145447 ⎘
Geometry; Three-dimensional helical
HYDRAULICALLY DRIVEN DE-OILER FOR GAS TURBINE ENGINES
#2Heat Engine
#3ROTOR BLADE SYSTEM FOR TURBINE ENGINES
#4SYSTEM FOR COOLING A REFRIGERANT FOR AN AIRCRAFT COMPRISING A SAFETY HEATING DEVICE AND METHOD FOR USING SUCH A SYSTEM
#5Airfoil assembly with an internal reinforcement structure
#6Cooling for detonation engines
#7Cooling for surface ignitors in torch ignition devices
#8Turbine engine inducer assembly
#9TURBINE COMPONENT WITH A THIN INTERIOR PARTITION
#10Fiber-reinforced aircraft component and aircraft comprising same
#11De-icing device for an air intake of an aircraft turbojet engine nacelle
#12Turbocharger, having a steel material for high-temperature applications
#13Alternating helicoid cell structure and methods of producing the same
#14Screw systems
#15Rotary machine with cooling jacket including helical groove
#16SPACE PROPULSION SYSTEM
#17Turbine engine inducer assembly
#18System for a combined turbine and bearing case for a turbocharger
#19Fiber-reinforced aircraft component and aircraft comprising same
#20Flow mixer duct for a bleed system
#21Fan cover
#22Spiraling grooves as a hub treatment for cantilevered stators in compressors
#23Diffuser-deswirler for a gas turbine engine
#24Abrasive flow machining method and article
#25Turbine with internal blades
#26Disc turbine with static distributor
#27Screw systems
#28GAS TURBINE ENGINE COMPONENT COOLING CAVITY WITH VORTEX PROMOTING FEATURES
#29Self-pumping fuel injector for a gas turbine engine and method of operation
#30Spiral cavities for gas turbine engine components
#31Turbine component with a thin interior partition
#32Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air
#33Power-generation Gas Turbine with Plasma-assisted Combustion Using Multiple Resonators and a Directed Flame Path
#34Flowmeter with discontinuous helicoid turbine
#35Duct assembly including helicoidal structure and gas turbine combustor including the same
#36Intershaft seal assembly with multi-axis stepped grooves
#37Jet engine with deflector
#38HELICAL SKIN COOLING PASSAGES FOR TURBINE AIRFOILS
#39Transmission mechanism comprising a coupling member, turbomachine equipped with such a mechanism and operating method of said mechanism
#40Centrifugal compressor and turbocharger
#41Coil spring hanger for exhaust duct liner
#42Turbine engine duct
#43Diffuser-deswirler for a gas turbine engine
#44System and method for system and method for a turbomachine multiphase hyrdrocarbon pump having an auger coupling
#45Arrangement for a gas turbine combustion engine
#46Turbine engine inducer assembly
#47Turbine engine components with cooling features
#48Cooling structure for a turbine component
#49Flow limiter
#50Solid rocket motor with vortex inducing feature
#51Rotor disc with passages
#52Gyratory-effect flow deflector of a discharge valve system, discharge valve system and turbine engine comprising such a discharge valve system
#53Gas turbine engine with a geared turbofan arrangement
#54Biomimetic airfoil bodies and methods of designing and making same
#55System and method for a multiphase hydrocarbon pump having an auger coupling
#56Method and system for rotating air seal with integral flexible heat shield
#57Abrasive flow machining method
#58Turbomachine including clearance control system
#59Acoustic attenuation panel for a turbojet engine nacelle
#60Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil
#61Anti-coking liquid fuel injector assembly for a combustor
#62Baffle insert for a gas turbine engine component and method of cooling
#63Gas turbine engine component with a baffle insert
#64Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine
#65Sealing assembly
#66Reversible spiral groove journal bearing for use on standard and reverse rotation turbochargers
#67Staggered crossovers for airfoils
#68Damper pin for a turbine blade
#69Catalyst chamber with a catalyst bed embedded therein for a monopropellant thruster of a rocket engine
#70Component manufacture
#71Movable vane control system
#72Self-pumping fuel injector for a gas turbine engine and method of operation
#73Intermittent grooved soft abradable material to reduce blade tip temperature
#74Gas turbine engine component cooling cavity with vortex promoting features
#75Turbine case coupling
#76Particle separating fluid intake
#77ROTATION BODY OF NOZZLE FOR REACTION-TYPE STEAM TURBINE
#78Tortuous cooling passageway for engine component
#79Pedestals with heat transfer augmenter
#80Turbomachine accessory gearbox equipped with an air/oil separator
#81Heat exchanger having a coaxial or concentric tube construction
#82Turbine blade cooling structure
#83Fuel reformer chamber with tubular mesh insert supporting a catalyst
#84Gas turbine engine component cooling channels
#85Airfoil cooling device and method of manufacture
#86Variable dual spring blade root support for gas turbines
#87Turbocharger shaft seal
#88Multi-orifice plate for cooling flow control in vane cooling passage
#89Jet engine with deflector
#90Fan casing arrangement for a gas turbine engine and related method
#91Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans
#92Helical seal system for a turbomachine
#93Gas turbine exhaust diffuser with helical turbulator
#94Gas turbine combustor exit piece with hinged connections
#95Fan containment system
#96Method for manufacturing an oxide/oxide composite material turbomachine blade provided with internal channels
#97Aerofoil cooling
#98Damper pin
#99Coil spring hanger for exhaust duct liner
#100SYSTEMS AND METHODS FOR PROCESSING INLET AIR
#101Jet engine with deflector
#102Jet engine deflector
#103Helical cross flow (HCF) pulse detonation engine
#104Non-combustion energy source and configuration for brayton cycle heat engines
#105Gas Turbine Pattern Swirl Film Cooling
#106Turbine engine gearbox
#107FIBER COMPOSITE ASSEMBLY AND PROCESS OF FABRICATING A FIBER COMPOSITE ASSEMBLY
#108Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping
#109Energy-absorbing fan case for a gas turbine engine
#110DESIGN AND SHAPE FOR PULSE CARTRIDGES TO ALLOW HYDROPHOBIC MEDIA TO DRAIN AND GENERALLY INCREASE WORKING SURFACE AREA
#111Fan case thrust reverser
#112Support assembly for transition duct in turbine system
#113FLOW MIXER
#114Turbine blade with mate face cooling air flow
#115Damper pin
#116Belted toroid pressure vessel and method for making the same
#117System and method of combustion for sustaining a continuous detonation wave with transient plasma
#118Spiral wound bound seal
#119Cooled turbine blades for a gas-turbine engine
#120Endwall component for a turbine stage of a gas turbine engine
#121Helical inner diameter groove journal bearing
#122Gas-turbine exhaust cone
#123Inlet air filtration system
#124FIRESEAL
#125Turbomachine
#126Helical inner diameter groove journal bearing
#127HYBRID RAM AIR TURBINE WITH INLET GUIDE VANES
#128Helical cross flow (HCF) pulse detonation engine
#129Film-cooling augmentation device and turbine airfoil incorporating the same
#130Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel
#131COOLING APPARATUS FOR COMBUSTOR TRANSITION PIECE
#132Heat exchanging hollow passages with helicoidal grooves
#133Cooling arrangement
#134Airfoil with cooling passage providing variable heat transfer rate
#135Spiral cooled fuel nozzle
#136Transition with a linear flow path for use in a gas turbine engine
#137System and method for power production using a hybrid helical detonation device
#138Counter-vortex paired film cooling hole design
#139Heat exchange injector for use in a rocket engine
#140Rotary pressure rise combustor for a gas turbine engine
#141System and method of continuous detonation in a gas turbine engine
#142Turbine blade
#143Apparatus and method for a gas turbine entrainment system
#144Aircraft Propulsion System
#145Solar heat collector, sunlight collecting reflector, sunlight collecting system and solar energy utilization system
#146Fuel distribution apparatus
#147Compact bearing support
#148Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
#149SYSTEM AND METHOD FOR POWER PRODUCTION USING A HYBRID HELICAL DETONATION DEVICE
#150Housing for a centrifugal fan, pump, or turbine
#151Blade mounting
#152Barrier sealing system for centrifugal compressors
#153Enhanced turbine airfoil cooling
#154Hybrid worm gas turbine engine
#155Ultra-compact, high performance aerovortical rocket thruster
#156Fan assembly and method
#157Propulsion system
#158Rotor for jet turbine engine having both insulation and abrasive material coatings
#159Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
#160Fan or compressor casing
#161Outlet nozzle and a method for manufacturing an outlet nozzle
#162Axial flow positive displacement worm gas generator
#163Axial flow positive displacement gas generator with combustion extending into an expansion section
#164Cooled turbine airfoils and methods of manufacture
#165Vortical flow rotor
#166Combustion transition duct providing stage 1 tangential turning for turbine engines
#167Cooled component of a fluid-flow machine, method of casting a cooled component, and a gas turbine
#168Housing for a centrifugal fan, pump, or turbine
#169Support system for transition ducts
#170Turbine component
#171Anti-rotation lock
#172Fan assembly and method
#173Bearing arrangement
#174Exhaust turbocharger
#175Turbulated hole configurations for turbine blades
#176Method of forming a fuel feed passage in the feed arm of a fuel injector
#177Microcircuit cooling for a turbine airfoil
#178Damper element with spring-suspended bearing member for vibration dampening system for turbine blade