuator

Nacelle for an aircraft turbojet engine provided with a hydraulic roto-linear actuator of a thrust reverser and of a variable-section nozzle

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

Gas turbine engine bifurcation located fan variable area nozzle

Convergent-divergent nozzle for a turbofan engine of a supersonic aircraft and method for adjusting the nozzle throat surface in a nozzle of a turbofan engine

Asymmetric load compensation system

Nozzle with variable throat and exit areas

Fan nacelle trailing edge

Unmanned aerial vehicle

Nacelle deflection measurement assembly

Enhanced durability drive link for high load misalignment

Control device of a variable section nozzle and the implementation method thereof

Fiber optic sensing for variable area fan nozzles

THROAT AREA CONTROL SYSTEM

Pulse detonation drive

Gas turbine engine with low stage count low pressure turbine

Variable area fan nozzle with wall thickness distribution

Telescoping electrical cable

Exhaust nozzle control for a gas turbine engine

Adaptive aircraft engine and aircraft having an adaptive engine

Variable area nozzle assisted gas turbine engine restarting

Controlling nozzle areas of variable area fan nozzles

Dual-cam bellcrank mechanism

Variable area fan nozzle with drive system health monitoring

Rod-and-bracket connector system for securing a pivoting member to a guide anchor moveably secured within a guide track

System for actuating an exhaust cowl

Integrated thrust reverser actuation system

Gas turbine engine system for modulating flow of fan by-pass air and core engine air

Engine cowling of a gas turbine with thrust-reversing device and adjustable outlet nozzle

Thrust vectoring apparatus, thrust vectoring method, and flying body

Electric boost actuation system for translating rings

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

Nozzle arrangement for a gas turbine engine

Variable area nozzle for gas turbine engine

Device for controlling a nozzle of variable cross-section of an aircraft

Pivot door thrust reverser with variable area nozzle

Gas turbine engine with low fan noise

Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzle

Self-sealing apparatus that adjusts a throat area of a nozzle

Aircraft comprising a control device for a jet pipe nozzle with variable cross-section powered by two independent electrical power supplies

Compact actuation system for flow nozzle

Three stream, variable area, vectorable nozzle

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

Translating outer cowl flow modulation device and method

Method for controlling a variable nozzle section of an aircraft

Fan variable area nozzle with cable actuator system

Gas turbine exhaust noise reduction

Three stream, variable area fixed aperture nozzle with pneumatic actuation

Variable geometry structure

Variable area fan nozzle position and skew sensing

Linked ring petal actuation for variable area fan nozzle

Device for controlling a variable section nozzle of an aircraft

Variable area fan nozzle with drive system health monitoring

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

Aircraft control system

ACTIVE FAN FLUTTER CONTROL

Gas turbine engine bifurcation located fan variable area nozzle

Variable area fan nozzle

Control mechanism

Gas turbine engine having slim-line nacelle

Gas turbine engine having slim-line nacelle

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

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

Translating core cowl having aerodynamic flap sections

TRANSLATING CORE COWL FOR A GAS TURBINE ENGINE

Core cowl airfoil for a gas turbine engine

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

Operational line management of low pressure compressor in a turbofan engine

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

Fan variable area nozzle with cable actuator system

Managing low pressure turbine maximum speed in a turbofan engine

Gas turbine engine having variable flow through a bifurcation having an intake with multiple louvers

Reduced take-off field length using variable nozzle

Variable area nozzle assisted gas turbine engine restarting

Gas turbine engine with variable area fan nozzle bladder system

Bifurcation and aft vent used to vary fan nozzle exit area

Gas turbine engine reheat fuel system

Fan variable area nozzle positional measurement system

System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft

Turbofan engine nozzle assembly and method of operating same

Gas turbine engine having slim-line nacelle

Pressure balance control for gas turbine engine nozzle

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

Fan variable area nozzle for a gas turbine engine fan nacelle

Rotary adjustable exhaust nozzle

Gas turbine engine having a thrust reverser system with drag link connectors at inter-compressor frame structure

High flow plug nozzle apparatus and method of using the same

Axially translating and radially tilting fan nozzle segments with combined actuation and position sensing