Load Controlling Slider Assembly

System for cooling an aircraft turbojet engine

Dual-mode plug nozzle

Turbine with adjusting ring

Axial flow turbine having a diaphragm split in two halves at a horizontal joint plane

Bleed valve system

Turbojet engine with thrust take-up means on the inter-compressor case

Non-contact seal assembly for rotational equipment

Oil tank mount arrangement on a geared turbofan engine

Composite piston ring seal for axially and circumferentially translating ducts

Device for modulating a gas ejection section

RETRACTABLE ROCKET MOTOR IGNITER

Mount structure for an aircraft ancillary engine unit

Segmented annular seal

Solenoid actuated tine lock

Aircraft engine rotor repaired with microstructural enhancement

Floating support assembly for compensating for axial thermal expansion

Pulse detonation drive

Non-contact seal assembly for rotational equipment

Fan casing assembly

Composite piston ring seal for axially and circumferentially translating ducts

Air turbine starter systems including gearbox-integrated clutch modules and gas turbine engines employing the same

Oil tank mount arrangement on a geared turbofan engine

Actuator device for moving a movable cowl of a thrust reverser

Conduit assembly and method of utilization

Decoupled translating sleeve

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

Sleeve linkage for thrust reverser

Turbine engine face seal arrangement including anti-rotation features

Nozzle arrangement for a gas turbine engine

Assembly tool for exhaust turbochargers

Turbofan engine with variable exhaust cooling

Aircraft propulsion system fan case comprising thrust reversing assembly

Turbomachine geared architecture support assembly

Metal joining and strengthening methods utilizing microstructural enhancement

METHODS AND SYSTEMS FOR OPERATING AN INTEGRATED ACTUATOR

Thrust reverser system

Inner turbine shell axial movement

Turbomachine geared architecture support assembly

Low-ductility turbine shroud

Mounting apparatus for low-ductility turbine shroud

Method and apparatus for supplying heated, pressurized air

Airplane jet engine thrust reverser having gratings or cascades

Gas turbine engines including broadband damping systems and methods for producing the same

Gas turbine engine generator switchable drive

RECONFIGURABLE HEAT TRANSFER SYSTEM FOR GAS TURBINE INLET

REVERSE THRUST DEVICE

Method for balancing a propulsive system having non-hull contra-rotating propellers

Gas-turbine engine with bleed-air tapping device

Guide system for nacelle assembly

EXHAUST GAS TURBOCHARGER

Turbojet engine nacelle

High-pressure turbine for turbomachine, associated guide vane sector and aircraft engine

Gas turbine combustor exit duct and hp vane interface

Flow discharge device

Rotary machine scroll structure and rotary machine

Gas turbine combustor exit duct and HP vane interface

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

Engine assembly for aircraft with sliding nacelle

Turbocharger

Pintle-controlled propulsion system with external ring actuator

Gas turbine with a gap blocking device

Method for producing a contoured gap, and turbo-engine comprising contoured gap

Gas turbine shroud support apparatus

BLADE ATTACHMENT RETENTION DEVICE

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

Annular isolator dual mode scramjet engine

Bleed off valve system

ASPIRATING LABYRINTH SEAL

Fan frame

Exhaust gas turbocharger for an internal combustion engine

Mounting arrangement

Turbomachine, especially a gas turbine

Variable-nozzle turbocharger with integrated bypass

Turbocharger support

Gas turbine engine assembly and methods of assembling same

Shroud tip clearance control ring

Missile control system and method

Exhaust gas turbocharger for an internal combustion engine

Gas turbine combustor sliding joint