145653 ⎘
Control; Purpose of the control system to prolong engine life by limiting mechanical stresses
COMPLIANT SHROUD DESIGNS WITH VARIABLE STIFFNESS
#2TRANSFER OF POWER BETWEEN THE HIGH-PRESSURE SHAFT AND THE LOW-PRESSURE SHAFT OF A TURBOMACHINE
#3CORE TURNING SYSTEM
#4Compliant shroud designs with variable stiffness
#5System and method for air filtration with self-cleaning filter medium for an aircraft engine
#6Methods and systems for operating an aircraft engine
#7GAS TURBINE ENGINE STARTER SYSTEMS AND ASSOCIATED METHODS
#8Compliant shroud designs with variable stiffness
#9Digital shaft positioning for a turbine rotor
#10Method and system for mitigating rotor bow in a turbo machine
#11Method for controlling the bending deformation of a turbomachine shaft at rest subjected to the residual heat of operation of the turbomachine
#12System and method for air filtration with self-cleaning filter medium for an aircraft engine
#13Gas turbine engine operating schedules for optimizing ceramic matrix composite component life
#14GAS TURBINE ENGINE AND OPERATION METHOD
#15Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
#16Independently controllable wheel for a turbine section of a gas turbine engine
#17Methods and systems for controlling operation of aircraft engines
#18AIRFLOW CONTROL FOR AIR TURBINE STARTER
#19Apparatus, assemblies, and methods for mitigating thermal bow in the rotor of an engine at start-up
#20Cost effective manufacturing method for GSAC incorporating a stamped preform
#21Method and device for detecting conditions conducive to the onset of pumping with a view to protecting a compressor of an aircraft turbine engine
#22Turbomachine rotor and method for producing same
#23Airflow control for air turbine starter
#24GAS TURBINE ENGINE MOTORING SYSTEM FOR BOWED ROTOR ENGINE STARTS
#25Method of starting a gas turbine engine
#26Turbine engine for reducing rotor bow and method thereof
#27Method of monitoring rubbing between a rotary party and a stationary part in a rotating turbomachine, monitoring arrangement and turbomachine
#28Fan stress tracking for turbofan gas turbine engines
#29Aircraft power setting trims for life extension
#30Integrated fuel and bleed system control architecture
#31Transient control to extend part life in gas turbine engine
#32SYSTEMS AND METHODS FOR BOWED ROTOR START MITIGATION
#33Piezo-electric motor for bowed rotor mitigation
#34Bowed rotor prevention system
#35Gas turbine blade flutter monitoring and control system
#36SYSTEM AND METHOD FOR IMPROVED TURBOMACHINERY OIL LUBRICATION SYSTEM
#37Methods and systems for controlling operation of aircraft engines
#38Turbine engine exhaust casing with improved lifetime
#39Metered orifice for motoring of a gas turbine engine
#40Airfoil with stress-reducing fillet adapted for use in a gas turbine engine
#41Shrouded blade of a gas turbine engine
#42Low-power bowed rotor prevention and monitoring system
#43Turbine engine and method of operating
#44System and method of gas turbine engine shaft cooling
#45Active clearance control for a turbine and case
#46Control device of a variable section nozzle and the implementation method thereof
#47System and method for protecting the structural integrity of an engine strut
#48Gas turbine engine bowed rotor avoidance system
#49Bowed rotor start using a variable position starter valve
#50Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
#51Auxiliary drive bowed rotor prevention system for a gas turbine engine
#52Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
#53Bowed rotor prevention system using waste heat
#54Bowed rotor start response damping system
#55Multi-shaft combined cycle plant, and control device and operation method thereof
#56Method of monitoring rubbing between a rotary party and a stationary part in a rotating turbomachine, monitoring arrangement and turbomachine
#57Thrust reversal for turbofan gas turbine engine
#58High pressure compressor rotor thermal conditioning using discharge pressure air
#59Gas turbine engine component
#60Stator assembly for a gas turbine engine
#61Cost effective manufacturing method for GSAC incorporating a stamped preform
#62Outer shroud with gusset
#63Combustion instability control method
#64Rotor tip clearance
#65Method and device for adjusting a threshold value of a fuel flow rate
#66Method and system for starting up an aircraft turbomachine
#67Method and system for starting up an aircraft turbomachine by real-time regulation of air flow
#68Turbomachine monitoring system and method
#69Turbine Rotor and Blade Assembly with Blind Holes
#70Optical detection of airfoil axial position with NSMS
#71Turbine component cooling with closed looped control of coolant flow
#72Method for mounting a stator blading of a turbomachine, an engine casing and a turbomachine comprising at least one stator blading mounted on this engine casing
#73System and method for predicting turbine rub
#74Turbine blade platform undercut
#75Rotating component of a turbine engine
#76SUPPORT BETWEEN TRANSITION PIECE AND IMPINGEMENT SLEEVE IN COMBUSTOR
#77PRODUCTION METHOD OF IMPELLER APPLIED TO SUPERCHARGER
#78Shell for aircraft turbo-engine stator with mechanical blade load transfer slits
#79Compressor blade root heating system
#80Method and a system for monitoring vibratory phenomena that occur in an aviation gas turbine engine in operation
#81Methods and systems for mitigating distortion of gas turbine shaft
#82High-pressure turbine for turbomachine, associated guide vane sector and aircraft engine
#83Guide vane for a gas turbine
#84Fuel nozzle swirler assembly
#85Managing spool bearing load using variable area flow nozzle
#86Method for determining the remaining service life of a rotor of a thermally loaded turboengine
#87METHOD AND DEVICE FOR IMPLEMENTING SIMULATED TEST OF CENTRIFUGAL STRESS IN TURBINE BLADE
#88Components for gas turbine engines
#89Gas turbine control method and device
#90Gas turbine engine systems and methods involving oil flow management
#91Variable area fan nozzle for accommodating a foreign object strike event
#92Turbomachinery disc
#93COOLED GAS TURBINE GUIDE BLADE FOR A GAS TURBINE, USE OF A GAS TURBINE GUIDE BLADE AND METHOD FOR OPERATING A GAS TURBINE
#94Managing spool bearing load using variable area flow nozzle
#95Operation of an aircraft engine after emergency shutdown
#96Method of operating a gas turbine engine
#97Method for increasing the fatigue life of a blade root of a turbomachine blade
#98Systems and methods for detecting undesirable operation of a turbine
#99High cycle fatigue management for gas turbine engines
#100Approach to extending life of gas turbine engine
#101Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine
#102System and method for utilization of transmitted digital flight data acquisition information to accomplish vibration balance solutions
#103Approach to extending life of gas turbine engine
#104System and method for turbine engine anomaly detection
#105Approach to extending life of gas turbine engine
#106Approach to extending life of gas turbine engine
#107Thrust reverser system actuator having an integral torque limiter
#108Core turning system
#109Bowed rotor prevention system