COMPRESSOR FRANGIBLE CONTAINMENT STRUCTURE

LUBRICANT PUMP SYSTEM AND METHOD FOR AIRCRAFT ENGINE

PROPELLER FOR A TURBINE ENGINE OF AN AIRCRAFT WITH A VARIABLE-PITCH VANE AND A GEARED COUNTERWEIGHT DEVICE

Effector inlet cover, and method of separation

Lubricant pump system and method for aircraft engine

Turbomachine module equipped with an electric machine rotor

Laterally biased system for mounting auxiliary components to gas turbine engines

Lubricant pump system and method for aircraft engine

Systems and methods for selectively disconnecting embedded electrical machines in gas turbine engines

Gas turbine engine bearing housing

Torque limiting device in a connection between a gearbox and a stationary structure in a gas turbine engine and a gas turbine engine

Geared gas turbine engine with gear driving low pressure compressor and fan at a common speed and a shear section to provide overspeed protection

Fan for an aircraft cooling unit

Frangible strut for gas turbine engine

Crushable spacer and bolted joint for a gas turbine engine

TURBINE ENGINE CASE ATTACHMENT AND A METHOD OF USING THE SAME

Turbomachine comprising a means of uncoupling a fan

Mechanical shear fuse for engine motoring system

Frangible Gas Turbine Engine Airfoil

Air turbine starter with decoupler

Frangible gas turbine engine airfoil with chord reduction

Frangible strut for gas turbine engine

Method and system for elastic bearing support

Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pin

Turbomachine comprising a means for decoupling a fan

Air turbine starter with decoupler

Method for manufacturing a motoring system for a gas turbine engine

Containment assembly

Method for compressing an incoming feed air stream in a cryogenic air separation plant

Method for compressing an incoming feed air stream in a cryogenic air separation plant

Method for compressing an incoming feed air stream in a cryogenic air separation plant

Fuse joint with fenestrated fuse pin

Frangible airfoil for a gas turbine engine

Turbomachine

Gas turbine engine with minimal tolerance between the fan and the fan casing

Decoupler assembly for engine starter

Gas turbine engine component with performance feature

Gas turbine engine with gearbox health features

Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section

Output assembly for an accessory gearbox of a gas turbine engine

Gas turbine engine fan blade containment systems

Gas turbine engine fan blade containment systems

Method and system for rotor overspeed protection

Fan rotatably connected to a drive shaft by means of a meltable element

Seal panel for a gas turbine engine

STUB SHAFT

Propulsive assembly having decouplable casing portions

Portable jig and fixture for precision machining

Dual stage catalytic thruster

Method and system for elastic bearing support

Gas turbine engine with a geared turbofan arrangement

Gas turbine engine with a geared turbofan arrangement

Fused pilot for boss-mounted gearbox link

Method for release of fan blisk airfoil with external shaped charge

Mechanical shear fuse for engine motoring system

Pinned mechanical fuse for engine motoring system

Deformable turbine bearing mount for air turbine starter

Air turbine starter with decoupler

Device for modulating a gas ejection section

Twist-breakable mechanical fuse and cooling unit of a turbine engine fitted with such a fuse

Fastener and method of restricting fluid flow using same

Accessory assembly of a turbine engine

Two degree-of-constraint semi-fusible gearbox mounting link

One degree-of-constraint semi-fusible gearbox mounting link

One degree-of-constraint semi-fusible gearbox mounting link

Two degree-of-constraint semi-fusible gearbox mounting link

Containment case trench filler layer and method of containing releasable components from rotatable machines

Connection system for housing elements of a turbine intermediate casing

Method and disconnector for disconnecting a drive shaft

TURBOMACHINE COMPRISING A MEANS OF UNCOUPLING A FAN

Gas turbine engine component with performance feature

Shaft assembly comprising a frangible coupling and a flexible coupling

Spring-assisted deployment of a pivotable rocket motor

Turbocharger turbine containment structure

Turbine assembly having a rotor system lock

Turbine engine case attachment and a method of using the same

Frangible airfoil

Auxiliary component mount including a fusible region configured to break at a predetermined load

Blade

Blade with metallic leading edge and angled shear zones

Collapsible support structure for a gas turbine engine

Bladed rotor arrangement and a lock plate for a bladed rotor arrangement

Method for compressing an incoming feed air stream in a cryogenic air separation plant

Method for compressing an incoming feed air stream in a cryogenic air separation plant

Frangible Sheath for a Fan Blade of a Gas Turbine Engine

Engine mount waiting fail safe lug joint with reduced dynamic amplification factor

Casing assembly

Stub shaft

Bearing cage and bearing means having this type of bearing cage as well as method for designing, repairing and/or replacing such a bearing cage

Frangible mounting arrangement and method for providing same

Turbomachine fan casing assembly

Structural guide vane circumferential load bearing shear pin

Safety device for a bearing arrangement of a rotor of a turbomachine

Break-away thermal blanket joint

Turbocharger

Apparatus for energy absorption, a turbo-machine and a method for energy absorption

Turbine engine gearbox mount with multiple fuse joints

Mounting arrangement

Mount with an axial upstream linkage for connecting a gearbox to a turbine engine case

Gas turbine spindle bolt structure with reduced fretting motion

Fan retention shaft

Containment ring for gas turbine engine

Compressor frangible containment structure

Fusible gearbox center guide support with frangible catcher pin systems and methods