145604 ⎘
Function; Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
Turbine Rotor and Blade Assembly with Blind Holes
#302Airfoil cover system
#303Turbine blade support
#304Shaft with shoulder and groove
#305SYSTEM AND METHOD FOR COUPLING ROTOR COMPONENTS WITH A SPLINE JOINT
#306COMBUSTOR AND METHOD FOR REDUCING THERMAL STRESSES IN A COMBUSTOR
#307Stress relieving slots for turbine vane ring
#308Housing-side structure of a turbomachine
#309Energy absorbent fan blade spacer
#310Exhaust gas housing for a gas turbine and gas turbine having an exhaust gas housing
#311Lateral turbojet improved in order to limit the deformation thereof
#312Gas turbine engine comprising a tension stud
#313Fan hub design
#314Rotating vane seal with cooling air passages
#315Shaft assembly for a gas turbine engine
#316Blade
#317Interface element between a blade root and a blade root housing of a turbine disc, and turbine rotor comprising an interface element
#318Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg
#319Gas duct for a gas turbine and gas turbine having such a gas duct
#320Turbocharger
#321Turbine blade pocket pin stress relief
#322Bearing surface combined load-lock slots for tangential rotors
#323Radial turbine backface curvature stress reduction
#324Scallop curvature for radial turbine wheel
#325Turbine rotor blade
#326Integrally bladed rotor with slotted outer rim
#327Variable geometry turbocharger lower vane ring retaining system
#328DAMAGE TOLERANCE OF A ROTOR ASSEMBLY
#329Cooled airfoil in a turbine engine
#330Compressor having blade tip features
#331Methods for controlling friction between heterogeneous contact surfaces
#332Power plant
#333ROTOR OF ROTARY MACHINE AND ROTARY MACHINE
#334Turbomachine component
#335Cooling of a gas turbine component designed as a rotor disk or turbine blade
#336SUPPORT BETWEEN TRANSITION PIECE AND IMPINGEMENT SLEEVE IN COMBUSTOR
#337Turbine blade, turbine shaft, turbine system and method for installing the turbine blade
#338Turbine rotor
#339Structure for gas turbine casing
#340Gas turbine assembly and method therefor
#341STEAM TURBINE VALVE HAVING INTEGRAL PRESSURE CHAMBER
#342Shell for aircraft turbo-engine stator with mechanical blade load transfer slits
#343Composite turbomachine blade
#344Turbine nozzles and methods of manufacturing the same
#345Turbine shroud
#346Ceramic coating systems and methods
#347Sealing apparatus at the blade shaft of a rotor stage of an axial turbomachine
#348GUIDE VANE FOR A GAS TURBINE
#349Ceramic gas turbine shroud
#350Bolt and manufacturing method of bolt
#351Gas turbine engine and frame
#352Seal for a platform in the rotor of a turbine engine
#353Anti-rotation slot for turbine vane
#354Strain tolerant bound structure for a gas turbine engine
#355Outlet guide vane structure
#356Integrally bladed rotor with slotted outer rim
#357Turbine blade structure
#358THERMAL MACHINE
#359Rotor for an axial-throughflow turbomachine and moving blade for such a rotor
#360Gas turbine engine thermal expansion joint
#361Turbine blade
#362Fuel nozzle swirler assembly
#363Turbine vane for a stationary gas turbine
#364Gas turbine combustor exit duct and hp vane interface
#365Turbine nozzle assembly including radially-compliant spring member for gas turbine engine
#366Structure of radial turbine scroll
#367Connection structure of exhaust chamber, support structure of turbine, and gas turbine
#368GAS TURBINE, DISK, AND METHOD FOR FORMING RADIAL PASSAGE OF DISK
#369Method and apparatus for providing rotor discs
#370Low stress circumferential dovetail attachment for rotor blades
#371Turbine disk and gas turbine
#372UNLOADED SPEED CONTROL FOR AVAILABILITY IMPROVEMENTS TO HEAVY FUEL FIRED GAS TURBINES
#373AVAILABILITY IMPROVEMENTS TO HEAVY FUEL FIRED GAS TURBINES
#374Turbine shroud ring with rotation proofing recess
#375Gas turbine combustor exit duct and HP vane interface
#376Method and apparatus for pre-spinning rotor forgings
#377Method for producing a turbine housing and turbine housing
#378THERMALLY BALANCED AERO STRUCTURES
#379THERMALLY BALANCED MATERIALS
#380Control of case wall growth during repair and method
#381Structural attachment system for transition duct outlet
#382Replacement of part of engine case with dissimilar material
#383Methods and apparatus for reducing nozzle stress
#384Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine blade
#385Vane with reduced stress
#386Method and system for cooling engine components
#387METHOD OF MANUFACTURING A VANE WITH REDUCED STRESS
#388TURBINE ROTOR BLADE AND FIXATION STRUCTURE THEREOF
#389Bearing support structure for turbine
#390Stator vane assembly
#391Turbine nozzle for a gas turbine engine
#392Turbine bucket for a turbomachine and method of reducing bow wave effects at a turbine bucket
#393Turbine vane of a gas turbine
#394Variable geometry turbocharger lower vane ring retaining system
#395Exhaust-driven turbocharger for a motor vehicle
#396AXIAL BLADE SLOT PRESSURE FACE WITH UNDERCUT
#397Method and apparatus for supporting rotor assemblies during unbalances
#398Reduced weight blade for a gas turbine engine
#399Method and system for supporting stator components
#400Diaphragm and blades for turbomachinery
#401Turbomachine blade
#402Turbine bucket shroud internal core profile
#403Turbine engine frame having an actuated equilibrating case
#404SHROUDED SINGLE CRYSTAL DUAL ALLOY TURBINE DISK
#405Fastening device
#406Steam turbine rotating blade
#407Steam turbine rotating blade
#408Steam turbine and rotating blade
#409Gas turbine systems involving feather seals
#410Bolt and Manufacturing Method of Bolt
#411Exhaust casing hub comprising stress-distributing ribs
#412Steam turbine exhaust hood and method of fabricating the same
#413Wear minimization system for a compressor diaphragm
#414Seal assembly
#415Blade/disk dovetail backcut for blade/disk stress reduction (7FA, stage 1)
#416Blade/disk dovetail backcut for blade/disk stress reduction (9FA, stage 1)
#417Rotor blade for a compressor or a gas turbine
#418TURBINE BLADE WITH TRAILING EDGE CUTBACK AND METHOD OF MAKING SAME
#419Fan frame
#420Gas turbine or compressor blade
#421Vane platform rail configuration for reduced airfoil stress
#422Apparatus and method for welding superalloys
#423Airfoil with heating source
#424Turbine disk
#425Methods and apparatus for assembling turbine nozzles
#426ASSEMBLY FOR CONTROLLING THERMAL STRESSES IN CERAMIC MATRIX COMPOSITE ARTICLES
#427Transition piece for gas turbine
#428Turbine blades
#429Thermally compliant C-clip
#430Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 2)
#431Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)
#432Gas turbine disk slots and gas turbine engine using same
#433Finger dovetail attachment between a turbine rotor wheel and bucket for stress reduction
#434Hoop stress relief mechanism for gas turbine engines
#435Flexible heat shields and method
#436Duct with integrated baffle
#437Radial-flow turbine wheel
#438Vane platform rail configuration for reduced airfoil stress
#439Spacer arrangement
#440Turbine blade
#441Advanced firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels
#442Rotor blade for a rotary machine
#443Rotor blade for a rotary machine
#444Method and apparatus for controlling steam turbine inlet flow to limit shell and rotor thermal stress
#445Turbine shroud segment
#446Turbine blade inner rib profile
#447High-speed pressurized impeller disk
#448Bowed-rotor mitigation system for a gas turbine
#449Method for processing the output of a speech recognizer
#450Exhaust nozzle having a compliant shell for a gas turbine engine
#451Method for integral turbine blade repair