136896 ⎘
Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator; Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing; Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
METHODS AND APPARATUS TO CONTROL A SURFACE OF AN AIRCRAFT ENGINE
#2CMC COMPONENT WITH COOLING CAVITY COVER PLATE
#3Control Logic for Thrust Link Whiffle-Tree Hinge Positioning for Improved Clearances
#4COOLING FEATURES FOR A COMPONENT OF A GAS TURBINE ENGINE
#5GAS TURBINE ENGINE HAVING COOLING SYSTEMS
#6VARIABLE FLOWPATH CASINGS FOR BLADE TIP CLEARANCE CONTROL
#7RAPID ACTIVE CLEARANCE CONTROL SYSTEM OF INTER STAGE AND MID-SEALS
#8LIFE AND PERFORMANCE IMPROVEMENT TRENCHES
#9VARIABLE FLOWPATH CASINGS FOR BLADE TIP CLEARANCE CONTROL
#10TURBINE ASSEMBLY WITH CASE-INTEGRATED COOLED CLEARANCE MEASUREMENT SYSTEM
#11Rapid active clearance control system of inter stage and mid-seals
#12ACTIVE CLEARANCE CONTROL ASSEMBLY
#13BLADE TIP CLEARANCE CONTROL USING MATERIAL WITH NEGATIVE THERMAL EXPANSION COEFFICIENTS
#14Ram air driven blade tip clearance control system for turboprop engines
#15METHODS AND APPARATUS TO TARGET ENGINE OPERATING CYCLE CONDITIONS FOR CLEARANCE CONTROL
#16Air seal system with backside abradable layer
#17THERMOELECTRIC GENERATOR FOR A TURBINE ENGINE
#18COOLING FEATURES FOR A COMPONENT OF A GAS TURBINE ENGINE
#19Turbine ring assembly for a turbomachine
#20METHODS AND APPARATUS FOR HEATING MOUNT LUGS
#21Variable flowpath casings for blade tip clearance control
#22ASYMMETRIC HEAT TRANSFER MEMBER FILLET TO DIRECT COOLING FLOW
#23Monitoring device, computer-readable storage medium for storing monitoring program and monitoring method for rotary machine, and rotary machine equipment
#24LOAD ADJUSTMENT METHOD, LOAD ADJUSTMENT DEVICE, AND PROGRAM
#25Active clearance control of fan blade tip closure using a variable sleeve system
#26VARIABLE FLOWPATH CASINGS FOR BLADE TIP CLEARANCE CONTROL
#27Gas turbine engine with a fluid conduit system and a method of operating the same
#28Air seal system with backside abradable layer
#29Containment assembly for an aircraft engine
#30Clearance control system for gas turbine
#31Clearance control for engine performance retention
#32System for controlling blade clearances within a gas turbine engine
#33Gas turbine engine with clearance control system
#34Gas turbine engine with a fluid conduit system and a method of operating the same
#35Turbine assembly, and gas turbine engine provided with such an assembly
#36Electric heating for turbomachinery clearance control powered by hybrid energy storage system
#37Turbine having an internal secondary space equipped with fins for correcting gyration of an airflow
#38Turbine shroud assembly
#39Control method and unit for controlling the clearance of a high-pressure turbine to reduce the effect of EGT overshoot
#40Clearance control assembly
#41HEAT TRANSFER DEVICE, TURBOMACHINE CASING AND RELATED STORAGE MEDIUM
#42Active clearance control system and method for an aircraft engine
#43Throttle mechanism and turbine
#44Control logic for thrust link whiffle-tree hinge positioning for improved clearances
#45Cooling device for a turbomachine casing
#46Steam turbine
#47Device for cooling an outer casing of a turbomachine and turbomachine provided with such a device
#48Heatshield for a gas turbine engine
#49SYSTEM FOR CONTROLLING BLADE CLEARANCES WITHIN A GAS TURBINE ENGINE
#50Turbine clearance control system
#51Turbine casing cooling device for a turbomachine
#52MECHANICALLY DRIVEN AIR VEHICLE THERMAL MANAGEMENT DEVICE
#53TURBINE ENGINE SEALING AND METHOD
#54System and method for modulating airflow into a bore of a rotor to control blade tip clearance
#55Apparatus for controlling turbine blade tip clearance and gas turbine including the same
#56Apparatus for controlling turbine blade tip clearance and gas turbine including the same
#57Cooling device for a turbine of a turbomachine
#58Axial flow turbine with upstream gland and extraction of cooling air
#59GAS TURBINE ENGINE AND OPERATION METHOD
#60Device for cooling a turbomachine housing
#61Valve assembly for an active clearance control system
#62Gas turbine engine flowpath component including vectored cooling flow holes
#63Heat transfer coefficients in a compressor case for improved tip clearance control system
#64Cooling device for a turbine of a turbomachine
#65Cooling device for a turbine of a turbomachine
#66Turbine shroud assembly with flange mounted ceramic matrix composite turbine shroud ring
#67TURBINE TIP SHROUD ASSEMBLY WITH PLURAL SHROUD SEGMENTS HAVING INTERNAL COOLING PASSAGES
#68CONTROL METHOD AND SYSTEM IN A HYBRID-ELECTRICAL AIRCRAFT PROPULSION SYSTEM
#69Negative thermal expansion compressor case for improved tip clearance
#70Panel for tip clearance control
#71Gas turbine and method for blade ring production method
#72Method for controlling a clearance control valve during a step-climb in cruise phase
#73Modulated turbine component cooling
#74Containment case active clearance control structure
#75Method and control unit for controlling the play of a high-pressure turbine
#76Gas turbine induction system, corresponding induction heater and method for inductively heating a component
#77Control of clearance between aircraft rotor blades and a casing
#78Electric heating for turbomachinery clearance control powered by hybrid energy storage system
#79Cooled cooling air for blade air seal through outer chamber
#80Active multi-effector control of high pressure turbine clearances
#81Device and method for cooling a low pressure turbine in a turbomachine
#82Mission adaptive clearance control system and method of operation
#83Method and device for measuring the flow rate of cooling air in a turbomachine casing
#84Anti-icing system for a gas turbine
#85Method and device for adjusting the clearance between a rotor and a concentric stator of an aircraft turbine engine
#86Gas turbine engine and method to cool a gas turbine engine case assembly
#87Device for holding a cooling tube for a turbomachine casing
#88Tip clearance control system
#89Turbine stator blade
#90Compressor case clearance control logic
#91Gas turbine engine and cooling air configuration for turbine section thereof
#92Blade outer air seal fin cooling assembly and method
#93Containment case active clearance control structure
#94TURBINE-TIP CLEARANCE CONTROL SYSTEM OFFTAKE
#95Turbine shroud segment with side perimeter seal
#96Method of regulating air pressure in anti-icing system
#97Turbine shroud block segment with near surface cooling channels
#98Passive clearance control for a centrifugal impeller shroud
#99BOAS thermal protection
#100Shroud for gas turbine engine
#101BLADE OUTER AIR SEAL WITH COOLED NON-SYMMETRIC CURVED TEETH
#102Method for controlling a turbomachine valve
#103Ceramic matrix composite blade track assembly with tip clearance control
#104Hybrid electric aircraft propulsion system
#105Electric heating for turbomachinery clearance control powered by hybrid energy storage system
#106Electric heating for turbomachinery clearance control
#107Dual response blade track system
#108Impeller shroud with thermal actuator for clearance control in a centrifugal compressor
#109Double bore basket
#110Active tip clearance control system for gas turbine engine
#111Cooling device for a turbine of a turbomachine
#112TURBINE ENGINE WITH CLEARANCE CONTROL SYSTEM
#113Gas turbine engine offtake
#114Turbine engine air control valve
#115Cooling arrangement for a turbine casing of a gas turbine engine
#116ACTIVE CLEARANCE CONTROL COOLING AIR RAIL WITH FINGERS
#117Impeller shroud with closed form refrigeration system for clearance control in a centrifugal compressor
#118System and method of controlling tip clearance in a shroud assembly for a bladed disc
#119Housing for a gas turbine compressor
#120Device for cooling a turbine casing with air jets
#121Method of clearance control for an interdigitated turbine engine
#122Gas turbine engine active clearance control system using inlet particle separator
#123ACTIVE CLEARANCE CONTROL SYSTEM FOR GAS TURBINE ENGINE WITH POWER TURBINE
#124Active clearance control system and manifold for gas turbine engine
#125TURBINE CLEARANCE CONTROL SYSTEM AND METHOD FOR IMPROVED VARIABLE CYCLE GAS TURBINE ENGINE FUEL BURN
#126Variable area turbine arrangement with secondary flow modulation
#127Gas turbine engine with diversion pathway and semi-dimensional mass flow control
#128Gas turbine engine with rotor tip clearance control system
#129Active clearance control for gas turbine engine
#130Assembly for a spreader connection between a turbine casing and a turbine engine ring element
#131Turbine tip shroud assembly with plural shroud segments having internal cooling passages
#132Plenum for cooling turbine flowpath components and blades
#133Resilient mounting assembly for a turbine engine
#134Turbomachine including a cooling and turbine clearance control system having an air supply scoop
#135Tip clearance control with variable speed blower
#136Cooling and insulating manifold seal assembly for a propulsion system
#137COOLING SYSTEM AND COOLING METHOD IN A GAS TURBINE
#138Clearance control arrangement
#139CLEARANCE CONTROL ARRANGEMENT
#140Gas turbine and component-temperature adjustment method therefor
#141Tip clearance control for turbine blades
#142Tip clearance control for gas turbine engine
#143Re-use and modulated cooling from tip clearance control system for gas turbine engine
#144Turbine engine turbine assembly
#145Flow diverter case attachment for gas turbine engine
#146Vane cooling system
#147Cooled cooling air for blade air seal through outer chamber
#148High temperature disk conditioning system
#149Device for ventilation of a turbomachine turbine casing
#150Adaptive active clearance control logic
#151Downhole turbine with an adjustable shroud
#152Seal pressurization in box shroud
#153Thrust rating dependent active tip clearance control system
#154Compressor with segmented inner shroud for an axial turbine engine
#155Turbomachine housing element
#156ACTIVE GAP CONTROL FOR TURBINE ENGINE COMPRESSOR
#157Aircraft turbine-engine module casing, comprising a heat pipe associated with a sealing ring surrounding a movable impeller of the module
#158PRESSURE RESPONSIVE VALVE FOR A COOLING FLOW IN A GAS TURBINE
#159Passive tip clearance control with variable temperature flow
#160Controlling tip clearance in a turbine
#161Turbine cooling system
#162Connecting assembly for cooling the turbine of a turbine engine
#163Stator heat shield segment for a gas turbine power plant
#164Turbine ring assembly comprising a cooling air distribution element
#165Turbine ring assembly comprising a cooling air distribution element
#166Turbine ring assembly comprising a cooling air distribution element
#167CONTROLLING TURBINE SHROUD CLEARANCE FOR OPERATION PROTECTION
#168NOISE-MITIGATING TRANSFER DUCT FOR ACTIVE TIP CLEARANCE CONTROL SYSTEM OF GAS TURBINE ENGINE
#169Turbine tip clearance control method and system
#170Fluid flow assembly
#171Active clearance control collector to manifold insert
#172Modulated turbine component cooling
#173Device of a turbomachine for actuating a setting device and turbomachine with such a device
#174Mechanically driven air vehicle thermal management device
#175Centrifugal compressor having a casing with an adjustable clearance and connections for a variable flow rate cooling medium, impeller clearance control apparatus for centrifugal compressor, and impeller clearance control method for centrifugal compressor
#176Method and apparatus for active clearance control on gas turbine engines
#177Nacelle anti ice system
#178Blade track assembly with turbine tip clearance control
#179Tip clearance control system
#180Gas turbine engine and method to cool a gas turbine engine case assembly
#181Impingement insert for a gas turbine engine
#182Passive clearance control system for gas turbomachine
#183Impeller shroud with thermal actuator for clearance control in a centrifugal compressor
#184Turbine blade track assembly
#185Hot gas path component and methods of manufacture
#186Clearance-control-type seal structure
#187TURBINE CLEARANCE CONTROL SYSTEM AND METHOD FOR IMPROVED VARIABLE CYCLE GAS TURBINE ENGINE FUEL BURN
#188Turbomachine including clearance control system
#189Impingement manifold
#190Engine casing with internal coolant flow patterns
#191Annular ring assembly for shroud cooling
#192Gas turbine engine having high pressure compressor case active clearance control system
#193Seal arc segment with sloped circumferential sides
#194COMPRESSOR SYSTEM
#195Active clearance control for a turbine and case
#196Thermal lifting member for blade outer air seal support
#197Gas turbine, combined cycle plant, and activation method of gas turbine
#198Method and apparatus for active clearance control
#199Blade outer air seal with flow guide manifold
#200Active HPC clearance control
#201Stator heat shield for a gas turbine, gas turbine with such a stator heat shield and method of cooling a stator heat shield
#202Turbine shroud with mounted full hoop blade track
#203Full hoop blade track with interstage cooling air
#204Gas turbine engine with health monitoring system
#205Auto thermal valve (ATV) for dual mode passive cooling flow modulation
#206Method and apparatus for active clearance control for high pressure compressors using fan/booster exhaust air
#207Active high pressure compressor clearance control
#208Manifold for use in a clearance control system and method of manufacturing
#209Thermal management system
#210Gas turbine engine turbine cooling system
#211Outer airseal for gas turbine engine
#212Rotor tip clearance
#213Method of operating a clearance control system
#214Blade outer air seal with cooling features
#215Ceramic matrix composite component and process of producing a ceramic matrix composite component
#216System and method for calibrating a case cooling system for a gas turbine engine
#217ACTIVE CLEARANCE CONTROL WITH INTEGRAL DOUBLE WALL HEAT SHIELDING
#218Shroud assembly for a gas turbine engine
#219Shrouds and methods for forming turbine components
#220Turbine engine assembly and method of operating thereof
#221Multi-flow cooling passage chamber for gas turbine engine
#222Actuator control
#223Blade outer air seal fin cooling assembly and method
#224Method for detecting an increase in the rating of a low-pressure turbine of an aircraft reactor during a cruising flight phase, and associated device and method for regulating the cooling air flow rate of a low-pressure turbine
#225System for the active setting of a radial clearance size and aircraft engine with a system for the active setting of a radial clearance size
#226Turbine shroud segment sealing
#227Turbine shroud segment with side perimeter seal
#228Gas turbine cool-down phase operation methods for controlling turbine clearance by adjusting air flow rate
#229Dual pressure deicing system
#230Methods and system for a turbocharger
#231Brackets for gas turbine engine components
#232Flow sleeve for thermal control of a double-walled turbine shell and related method
#233System and method for improving exhaust energy recovery
#234Turbine tip clearance
#235Axial skin core cooling passage for a turbine engine component
#236Gas turbine, gas turbine control device, and gas turbine cooling method
#237Meter plate for blade outer air seal
#238Blade outer air seal cooling passage
#239Adaptive turbomachine cooling system
#240Method, system, and apparatus for reducing a turbine clearance
#241System for cooling a turbine engine
#242System for cooling a turbine shroud
#243Tortuous cooling passageway for engine component
#244BOAS thermal protection
#245CMC turbine components and methods of forming CMC turbine components
#246Active clearance control systems
#247Variable area turbine arrangement with secondary flow modulation
#248Blade outer air seal with cooling holes
#249Gas turbine engine component providing prioritized cooling
#250BOAS with radial load feature
#251Blade track assembly with turbine tip clearance control
#252Shroud assembly for a turbine engine
#253TURBINE COOLING APPARATUS
#254Hot gas path component
#255Tip clearance control for turbine blades
#256Tip clearance control for turbine blades
#257Turbine blade tip clearance control
#258Air guiding device and turbo engine with air guiding device
#259Gas turbine comprising a compressor casing with an inlet opening for tempering the compressor casing and use of the gas turbine
#260Gas turbine engine flow control device
#261Systems and methods for controlling rotor to stator clearances in a steam turbine
#262Turbo machine and method for operating such turbo machine
#263System and method for blade tip clearance control
#264Self-modulated cooling on turbine components
#265Radial position control of case supported structure with axial reaction member
#266High temperature disk conditioning system
#267Annular ring assembly for shroud cooling
#268Cooled composite sheets for a gas turbine
#269Turbine case cooling system
#270Cooling device for the casing of an aircraft jet engine comprising a supporting device
#271Edge treatment for gas turbine engine component
#272Gas turbine engine spring mounted manifold
#273Gas turbine and operating method thereof
#274Gas turbine and operating method thereof
#275Gas turbine and operating method thereof
#276Suction-based active clearance control system
#277Hybrid passive and active tip clearance system
#278Acoustic treatment to mitigate fan noise
#279Apparatus and system for compressor clearance control
#280Holding device of a cooling tube for a turbojet casing
#281Active clearance control for gas turbine engine
#282Distributor device for cooling air within an engine
#283Turbine casing made of two materials
#284Rotor blade tip clearance control
#285Blade outer air seal with cored passages
#286Method and apparatus for clearance control utilizing fuel heating
#287Flow guiding system and rotary combustion engine
#288System and method for active clearance control
#289Turbine rotor blades with platform cooling arrangements
#290Layered arrangement, hot-gas path component, and process of producing a layered arrangement
#291Seal for a rotary machine
#292System and method for turbine blade clearance control
#293Ceramic matrix composite component and method of forming thereof
#294Stator casing cooling system
#295Gas turbine engine turbine blade tip active clearance control system and method
#296Re-use of internal cooling by medium in turbine hot gas path components
#297Method and system for passive clearance control in a gas turbine engine
#298Passive cooling system for control valve actuators within a negative pressure turbine enclosure using ambient cooling air
#299Disc axis adjusting mechanism in gas turbine
#300Clearance control system for a rotary machine and method of controlling a clearance