GAS TURBINE ENGINE NOZZLE

VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

TURBOMACHINE FOR A FLIGHT PROPULSION DRIVE

IMPELLER PUMP AND METHOD

Inlet cone for an aircraft turbomachine

AIRFOIL FOR A TURBINE ENGINE

Pump comprising an impeller body provided as an oblique cone

Energy-saving device for rapidly and infinitely compressing air

Service tube locking device

Exhaust frequency mitigation apparatus

Turbocharger

Flexible frustoconical input shaft

ASSEMBLY FOR A TURBINE ENGINE

Preform crossovers for composite airfoils

Dual pressure fuel nozzles

POST-SHUTDOWN ENGINE HEAT REMOVAL SYSTEM

Triple flow aircraft turbomachine provided with a power transmission module

MITIGATING COMBUSTION DYNAMICS USING VARYING LIQUID FUEL CARTRIDGES

Seal assembly between a transition duct and a first stage vane structure

Turbocharger compressor with inlet-adjustment mechanism having pivoting blades forming adjustable uninterrupted blade ring

Method of making a single-crystal turbine blade

Fuel injector assembly for a turbine engine

Pump comprising an impeller body provided as an oblique cone

Turbofan engine comprising an outlet cone cooled by its secondary flow

Flow straightener unit comprising a centering and attachment plate

Mechanical reduction gear for aircraft turbomachine

Cast turbine nozzle having heat transfer protrusions on inner surface of leading edge

Gas turbine stator

Bypass turbomachine

Assembly for axial turbomachine, associated axial turbomachine, assembly method, and sealing joint

Exhaust gas turbocharger

Turbine nozzle having an angled inner band flange

Method of making a single-crystal turbine blade

HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING-DIVERGING PASSAGE PORTIONS

Impingement cooling dust pocket

A TURBOMACHINE BLADE OR VANE HAVING A VORTEX GENERATING ELEMENT

Turbocharger and turbine housing therefor

AIRFOIL FOR A TURBINE ENGINE

Film-cooled multi-walled structure with one or more indentations

Beveled coverplate

Gas turbine engine airfoil with wishbone baffle cooling scheme

Noise reducer for a wind turbine rotor blade having a cambered serration

Turbo-shaft ejector with flow guide ring

Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pin

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Rib bumper system

Hot section dual wall component anti-blockage system

Gas turbine engine nose cone assembly

COMPOSITE COMPONENT HAVING ANGLED BRAZE JOINT, COUPON BRAZING METHOD AND RELATED STORAGE MEDIUM

AXIAL STIFFENING RIBS/AUGMENTATION FINS

Flared anti-vortex tube rotor insert

BLADED ROTOR WITH INTEGRATED GEAR FOR GAS TURBINE ENGINE

Passageway between a shroud and a rotor platform in a turbine engine

Wastegate valve of turbocharger

Turbine engine assembly comprising a nose cone and a front shroud

Gas turbine engines and compression systems therefor

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine engine

Engine component with non-diffusing section

Turbine wheel for a turbine

Turbine frame assembly for gas turbine engines

Turbine nozzle having an angled inner band flange

Contacting dry face seal with tapered carbon nose

Apparatus for handling a turbomachine part

VANE WHEEL AND BLOWING DEVICE

VANE WHEEL AND BLOWING DEVICE

Seal structure and turbine

Step seal, seal structure, turbo machine, and method for manufacturing step seal

Composite component having angled braze joint, coupon brazing method and related storage medium

Exhaust diffuser

Turbine engine airfoil insert

Turbine engine and containment assembly for use in a turbine engine

Brush seal for a turbine engine rotor

Wear indicator for determining wear on a component of a gas turbine engine

Apparatus including heat exchanger and sound attenuator for gas turbine engine

Particle separator assembly for a turbine engine

Asymmetric gas turbine exhaust diffuser

Stage of variable-pitch blades for a turbine engine, turbine engine and associated installation method

Variable nozzle unit and variable displacement-type turbocharger

Blade to stator heat shield interface in a gas turbine

SOUND ATTENUATING SYSTEM FOR GAS TURBINE ENGINE

Flanged component for a gas turbine engine

Circumferentially varying thickness composite fan casing

ROTATING BRUSH SLEA WITH BRISTLE SHIELD

Engine component with porous trench

Components having outer wall recesses for impingement cooling

Seal device for turbine, turbine, and thin plate for seal device

Impingement insert for a gas turbine engine

Method for repairing a fan casing

Cooled hot section components for a gas turbine engine

ANTI-BIRD STRIKE PROTECTION NET FOR AIRCRAFT JET ENGINE

Turbomachine blade assembly

AIRFOIL FOR A TURBINE ENGINE

Fuel nozzle with increased spray angle range

Self-stiffened casing consisting of a composite material with an organic matrix

Impingement holes for a turbine engine component

Conical screw connection for a fuel line

NOSE CONE FOR A FAN OF AN AIRCRAFT ENGINE

Turbine shroud with mounted full hoop blade track

Gas turbine engine blade outer air seal profile

Variable stator vane undercut button

High pressure exhaust muffling device with multiple sources

Crossover hole configuration for a flowpath component in a gas turbine engine

Run-up surface for the guide-vane shroud plate and the rotor-blade base plate

Stacking of rotor blades on centroids

COATED AND UNCOATED SURFACE-MODIFIED AIRFOILS FOR A GAS TURBINE ENGINE COMPONENT AND METHODS FOR CONTROLLING THE DIRECTION OF INCIDENT ENERGY REFLECTION FROM AN AIRFOIL

Positive displacement rotary motion device including a pulse detonation device

Nose cone and shaft balancing assembly

Crosswind performance aircraft engine spinner

Gas turbine engine hybrid variable bleed valve

Nozzle guide vane and method for forming such nozzle guide vane

MIM-FORMED TiA1 TURBINE WHEEL SURROUNDING A CAST/MACHINED CORE

Gas turbine rapid response clearance control system with annular piston

Steam turbine

Variable turbine and/or compressor geometry for an exhaust-gas turbocharger

Angled impingement inserts with cooling features

Rotating labyrinth M-seal

Balanced turbine engine portion and turbine engine

Film cooled multi-walled structure with one or more indentations

Particle separating fluid intake

Pipe connection arrangement, high-pressure fluid line system of a dual fuel engine, dual fuel engine and use of a tension nut

Turbine compressor wheel with axially extended blades

Gas turbine engine airfoil with wishbone baffle cooling scheme

Airfoil fillet

Gas turbine engine component with increased cooling capacity

Turbine airfoil platform segment with film cooling hole arrangement

Airfoil including loose damper

Turbine rotor nut and bolt arrangement with improved fatigue resistance under centrifugal load

Ice-shedding spinner for ram air turbine

Gas turbine engine nacelle

Rotor disk blade with friction-held root, rotor disk, turbomachine and associated assembly method

Nacelle and compressor inlet arrangements

Aero engine with a bearing chamber and an appliance for introducing oil

Beveled coverplate

Gas turbine engine ejector

Tie shaft flow trip

End-burning propellant grain with area-enhanced burning surface

Geared turbofan with improved spinner

Bell mouth inlet for turbine blade

System and method for aft mount of gas turbine engine

Thermocouple with a vortex reducing probe

Fluid film conical or hemispherical floating ring bearings

Rib bumper system

Heat exchanger for aircraft engine

Gas turbine engine

Compressor wheel with balance correction and positive piloting

Rotor blade tip clearance

Layered arrangement, hot-gas path component, and process of producing a layered arrangement

Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same

METHOD FOR PRODUCING A STATOR BLADE AND STATOR BLADE

Double frangible bearing support

Modular industrial gas turbine exhaust system

Gas turbine engine flow path geometry

Exhaust gas turbocharger having guiding screen rings that are rotatable relative to each other

Gas turbine engines with turbine airfoil cooling

Multi-sectional acoustic septum

System and method relating to axial positioning turbine casings and blade tip clearance in gas turbine engines

Turbine casing false flange flow diverter

Heat exchanger for aircraft engine

Combustor assembly including a transition inlet cone in a gas turbine engine

Electrode for forming a cooling channel in a wall

Gas turbine engines having plasma flow-controlled intake systems

Rotor wheel for a turbine engine

Solar collector and turbine arrangement

Gas turbine exhaust diffuser with helical turbulator

Interior cooling circuits in turbine blades

High pressure compressor thermal management

Indexed positive displacement rotary motion device

Turbo engine comprising a damping fluid film for damping a guide bearing of a shaft of the turbo engine and method of adjusting the thickness of such a damping fluid film

Suction side turbine blade tip cooling

Turbine bucket with notched squealer tip

Convective shielding cooling hole pattern

Guide vane attachment structure and fan

High pressure muffling devices

Airfoil including loose damper

Turbomachine thermal management

GAS TURBINE ENGINE NOSE CONE

Gas turbine engine component with multi-lobed cooling hole

NEAR FLOW PATH SEAL FOR A TURBOMACHINE

Compressor and a turbine engine with optimized efficiency

End-burning propellant grain with area-enhanced burning surface

Mechanism for variable adjustment of blades for a system of contra-rotating propellers, and a system of contra-rotating propellers comprising at least one such mechanism

Nozzled turbocharger turbine and associated engine and method

Support structure forming method

TURBINE HOUSING AND METHOD FOR DIRECTING EXHAUST

FRONT CENTERBODY SUPPORT FOR A GAS TURBINE ENGINE

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

Methods and apparatus to repair a rotor disk for a gas turbine

Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings

Turboshaft engine with parallel shafts

Filter cartridge assembly for use with turbine engine systems

Gas turbine engine and blade for gas turbine engine

COOLED BLADE FOR A GAS TURBINE

Bellows type sealing device for partition penetration by a connecting rod of a turboprop fan blade orientation control system

Turbine engine seals

Exhaust plenum flow splitter

Dovetail connection for turbine rotating blade and rotor wheel

Gas-turbine exhaust cone

Reduction of turbocharger core unbalance with centering device

STEAM VALVE

Method for the production of an integrally bladed rotor, and rotor

Gas turbine engine nose cone

Guide blade carrier

SUPERSONIC COMBUSTOR ROCKET NOZZLE

STEAM TURBINE NOZZLE SEGMENT HAVING ARCUATE INTERFACE

turbine engine component for adaptive cooling

Turbocharger

TURBINE

Sealing rings for a labyrinth seal

Joining mechanism with stem tension and interlocked compression ring

TURBOFAN ENGINE

Method and apparatus for simplified thrust chamber configurations

Nosecone bolt access and aerodynamic leakage baffle

APPARATUSES, SYSTEMS, AND METHODS FOR PREVENTING FOREIGN OBJECTS FROM BEING INGESTED INTO A JET ENGINE

Variable-vane assembly having fixed guide pins for unison ring

Flow-optimized bypass for turbo engines

Device and method for connecting a blade to a rotor shaft of a continuous flow machine

STEAM TURBINE

Cooling channel formed in a wall

DIFFUSER ARRANGEMENT

Centrifugal blower

Borescope boss and plug cooling

Device for inhibiting the flow of oil along a rotating shaft

Floatable unit for evacuation purposes

Method and system for cooling engine components

INLET CONE FOR JET ENGINE

Eccentric chamfer at inlet of branches in a flow channel

Turbine ring assembly for gas turbine

Indexed positive displacement rotary motion device

Conical pin to maintain bearing system

Cooled airfoils and gas turbine engine systems involving such airfoils

Low velocity injector manifold for hypergolic rocket engine

Apparatus and method for cooling turbomachine exhaust gas

Device for injecting mono-propellant at a flow rate that can be modulated with an injection speed that is stable

Device for injecting a mono-propellant with a large amount of flow rate modulation

Gas turbine nozzle seals for 2000° F. gas containment

System and method of continuous detonation in a gas turbine engine

Turbomachinery disc

Methods and apparatus to repair a rotor disk for a gas turbine

Balancing group for the rotor of a fluid rotary machine

Aircraft turbomachine fan comprising a balancing flange concealed by the inlet cone

Nozzle arrangement for a gas turbine engine

Turbine blade with micro-turbine nozzle provided in the blade root

Turbojet engine accessory gear box driveshaft; modular additional accessory

Method for preventing backflow and forming a cooling layer in an airfoil

System for manufacturing a rotor having an MMC ring component and an airfoil component having monolithic airfoils

Turbocharger having inclined volutes

TURBINE INLET AIR TREATMENT APPARATUS

Annular isolator dual mode scramjet engine

ANNULAR GAS TURBINE ENGINE CASE AND METHOD OF MANUFACTURING

Annular gas turbine engine case and method of manufacturing

Venturi gate valve assembly for an auxiliary power unit

Bleed off valve system

External datum system and film hole positioning using core locating holes

Rotor For A Turbo Machine And Method For The Manufacture Of Such A Rotor

Mechanical coupling for a rotor shaft assembly of dissimilar materials

Method and device for the finish machining of gas-turbine engine blades cast in a brittle material

Heat shield for mounting on a heat-radiating object, particularly on a rocket engine

Cooled turbine blade

Turbine

Pivot bushing for a variable-pitch vane of a turbomachine

Cooling channel formed in a wall

Stress defender holes

Gas turbine engine

Axial flow compressor

Cooled rotor blade with vibration damping device

Lubrication system for a counter-rotating turbine engine and method of assembling same

Nose cone for a turbomachine

Thrust vector control system for a plug nozzle rocket engine

Bladeless conical radial turbine and method

Gas turbine with stator shroud in the cavity beneath the chamber

Rotor blade for a rotary machine

Rotor blade for a rotary machine

Rotor blade connecting arrangement for a turbomachine

Conical tip shroud fillet for a turbine bucket

Cooled gas turbine engine vane

Service tube locking device

Cast integrally bladed rotor with bore entry cooling