TURBINE BLADE TIP GEOMETRY SYSTEM AND METHOD FOR GAS TURBINE ENGINE

GAS TURBINE ENGINE HAVING COMPOSITE FAN BLADES

AIRFOIL ASSEMBLY

AIRFOIL ASSEMBLY

Deformable root spacer for a gas turbine engine rotor blade

COOLING FEATURES FOR A COMPONENT OF A GAS TURBINE ENGINE

BLADES OF AN AXIAL TURIBINE

AIR-CONDITIONING APPARATUS AND REFRIGERATION CYCLE APPARATUS [AS AMENDED]

Impeller and centrifugal compressor

Rotor with balancing features and balancing method

Water heater blower housing, impeller, and static tap system

Gas turbine blade

Centrifugal compressor and turbocharger

Centrifugal compressor for fuel cell

Low speed fan up camber

Wind turbine blade root attachment system and method of manufacture

Characteristic distribution for rotor blade of booster rotor

Gas turbine engine with blade channel variations

Impeller and centrifugal compressor

HYBRID AIRFOIL

Centrifugal compressor

Water heater blower housing, impeller, and static tap system

Centrifugal fan, air-sending device, air-conditioning apparatus, and refrigeration cycle apparatus

Multi-stage centrifugal compressor, casing, and return vane

Blade of steam turbine and steam turbine

Exhaust hood and steam turbine

COMPRESSOR HAVING EXTENDED RANGE AND STABILITY

Impeller with hub sweep

Turbine rotor blade, turbocharger, and method for producing turbine rotor blade

High pressure turbine blade airfoil profile

Centrifugal fan

Rotary machine

Rotor, turbine equipped with such a rotor and turbomachine equipped with such a turbine

Blade and rotary machine having the same

Multistage axial-centrifugal compressor systems and methods for manufacture

Diffuser-deswirler for a gas turbine engine

Method for machining free-form surface on elongated material

Accessory box for a turbomachine

Modal response tuned turbine blade

Auxiliary power unit for reducing flow loss of gas

Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distribution

Gas turbine engine airfoil

Concentric turbomachine with electric machine

Concentric turbomachine with trailing edge

Turbofan arrangement with blade channel variations

FEATHERSEAL FORMED OF CMC MATERIALS

Wind turbine blade root attachment system and method of manufacture

Rotary machine blade, supercharger, and method for forming flow field of same

Covered radial fan wheel with a periodically and asymmetrically shaped plate

Turbine wheel assembly with pinned ceramic matrix composite blades

Compressor diffuser with diffuser pipes varying in natural vibration frequencies

Compressor diffuser with diffuser pipes having aero-dampers

Propeller fan

Aircraft fan with low part-span solidity

Short inlet with low solidity fan exit guide vane arrangements

GAS TURBINE ENGINE OUTLET GUIDE VANES

Platform cover plates for gas turbine engine components

Converging duct with elongated and hexagonal cooling features

Cooling passage with structural rib and film cooling slot

Compressor bleed port structure

Method for profiling blades of an axial turbomachine

Variable inlet guide vane

Fan housing for reduced noise

Rotor disk for an exhaust turbocharger, exhaust turbocharger and method for balancing a rotor assembly for an exhaust turbocharger

Gas turbine engine airfoil

Centrifugal fan

Gas turbine engine airfoil shaped component

Intersector sealing tab for an aircraft turbine engine

Rotating airfoil with tip pocket

Low-noise airfoil for an open rotor

Vacuum pump, and rotor blade and reflection mechanism mounted in vacuum pump

Debris filter apparatus for preventing clogging of turbine vane cooling holes

Seal fin, seal structure, turbo machine, and method for manufacturing seal fin

Fluid pump with volute shaped housing

Method for introducing a balancing mark into the compressor wheel of a turbocharger, and turbocharger comprising a compressor wheel which has a balancing mark

Gas turbine engine

Diffuser-deswirler for a gas turbine engine

Two pieces stator inner shroud

Cooling structure for a turbine component

LARGE AREA RATIO COOLING HOLES

Structure for cooling rotor of turbomachine, rotor and turbomachine having the same

Method for profiling a turbine rotor blade

Variable stator vane assemblies and variable stator vanes thereof having a locally swept leading edge and methods for minimizing endwall leakage therewith

TURBOMACHINE COMPONENT HAVING A PLATFORM CAVITY WITH A STRESS REDUCTION FEATURE

Turbine

ENGINE COMPONENT WALL WITH A COOLING CIRCUIT

Gas turbine engine with an offtake

Centrifugal compressor

Creep resistant axial ring seal

Blade for an axial flow machine

Aerofoil

Gas turbine engine airfoil

Gas turbine engine components with optimized leading edge geometry

Inlet guide vanes for turbocharger compressors

Turbomachine and turbine nozzle therefor

Turbomachine and turbine blade transfer

Gas turbine engine airfoil

Gas turbine engine

Multistage compressor with aerofoil portion profiled in a spanwise direction

LAST STAGE AIRFOIL DESIGN FOR OPTIMAL DIFFUSER PERFORMANCE

Gas turbine engine airfoil

Additively manufactured connection for a turbine nozzle

Turbofan for air conditioning apparatus

Centrifugal fan

Gas turbine compressor stage

Bulged nozzle for control of secondary flow and optimal diffuser performance

Air-shielded fuel injection assembly to facilitate reduced NOemissions in a combustor system

Compressor airfoil with compound leading edge profile

Reverse fin cooling fan

Wrapped dog bone seal

Gas turbine engine fuel cooled cooling air heat exchanger

Turbofan arrangement with blade channel variations

Isentropic compression inlet for supersonic aircraft

Fan root endwall contouring

Gas turbine axial compressor

Turbomachine flow path having circumferentially varying outer periphery

Extruded profile for manufacturing a blade of an outlet guide vane

METHOD OF FORMING COOLING HOLES

Counter-swirl doublet combustor with plunged holes

Gas turbine engine airfoil shaped component

Thrust reverser system with translating-rotating hinge assembly

Gas turbine engine component with converging/diverging cooling passage

Vacuum pump

Engine airfoils and methods for reducing airfoil flutter

Gas turbine engine

Variable stator vane assemblies and variable stator vanes thereof having a locally swept leading edge and methods for minimizing endwall leakage therewith

Turbojet engine nacelle including a thrust reversing device with doors, including inner flanks on the sides of an opening

Air inlet arrangement and method of making the same

Endwall contouring for airfoil rows with varying airfoil geometries

Tangential blade root neck conic

Turbomachine blade assemblies

Gas turbine blade

Impeller wheel for diagonal or radial fans, injection molding tool for manufacturing such an impeller wheel, and device comprising such an impeller wheel

Centrifugal rotation machine

Torsion spring internal damper

Device for controlling a gas flow, an exhaust aftertreatment system and a system for propelling a vehicle

Blade with 3D platform comprising an inter-blade bulb

Gas turbine engine flow path geometry

Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same

Diffuser with strut-induced vortex mixing

Fixed turbine engine receiver part comprising an assembly for holding ancillary systems in position inside a fixed hollow shaft

Subsonic shock strut

Blade with an S-shaped profile for an axial turbomachine compressor

Turbine engine blade, in particular for a one-piece bladed disk

Unlockable device for axially arresting a sealing ring with which an aircraft turbomachine module rotor wheel makes contact

Turbomachine vane cooperating with a vane retention disk

One-block bladed disk provided with blades with adapted foot profile

Gas turbine engine rotor blade

Rotor blade for a turbomachine and turbomachine

Impingement cooling of turbine blades or vanes

Turbine blade

Turbocharger and method of manufacturing floating bush

Gas turbine conical flange bolted joint

Propfan engine

Bleed valve of an exhaust gas turbocharger

Twisted variable inlet guide vane

Systems And Apparatuses For Hot Gas Flow In A Transition Piece

Method, systems, and apparatuses for transition piece contouring

Gas turbine engine component with compound cusp cooling configuration

MULTI-LOBED COOLING HOLES IN GAS TURBINE ENGINE COMPONENTS HAVING THERMAL BARRIER COATINGS

Gas turbine engine component with converging/diverging cooling passage

Turbomachine rotor with blade roots with adjusting protrusions

Cooled turbine blade for gas turbine engine

Blade skirt

Exhaust-gas turbocharger

Method 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

Isentropic compression inlet for supersonic aircraft

System and method for conditioning air flow to a gas turbine

Interface element between a blade root and a blade root housing of a turbine disc, and turbine rotor comprising an interface element

Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg

PRE-COMPRESSED SEAL INCLUDING REMOVABLE PRE-COMPRESSION MEMBER

AIRFOIL WITH NONLINEAR COOLING PASSAGE

Shaft assembly for a gas turbine engine

Supersonic aircraft jet engine installation

Butterfly plate for a steam turbine exhaust hood

Air inlet arrangement and method of making the same

Vane assembly for a gas turbine engine

CHEVRON PLATFORM TURBINE VANE

Turbine wheel

Diffuser pipe and assembly for gas turbine engine

FORMED FLEXIBLE SEAL

Turbine blade base load balancing

Impeller and turbomachinery including the impeller

Stator of an axial compressor stage of a turbomachine

STATOR-ROTOR ASSEMBLIES WITH FEATURES FOR ENHANCED CONTAINMENT OF GAS FLOW, AND RELATED PROCESSES

Cooled gas turbine engine component

Turbine blade fastening for a turbomachine

Gas turbine engine air intake in a nacelle

Cooling system having reduced mass pin fins for components in a gas turbine engine

Turbomachine flow path having circumferentially varying outer periphery

Leaf seal device

Isentropic compression inlet for supersonic aircraft

Gas turbine engine airfoil shaped component

Annulus filler

Turbine engine compressor stator

Blade orientation of an impeller or propeller

Impeller

Isentropic compression inlet for supersonic aircraft

Turbine component cooling channel mesh with intersection chambers

Turbine exhaust plenum

Ring segment with serpentine cooling passages

Ring segment with forked cooling passages

Minimizing blockage of holes in turbine engine components

Blade for use with a rotary machine and method of assembling same rotary machine

Recessed metering standoffs for airfoil baffle

Exhaust plenum flow splitter

Low-ductility turbine shroud and mounting apparatus

Accessory gearbox with internal layshaft

Airfoil for a compressor blade

Airfoil for a compressor blade

OPTIMIZED GEOMETRY TURBOCOMPRESSOR

Mould for soldering, arrangement of moulds, a method and a component

Seal for a platform in the rotor of a turbine engine

Sealing structure on a shroud of a turbine blade

Ring segment positioning member

Method for joining components

Turbo engine

GAS TURBINE BLADE, MANUFACTURING METHOD THEREFOR, AND GAS TURBINE USING TURBINE BLADE

Shape-changing structure member with embedded spring

Radial or diagonal fan wheel

Compressor aerofoil

METHOD FOR OPTIMISING THE SHAPE OF AN AEROFOIL

Blade with non-axisymmetric platform: recess and boss on the extrados

Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut

CROSS-FLOW FAN, BLOWER AND MOLDING MACHINE FOR IMPELLER

Airfoil for a compressor blade

Airfoil for a compressor blade

Seal and seal arrangement for confining leakage flows between adjacent components of turbo-machines and gas turbines

Tip vortex control

BLADE WITH 3D PLATFORM COMPRISING AN INTER-BLADE BULB

Rotor for an axial-throughflow turbomachine and moving blade for such a rotor

Gas turbine exhaust strut refurbishment

Vane or blade for an axial flow compressor

System and method for accommodating changing resource conditions for a steam turbine

Turbomolecular pump

Gas turbine transition duct profile

Cooled gas turbine engine airflow member

BLADE FOR A ROTATING THERMAL MACHINE

Compound cooling flow turbulator for turbine component

Electrical Cable Shroud

Blade with non-axisymmetric platform

Turbine blade assembly and seal strip

Aerodynamic swept vanes for fuel injectors

Cooling hole exits for a turbine bucket tip shroud

Airfoil Having an Improved Trailing Edge

Compliant element

Leaf seal device

TURBOCHARGER

Cartridge-loaded rocket motor with castellated grain segments

Cooling arrangements

Turbine blade with single tip rail with a mid-positioned deflector portion

TURBINE BLADE CASCADE ENDWALL

Multi stage radial compressor

Gas turbine exhaust diffuser

Recessed metering standoffs for airfoil baffle

Structural members in a pedestal array

Turbine blade or vane with improved cooling

Modular serpentine cooling systems for turbine engine components

Metal seals for weld-deformed high temperature pneumatic ducting joints

Cut-off construction for transverse fan assemblies that have elongated fan blades of arcuate cross-section

Apparatus to reduce thrust oscillations in a launch vehicle

Rotor of a gas turbine

Turbocharger with variable turbine geometry

METHODS, SYSTEMS AND/OR APPARATUS RELATING TO STEAM TURBINE EXHAUST DIFFUSERS

COMPLIANT PLATE SEAL WITH SELF-CORRECTING BEHAVIOR

Turbomachine with separate fuel injection systems, using identical sealing joints

Hub cone for an aircraft engine

System and method for reducing bucket tip losses

Charging equipment

Turbine blade

Turbine blade assembly

Diffuser for decelerating a compressed fluid

Gas turbine engine nacelle

Turbofan gas turbine engine fan blade and a turbofan gas turbine fan rotor arrangement

Cascade tip baffle airfoil

Reverse curved nozzle for radial inflow turbines

Compact multiphase pump

Impeller and centrifugal fan

Platform mate face contours for turbine airfoils

Shape-changing structure member with embedded spring

Compressor stator chord restoration repair method and apparatus

Fluid flow machine including rotors with small rotor exit angles

Airfoil for nozzle and a method of forming the machined contoured passage therein

Gas turbine arrangement

Airfoil design for rotor and stator blades of a turbomachine

Swept fan ramp for pivot door thrust reverser

CENTRIFUGAL IMPELLER

Method to prevent brinelling wear of slot and pin assembly

Nozzle with temperature-responsive throat diameter

Turbine bucket shroud internal core profile

Fuel injection system for a gas turbine engine

Cooling structure

Fuel inlet with crescent shaped passage for gas turbine engines

Arrangement for axially securing rotating blades in a rotor, sealing element for such an arrangement, and use of such an arrangement

Feather Seals and Gas Turbine Engine Systems Involving Such Seals

Systems and methods for controlling seal clearance in a turbine engine

Blade outer air seal with improved thermomechanical fatigue life

Advanced turbulator arrangements for microcircuits

Variable geometry turbine

Rotor blade, method for producing a rotor blade, and compressor with a rotor blade