VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

DESIGN OF A REAR-CONE EXHAUST DUCT FOR ADDITIVE MANUFACTURING

ACTUATION MECHANISM

Seal system using layers of seal segments forced into sealing engagement using tension cable

Exhaust nozzle assembly for an aircraft propulsion system

Liquid hydrogen-liquid oxygen fueled powerplant

Variable area exhaust nozzle system and method for control thereof

Single movement convergent and convergent-divergent nozzle

Variable area nozzle exhaust system with integrated thrust reverser

Reconfigurable exhaust nozzle for a gas turbine engine

Exhaust nozzle with centerbody support structure for a gas turbine engine

Exhaust nozzle with vane support structure for a gas turbine engine

Methodology for minimizing aerodynamic buzz in an exhaust nozzle

Single movement convergent and convergent-divergent nozzle

Exhaust nozzle

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Propelling nozzle for a turbofan engine on a supersonic aircraft

Nacelle of a turbojet comprising a reverser flap and a deployment system with delay

Auxiliary device for three air flow path gas turbine engine

Split sleeve hidden door thrust reverser

Supersonic aircraft turbofan

Dual-mode plug nozzle

Supersonic aircraft turbofan engine

Tail cone apparatus and methods for reducing nozzle surface temperatures

Moveable exhaust plug liner

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

AIRCRAFT GAS TURBINE HAVING A VARIABLE OUTLET NOZZLE OF A BYPASS FLOW CHANNEL

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

Expandable exhaust cone

Turbine engines with variable area nozzle

Dielectric seal device

CHEVRON SYSTEM FOR GAS TURBINE ENGINE

Aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other

Pulse detonation drive

Exhaust nozzle with non-coplanar and/or non-axisymmetric shape

Exhaust nozzle control for a gas turbine engine

Liner for a gas turbine engine

Convergent-divergent nozzle

Variable area fan nozzle with drive system health monitoring

Stepped fairing modulated exhaust cooling

Split sleeve hidden door thrust reverser

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

Variable fan nozzle using shape memory material

Nozzle arrangement for a gas turbine engine

Nozzle having a variable neck section for a spacecraft thruster provided with a mobile needle

Variable area nozzle for gas turbine engine

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

Turbofan with variable bypass flow

Flow control device for a three stream turbofan engine

Variable area fan nozzle systems with improved drive couplings

Exhaust nozzle and method for changing exhaust flow path

Threaded rod for system for deploying a deployable divergent segment of a thruster

Gas turbine engine exhaust nozzle cooling valve

Jet flow nozzle and jet engine

Multi axis slide carriage system

Aircraft gas turbine with variable bypass nozzle by deforming element

Gas turbine engine with bypass mixer

EXHAUST NOZZLE FOR A BYPASS AIRPLANE TURBOJET HAVING A DEPLOYABLE SECONDARY COVER AND A RETRACTABLE CENTRAL BODY

Flade discharge in 2-D exhaust nozzle

Thrust reverser and variable area fan nozzle actuation system and method

Integrated variable geometry flow restrictor and heat exchanger

Actuation mechanism for a convertible gas turbine propulsion system

Variable area fan nozzle

Guide system for nacelle assembly

Variable fan duct nozzle translatable core/inner cowl including two overlapping portions made of different materials

Nacelle with an adaptable outlet section

Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise

Magnetic advanced generation jet electric turbine

Method of operating a turbofan engine cowl assembly

VARIABLE AREA FAN NOZZLE STIFFENERS AND PLACEMENT

TURBOFAN TEMPERATURE CONTROL WITH VARIABLE AREA NOZZLE

Cooling system for an aero gas turbine engine

Linear telescopic actuator for moving a first and a second element relative to a stationary element

Integral composite slider for aircrafts

Gas turbine engine device

Jet nozzle plug with varying, non-circular cross sections

Translating core cowl having aerodynamic flap sections

System and apparatus for vectoring nozzle exhaust plume from a nozzle

CONTROLLING THE AERODYNAMIC DRAG OF A GAS TURBINE ENGINE DURING A SHUTDOWN STATE

Core cowl airfoil for a gas turbine engine

Variable slope exhaust nozzle

Variable fan nozzle using shape memory material

Gas turbine engine systems involving variable nozzles with sliding doors

Gas turbine engine variable exhaust nozzle

Actuation mechanism for a convertible gas turbine propulsion system

Method of operating an exhaust nozzle assembly

Turbofan engine cowl assembly and method of operating the same

Turbofan engine cowl assembly and method of operating the same

Turbofan engine nozzle assembly and method for operating the same

Device for Controlling a Gas Flow, a Jet Engine Comprising the Device and an Aircraft Comprising the Device

Central body for a turbojet exhaust channel, turbojet

Continuous real time EGT margin control

Double bypass turbofan

Thrust vector control

Variable area nozzle

Noise reduction tubes

Variable area nozzle for an aircraft engine

Variable area nozzle assembly for an aircraft propulsion system

Exhaust nozzle having a compliant shell for a gas turbine engine

High flow plug nozzle apparatus and method of using the same

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