136961 ⎘
Component parts, details, or accessories, not provided for in, or of interest apart from, other groups Cooling ; Heating; Heat-insulation
Sub-classes:METHODS AND APPARATUS TO DETERMINE ENGINE STATUS WITH PLENUM MEASUREMENTS
#2LIGHT EMITTING FAN
#3TURBOCHARGER
#4METHODS AND APPARATUS TO DETERMINE ENGINE STATUS WITH PLENUM MEASUREMENTS
#5THERMAL ENERGY SYSTEM TO MINIMIZE OR ELIMINATE ROTOR BOW
#6Vortex restart structures for turbulated passages
#7Light emitting fan
#8CONTINUOUS FLOW ENGINE SKID COMPONENT SYSTEM
#9PROTECTIVE HEAT SHIELD ENCLOSURE FOR TURBOCHARGED ENGINES
#10Turbocharger including an actuator housing with a through hole
#11PRE-CERAMIC THERMAL BARRIER FOR GAS TURBINE ENGINE COMPONENTS
#12COOLING AIR FOR GAS TURBINE ENGINE WITH THERMALLY ISOLATED COOLING AIR DELIVERY
#13GUIDING ARRAY
#14Reactive thermal barrier coating
#15Turbine component with heated structure to reduce thermal stress
#16Heat transfer system for gas turbine engine
#17Turbine for a turbine engine comprising heat-shielding foils
#18Heat-protection element for a bearing chamber of a gas turbine
#19Methods and systems for a turbo shield
#20Flange cooling structure for gas turbine engine
#21Environmental barrier coating with porous bond coat layer
#22Cooling air for gas turbine engine with thermally isolated cooling air delivery
#23Gas turbine engine forward bearing compartment architecture
#24Concentrated Solar Thermal Reactor
#25Power generation system and method to generate power by operation of such power generation system
#26Rapid processing of laminar composite components
#27Low nitrogen coupling combustion system for the disposal of waste stink gas and solid waste
#28Systems and methods for controlling temperature in a supporting foundation used with a gas turbine engine
#29Methods and materials for repairing a thermal barrier coating of a gas turbine component
#30OGV electroformed heat exchangers
#31Gas turbine engine forward bearing compartment architecture
#32Environmental barrier coating with porous bond coat layer
#33Restoration coating system and method
#34Device for cooling a component of a gas turbine/turbo machine by means of impingement cooling
#35Enhanced adhesion thermal barrier coating
#36Heat exchanger with stacked flow channel modules
#37Method for producing a surface layer on a ceramic matrix composite
#38Turbomachinery heat management system
#39Airfoils and core assemblies for gas turbine engines and methods of manufacture
#40Reactive thermal barrier coating
#41Rapid processing of laminar composite components
#42Air-oil heat exchanger
#43Feather seals with leakage metering
#44Turbocharger with variable-nozzle cartridge, including resilient heat shield assembly to locate the cartridge axially
#45Turbocharger
#46Gas turbine engine forward bearing compartment architecture
#47Gas turbine components and methods of assembling the same
#48Air-film cooled component for a gas turbine engine
#49Cooling air for gas turbine engine with thermally isolated cooling air delivery
#50One-piece combustion chamber
#51Mini-disk for gas turbine engine
#52Method of regulating air pressure in anti-icing system
#53Sealing ring assembly
#54THERMAL-SPRAYED BONDING OF A CERAMIC STRUCTURE TO A SUBSTRATE
#55THREE-DIMENSIONAL METAL INSULATING PART
#56Silicon-Based Materials Containing Indium and Methods of Forming the Same
#57Heat exchange module for a turbine engine
#58Monitoring device, method for monitoring target device, and program
#59Closed circuit functioning according to a Rankine cycle with a device for the emergency stopping of the circuit, and method using such a circuit
#60TURBINE ENGINE WITH CLEARANCE CONTROL SYSTEM
#61GAS TURBINE INCLUDING EXTERNAL COOLING SYSTEM AND METHOD OF COOLING THE SAME
#62Thermal insulation coating member, axial flow turbine, and method for producing thermal insulation coating member
#63Airfoil for a gas turbine engine having insulating materials
#64OGV electroformed heat exchangers
#65Multilayer Encapsulated Heat Shield for a Turbocharger
#66Methods for forming vertically cracked thermal barrier coatings and articles including vertically cracked thermal barrier coatings
#67Multi-source turbine cooling air
#68Process for producing a thermal barrier in a multilayer system for protecting a metal part and part equipped with such a protective system
#69Device for cooling a turbine casing with air jets
#70Gas turbine engine cooling air manifolds with spoolies
#71Casing Of A Turbocharger And Turbocharger
#72Plasma device and method for delivery of plasma and spray material at extended locations from an anode arc root attachment
#73Cooling device for casing support part of rotary machine, rotary machine, and cooling method for casing support part of rotary machine
#74Boas segmented heat shield
#75Method of forming a hole in a coated component
#76Flow metering and retention system
#77Aircraft incorporating a thrust recovery system using cabin air
#78BLADE-DISC ARRANGEMENT FOR A TURBOMACHINE
#79Manufacturing a heat exchanger using a material buildup process
#80Slotted ceramic coatings for improved CMAS resistance and methods of forming the same
#81Turbocharger
#82Platform cooling arrangement in a turbine rotor blade
#83Gas turbine engine component having vascular engineered lattice structure
#84VARIABLE VANE SEGMENT
#85Turbine shroud assembly with multi-piece seals
#86Insulated seal seat
#87Engine shaft assembly and method
#88Gas turbine engine forward bearing compartment architecture
#89Gas turbine engine forward bearing compartment architecture
#90Silicon-based materials containing indium and methods of forming the same
#91Components having channels for impingement cooling
#92Lubrication system for a turbine engine
#93Gas turbine engine lubrication system
#94Gas turbine engine forward bearing compartment architecture
#95Airfoil with geometrically segmented coating section
#96AIRFOIL WITH LEADING END HOLLOW PANEL
#97APPARATUS AND METHOD FOR PROVIDING FLUID TO A BEARING DAMPER
#98Turbine airfoil trailing edge coolant passage created by cover
#99Silicon-based materials containing indium and methods of forming the same
#100Apparatus and process of retrofitting a combined cycle power plant
#101Air-film cooled component for a gas turbine engine
#102Vane segment for a gas turbine
#103Exhaust gas turbocharger
#104Nacelle anti ice system
#105Mini-disk for gas turbine engine
#106REFRACTORY METAL CORE AND COMPONENTS FORMED THEREBY
#107HIGH TEMPERATURE COATING FOR SILICON NITRIDE ARTICLES
#108Centrifugal compressors with integrated intercooling
#109Methods and articles relating to ionic liquid bath plating of aluminum-containing layers utilizing shaped consumable aluminum anodes
#110Heat shield
#111COMPONENT FOR A TURBINE ENGINE WITH A FILM-HOLE
#112TURBOMACHINE COMPONENT, PARTICULARLY A GAS TURBINE ENGINE COMPONENT, WITH A COOLED WALL AND A METHOD OF MANUFACTURING
#113Compressed air, utility-scale, non-polluting energy storage and nuclear reactor emergency cooling system using thermal power plant waste heat
#114Shield member and jet engine using the same
#115Boas segmented heat shield
#116Firewall mount hub
#117Apparatus, turbine nozzle and turbine shroud
#118Cooled turbine vane platform comprising forward, midchord and aft cooling chambers in the platform
#119ENGINE COMPONENT ASSEMBLY
#120COMPRESSED AIR, UTILITY-SCALE, NON-POLLUTING ENERGY STORAGE AND NUCLEAR REACTOR EMERGENCY COOLING SYSTEM USING THERMAL POWER PLANT WASTE HEAT
#121Multi-source turbine cooling air
#122Baffle insert for a gas turbine engine component and method of cooling
#123Enhanced adhesion thermal barrier coating
#124Thermal barrier coatings and methods
#125Heat exchange module for a turbine engine
#126Wheel space purge flow mixing chamber
#127Nozzle for a gas turbine engine
#128Gas turbine engine with a transition duct and corresponding method of manufacturing a transition duct
#129Turbine engine advanced cooling system
#130Turbine engine assembly and method of assembling the same
#131TURBOENGINE COMPONENT AND METHODS FOR ASSEMBLING AND RECONDITIONING A TURBOENGINE COMPONENT
#132Gas turbine rotor cover
#133Gas turbine engine cooling air manifolds with spoolies
#134Turbine shroud assembly
#135Nozzle guide vane with composite heat shield
#136Dual pressure deicing system
#137Heat shield for a vane assembly of a gas turbine engine
#138Flow sleeve for thermal control of a double-walled turbine shell and related method
#139Lubrication system for a turbine engine
#140Rotor disk having a centripetal air collection device, compressor comprising said disc and turbomachine with such a compressor
#141System for thermally shielding a portion of a gas turbine shroud assembly
#142System for thermally isolating a turbine shroud
#143System and method for improving exhaust energy recovery
#144Reflective coating for components
#145Method of recycling energy in process of butadiene preparation
#146Method of depositing abradable coatings under polymer gels
#147ATTACHMENT ASSEMBLY FOR HEAT-SHIELD ARRANGEMENT
#148Sheet-metal turbine housing
#149Turbocharger turbine containment structure
#150Integral metering feature, systems and methods
#151Gas turbine engine component with vascular cooling scheme
#152Methods of manufacturing and cleaning
#153A COMPONENT FOR A TURBOMACHINE AND A METHOD FOR CONSTRUCTION OF THE COMPONENT
#154Integrally bladed rotor having axial arm and pocket
#155Clutch assembly with integrated surface cooling
#156Turbine component surface treatment processes and systems
#157Rotating blade for a gas turbine
#158Gas turbine engine forward bearing compartment architecture
#159Transportable modular coating systems and methods
#160Device and method for separating dirt particles from the working medium of a turbine
#161GAS TURBINE AND HEAT SHIELD FOR A GAS TURBINE
#162ENGINE CASING ELEMENT
#163Supply duct for cooling air from gas turbine compressor
#164Heatshield assembly with double lap joint for a gas turbine engine
#165High pressure compressor rotor thermal conditioning using outer diameter gas extraction
#166Thermal-sprayed bonding of a ceramic structure to a substrate
#167Corrugated mid-turbine frame thermal radiation shield
#168Partially coated blade
#169Diffuser case strut for a turbine engine
#170Heatshield discourager seal for a gas turbine engine
#171Intermediate casing for a turbofan engine
#172Exhaust system having a flow path liner supported by structural duct segments
#173Interlocking rotor assembly with thermal shield
#174TURBOCHARGER INTERNAL TURBINE HEAT SHIELD HAVING AXIAL FLOW TURNING VANES
#175Gas turbine engine component having curved turbulator
#176Multi-circuit lubrication system for a turbine engine
#177Duct arrangement for an internal combustion engine
#178Gas turbine engine component having vascular engineered lattice structure
#179Gas turbine engine component having vascular engineered lattice structure
#180Gas turbine engine component having vascular engineered lattice structure
#181Variable vane segment
#182Vane segment for a gas turbine coated with a MCrAlY coating and TBC patches
#183Insulating coating to permit higher operating temperatures
#184Generator with controlled air cooling amplifier
#185Cooling system with a bearing compartment bypass
#186Rotor-stator assembly for a gas turbine engine
#187Buffer airflow to bearing compartment
#188Gas turbine including sealing band and anti-rotation device
#189Gas turbine engine lubrication system
#190Gas turbine engine with a fire wall and an off-take device
#191Device for connecting a fixed portion of a turbine engine and a distributor foot of a turbine engine turbine
#192Low thermal mass joint
#193Steam turbine facility and method of operating the same
#194Axial flow machine cooling system
#195MANUFACTURING METHOD FOR STRUT SHIELD COLLAR OF GAS TURBINE EXHAUST DIFFUSER
#196Gas turbine engine component having foam core and composite skin with cooling slot
#197Exhaust-gas turbocharger having heat throttle cavity
#198Flow sleeve for thermal control of a double-wall turbine shell and related method
#199COOLED TURBINE RING SEGMENTS WITH INTERMEDIATE PRESSURE PLENUMS
#200Calcium-magnesium-aluminosilicate resistant coating and process of forming a calcium-magnesium-aluminosilicate resistant coating
#201Turbine engine temperature control system with heating element for a gas turbine engine
#202Trenched cooling hole arrangement for a ceramic matrix composite vane
#203Gas turbine engine lubrication system
#204Compressor air provided to combustion chamber plenum and turbine guide vane
#205Aeroengine sealing arrangement
#206Gas turbine engine end-wall component
#207Inlet bleed heat system with integrated air knife/silencer panels
#208Gas Turbine Engine With Inlet Particle Separator and Thermal Management
#209Part load performance improvement using deformable bore plugs
#210Germanate-containing thermal barrier coating
#211Annular turbomachine seal and heat shield
#212Assembly comprising a protection device and a turbine machine element for protecting
#213METHOD OF APPLICATION FOR LAYERED THERMAL BARRIER COATING WITH BLENDED TRANSITION
#214Method for operating a solar installation
#215Corrugated mid-turbine frame thermal radiation shield
#216Wireless component and methods of fabricating a coated component using multiple types of fillers
#217Process for producing a thermal barrier in a multilayer system for protecting a metal part and part equipped with such a protective system
#218Turbine cooling apparatus
#219COVER HUB WITH SEALING RING
#220Impingement cooling system for use with contoured surfaces
#221TURBINE COOLING SYSTEM
#222Turbine to operate at part-load
#223Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system
#224Gas turbine engine with outer case ambient external cooling system
#225Segmented thermally insulating coating
#226Gas turbine engine lockout reduction
#227Insulator, and stator and motor provided with same
#228Gas turbine engine exhaust nozzle cooling valve
#229Structural cooling fluid tube for supporting a turbine component and supplying cooling fluid to transition section
#230Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg
#231Layered thermal barrier coating with blended transition and method of application
#232Compressor rotor
#233Coated gas turbine components
#234Flade duct turbine cooling and power and thermal management
#235Controller, for use in a power plant having a liquid cooling system and an air cooling system
#236Component and methods of fabricating a coated component using multiple types of fillers
#237Apparatus for distributing fluid into a gas turbine
#238System and method for removing heat from a turbomachine
#239Gas turbine power plant with flue gas recirculation and oxygen-depleted cooling gas
#240Aircraft fuel system cooling flow device
#241Cross-over purge flow system for a turbomachine wheel member
#242INTEGRATION OF A SURFACE HEAT-EXCHANGER WITH REGULATED AIR FLOW IN AN AIRPLANE ENGINE
#243Gas turbine engine and cooling system
#244Fluid impingement arrangement
#245Flow path for steam turbine outer casing and flow barrier apparatus
#246Rotating machine
#247INTERDEPENDENT LUBRICATION SYSTEMS
#248Air-oil heat exchanger
#249Air bleed having an inertial filter in the tandem rotor of a compressor
#250LANDFILL GAS UTILIZATION
#251Layered thermal barrier coating with blended transition
#252METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED USING THIS METHOD
#253TURBINE ALIGNMENT CONTROL SYSTEM AND METHOD
#254Preferential cooling of gas turbine nozzles
#255ACCELERATED COOLING OF A GAS TURBINE
#256METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED ACCORDING TO THIS METHOD
#257Aircraft gas turbine engine
#258Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method
#259SYSTEM FOR REGULATING A COOLING FLUID WITHIN A TURBOMACHINE
#260HEAT RECOVERY SYSTEM
#261Method and apparatus for double flow turbine first stage cooling
#262Turbine cooling system
#263Gas turbine engine component cooling scheme
#264Guide vane for a gas turbine
#265Gas turbine engine component cooling scheme
#266Method and apparatus for turbine engines
#267Heat transfer system and method for turbine engine using heat pipes
#268Apparatus, methods, and/or systems relating to the delivery of a fluid through a passageway
#269Heat exchanger to cool turbine air cooling flow
#270Steam turbine and method of cooling steam turbine
#271Aircraft conduit
#272Heat Exchange System In A Turbomachine
#273Duplex turbine shroud
#274Extended impingement cooling device and method
#275Disk spring for a turbocharger
#276Casing and gas turbine
#277Pane arrangement for a turbocharger
#278Gas turbine engine component cooling scheme
#279Heat transfer system for turbine engine using heat pipes
#280Exhaust-gas-turbine casing
#281Interdependent lubrication systems in a turbine engine
#282Air-oil heat exchanger
#283Component with thermal barrier coating and erosion-resistant layer
#284Methods and apparatus for double flow turbine first stage cooling
#285System for actively controlling compressor clearances
#286Device for lubricating a component in a turbomachine
#287Methods and apparatus for coupling ceramic matrix composite turbine components
#288Extended impingement cooling device and method
#289Methods and apparatus for cooling gas turbine engine rotor assemblies
#290High temperature splash plate for temperature reduction by optical reflection and process for manufacturing
#291Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
#292Integral cooling system for turbine casing and guide vanes in aeroengine
#293Housing for bearing cavity in a gas turbine engine