FEATURE FOR SAFELY INDICATING ROTOR TO STATOR CLASHING

GAS TURBINE ENGINE HAVING A SENSOR ASSEMBLY FOR MONITORING PROPELLER WHIRL

GEARED TURBOFAN WITH OVERSPEED PROTECTION

HYDROGEN PROPULSION ASSEMBLY COMPRISING A DEVICE FOR INJECTING INERT GAS, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY

METHOD AND SYSTEM FOR DETECTING A SHAFT SHEAR EVENT

TURBINE OVERSPEED PROTECTION

TURBINE OVERSPEED PROTECTION

CORE TURNING SYSTEM

SYSTEM AND METHOD FOR DETERMINING PROBABILISTIC BURST

Method and system for detecting a shaft shear event

TURBINE ENGINE SHAFT SHEAR DETECTION

Turbine containment system

Gas turbine engine

System and method for detecting failure of a propeller control unit

GEARED TURBOFAN WITH OVERSPEED PROTECTION

Safety apparatus

System and method for detecting a shaft event on an engine

Detecting damage to a gas turbine engine

Electrical resistance wear indicator

Shaft shear detection in a gas turbine engine

FAN TRACK LINER

Geared turbofan with overspeed protection

Rotor overspeed protection assembly

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

Anti-rotation method for angled face cap probe

Aircraft engine intake arrangement comprising a mechanical decoupler

Method and a system for detecting the angular position of blades of a turbine engine rotor wheel

Anti-windmilling system for a gas turbine engine

SYSTEMS AND METHODS FOR ENGINE VIBRATION MONITORING

Shaft shear detection through shaft oscillation

Method of monitoring rubbing between a rotary party and a stationary part in a rotating turbomachine, monitoring arrangement and turbomachine

Active centering control for static annular turbine flowpath structures

Axial retention of a fan shaft in a gas turbine engine

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

Electrical resistance wear indicator

Geared turbofan with overspeed protection

Following blade impact load support

Gas turbine blade flutter monitoring and control system

STUB SHAFT

Portable jig and fixture for precision machining

SYSTEMS AND METHODS INVOLVING MULTIPLE TORQUE PATHS FOR GAS TURBINE ENGINES

Gas turbine engine with a geared turbofan arrangement

Fan containment case for a gas turbine engine

Shaft shear detection through shaft oscillation

Rotor blade damage

Composite airfoil with fuse architecture

Anti-windmilling system for a gas turbine engine

Shaft shear detection through shaft oscillation

Run-up surface for the guide-vane shroud plate and the rotor-blade base plate

Steam turbine stage measurement system and a method

Method of monitoring rubbing between a rotary party and a stationary part in a rotating turbomachine, monitoring arrangement and turbomachine

Calibration circuit and method of use

Shaft failure detection using passive control methods

Gas turbine cool-down phase operation methods for controlling turbine clearance by adjusting air flow rate

Emergency shut-down detection system for a gas turbine

SYSTEM FOR DETECTING ABNORMAL MOVEMENT OF A SHAFT IN A GAS TURBINE ENGINE

GAS TURBINE ENGINE HAVING ENERGY DISSIPATING GAP AND CONTAINMENT LAYER

PROTECTIVE DEVICE FOR A TURBOMACHINE

Turbocharger turbine containment structure

Frangible airfoil

Turbine engine shaft break detection

Acoustic measurement system for detecting turbine blade lockup

Ground handling system for a composite fan case and a method of using the same

Nonlinear rolling bearing radial support stiffness

System and method for turbomachinery vane prognostics and diagnostics

Turbine engine comprising a device for braking the fan rotor

Method of stopping a rotorcraft engine in overspeed, and a system and a rotorcraft associated therewith

Case with vane retention feature

High sensitivity inductive sensor for measuring blade tip clearance

Stub shaft

Pivoting fan track liner for blade retainment

Sensor for measuring blade tip clearance in gas turbines

Disc axis adjusting mechanism in gas turbine

Method and device for monitoring the malfunction of APU turbine vane fracture and rotor shaft jam

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

Methods and systems for blade health monitoring

Sensor hoop storage and transport apparatus

Methods and apparatus for measuring axial shaft displacement within gas turbine engines

Determining the deterioration of a gas turbine engine in use

Method of detecting and localizing partial rotor-stator rubbing during the operation of a turbine

Methods and system for detecting turbocharger degradation

Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane

Tip clearance probe including anti-rotation feature

Method for determining the diameter of a rotor, which is equipped with rotor blades, of a turbomachine

NEURAL NETWORK-BASED TURBINE MONITORING SYSTEM

Method for adjusting the radial gaps which exist between blade airfoil tips or rotor blades and a passage wall

Axial turbine with containment shroud

Fan and boost joint

System for detecting an impact on an aircraft engine impeller wheel

Gas turbine engine comprising means for axially retaining a fan of the engine

Method and apparatus for obtaining discrete axial clearance data using radial clearance sensors

Dynamic load reduction system

Shaft break detection

Rotatable component with controlled load interface

Target sensor

Fan blade with sheath

Wear pin gap closure detection system for gas turbine engine

TURBINE ENGINE AND LOAD REDUCTION DEVICE THEREOF

Joint assembly

Systems and methods involving multiple torque paths for gas turbine engines

TURBO MACHINE SPOOL PARAMETER DETECTION

Case with ballistic liner

System and method for rotary machine online monitoring

System for detecting an ephemeral event on a vane impeller of an aircraft engine

DIAGNOSIS OF BEARING THERMAL ANOMALIES IN AN ELECTRICAL MACHINE

Systems and methods involving multiple torque paths for gas turbine engines

Automated sensor specific calibration through sensor parameter download

Method and system for monitoring a turbojet engine

Method and system for detecting the ingestion of an object by an aircraft turbine engine during a mission

Managing spool bearing load using variable area flow nozzle

Methods, systems and/or apparatus relating to turbine blade monitoring

Automated sensor specific calibration through sensor parameter download

Method for the provision of fire protection for titanium components of an aircraft gas turbine and titanium components for an aircraft gas turbine

System and method for monitoring radial motion of a rotating shaft of a turbocharger

METHOD AND SYSTEMS FOR MEASURING BLADE DEFORMATION IN TURBINES

Decoupler system for rotor assemblies

Vibration management for gas turbine engines

Turbine engine wheel

Systems and methods involving multiple torque paths for gas turbine engines

Managing spool bearing load using variable area flow nozzle

System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine

Blade assembly

Method and device for reducing the speed in the event of breakage of a gas turbine engine turbine shaft

Gas turbine and method for shutting off a gas turbine when breakage of a shaft is identified

Low-cost frangible cable for gas turbine engine

Gas turbine engine assembly and methods of assembling same

Systems and methods for monitoring thermal growth and controlling clearances, and maintaining health of turbo machinery applications

Shroud for an air turbine starter

Displacement sensor system and method of operation

Nacelle assembly for a gas turbine engine

Warning system for turbine component contact

Gas turbine engine blade tip clearance apparatus and method

Device to measure the axial displacement of the tip of the blades of a turbomachine for tests on the ground, and a process for using the device

Axial-flow thermal turbomachine

Thermal turbomachine

Apparatus and method of detecting wear in an abradable coating system

Methods and systems for operating rotary machines

Air intake structure for aircraft engine

Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing

Air intake structure for aircraft engine

Smart component for use in an operating environment

Apparatus and method for detecting an impact on a rotor blade

Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement

Fan blade with embrittled tip

Method of minimizing the gap between a rotating turbine blade and a casing of a turbine, a turbine, and a method of determining the wear behavior of a wheel of a rotor

Electronic safety system for the avoidance of an overspeed condition in the event of a shaft failure

Core turning system