GAS TURBINE ENGINE NOZZLE

TURBINE ENGINE WITH A NOZZLE HAVING COOLING FEATURES

FAN ASSEMBLY

DILUTION HOLES WITH RIDGE FEATURE FOR GAS TURBINE ENGINES

PROPULSOR WING TRAILING EDGE EXHAUST AREA CONTROL

STATOR VANE FOR A GAS TURBINE ENGINE

REGENERATIVE COOLING AND ADJUSTABLE THROAT FOR ROTATING DETONATION ENGINE

Rotor blade and rotor blade assembly for a turbomachine

Face sheet of acoustic liner having streamlined holes with elongated edges

Blade for a rotating bladed disk for an aircraft turbine engine comprising a sealing lip having an optimized non-constant cross section

Multi-function monolithic combustion liner

Fuel nozzle with integrated metering and flashback system

Propulsor wing trailing edge exhaust area control

Regenerative cooling and adjustable throat for rotating detonation engine

Combustor dilution hole

Inertial particle separator for a turbine section of a gas turbine engine

Annular component for supporting a turbine engine bearing

ROTOR DISK AND ROTOR BLADE FOR A GAS TURBINE COMPRESSOR OR TURBINE STAGE OF AN AEROENGINE

VACUUM PUMP AND CONNECTION PORT USED IN VACUUM PUMP

Sealing arrangement with vent for an engine component with a service port

Dilution holes with ridge feature for gas turbine engines

Turbine ring assembly having indexed flanges

Two-stage combustor for gas turbine engine

Turbine blade having gas film cooling structure with a composite irregular groove and a method of manufacturing the same

Method and systems for a fluidic variable turbocharger for an engine

Liner cooling device, combustor including same, and gas turbine including same

Modular casing manifold for cooling fluids of gas turbine engine

Replaceable rotor blade tip clearance measurement device for a gas turbine engine

SEALED CMC TURBINE CASE

ACOUSTIC TREATMENT FOR AIRCRAFT ENGINE

Rotor drum for a turbomachine

Quench aperture body for a turbine engine combustor

Compressor impeller

COMPONENT FOR A TURBINE ENGINE WITH A FILM HOLE

Reinforced axial diffuser

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Turbine airfoil multilayer exterior wall

Turbine component with tip rail cooling passage

Turbine wheel for a turbine

Gas turbine engine having a flow-conducting assembly formed of nozzles to direct a cooling medium onto a surface

TURBINE BLADE

Dilution holes with ridge feature for gas turbine engines

Labyrinth seal for a turbine engine of an aircraft

Compressor and gas turbine including the same

BLADE OF A TURBOMACHINE, INCLUDING A COOLING CHANNEL AND A DISPLACEMENT BODY SITUATED THEREIN, AS WELL AS A METHOD FOR MANUFACTURING

Gas turbine blade

Turbine engine and components for use therein

Turbine vane cluster including enhanced vane cooling

TURBINE VANE CLUSTER INCLUDING ENHANCED PLATFORM COOLING

Turbine component with bounded wear coat

Equipment drive gearbox in a turbomachine

Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustor

Endwall cooling system

Rotor with subset of blades having a cutout leading edge

Method for real-time simultaneous and calibrated additive and subtractive manufacturing

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

COMBUSTOR LINER PANEL END RAIL MATCHING HEAT TRANSFER FEATURES

Turbine engine component with a core tie hole

Nozzle assembly and method for forming nozzle assembly

High-pressure distributor blading having a variable-geometry insert

Oil tank comprising an oil level control device

Turbine assembly

Segmented annular seal

Fan for aircraft turbomachine

Positioning element with recesses for a guide vane arrangement

Component for a turbine engine with a hole

Transition Duct Support Arrangement for a Gas Turbine Engine

Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine

Impingement cooling system for a gas turbine engine

Method for repairing a fan casing

ANTI-BIRD STRIKE PROTECTION NET FOR AIRCRAFT JET ENGINE

Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article

Gas-turbine combustion chamber with impingement-cooled bolts of the combustion chamber tiles

Turbine blade

Component for a turbine engine with a film hole

Turbine blade attachment curved rib stiffeners

AIRFOIL PLATFORM COOLING CORE CIRCUITS WITH ONE-WALL HEAT TRANSFER PEDESTALS FOR A GAS TURBINE ENGINE COMPONENT AND SYSTEMS FOR COOLING AN AIRFOIL PLATFORM

Cooling of turbine blades and method for turbine blade manufacture

NMR-MAS turbine assembly

Gas turbine disk

Composite booster spool with separable composite blades

AXIAL TURBO MACHINE

Damper pin for a turbine blade

EXHAUST MIXER WITH OUTER LOBE CONSTRAINT BAND

Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element

Turbine shroud segment sealing

Diffuser part for a gas turbine

Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduit

Turbine component thermal barrier coating with depth-varying material properties

Turbine component thermal barrier coating with crack isolating engineered groove features

Gas turbine diffuser outer diameter and inner diameter wall strips for turbine exhaust manifold pressure oscillation reduction

Additive manufactured non-round, septum tied, conformal high pressure tubing

Angled impingement inserts with cooling features

TWO-STAGE COMBUSTOR FOR GAS TURBINE ENGINE

High visibility latch handle

Turbine rotor blade

Quench aperture body for a turbine engine combustor

Shroud assembly for a turbine engine

Flowpath boundary and rotor assemblies in gas turbines

Turbine blade having film cooling hole arrangement

Blade or vane for a turbomachine and axial turbomachine

Turbine blade cooling structure

POWER TURBINE INLET DUCT LIP

Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle

POWER TURBINE AIR STRUT

Variable area nozzle and associated propulsion system and method

Gas turbine engine component having shaped pedestals

Cooled airfoil trailing edge and method of cooling the airfoil trailing edge

Air intake guide

Gas turbine shroud assemblies

Turbine shroud segment sealing

Elliptical air opening at an upstream end of a fuel injector shroud and a gas turbine engine combustion chamber

Gas turbine engine cooling hole with circular exit geometry

Method for fabricating a single-piece part for a turbine engine by diffusion bonding

Turbomachine thermal management

Fan blade attachment of gas turbine engine

Two-stage combustor for gas turbine engine

Exhaust-gas turbocharger with silencer

GAS TURBINE ENGINE

Air turbine starter one-piece air exit port baffle

Replaceable orifice for combustion tuning and related method

Fastener aperture having an elongated geometry

Assembly for directing combustion gas

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

Method of fuel staging in combustion apparatus

Combustion cavity layouts for fuel staging in trapped vortex combustors

Vortex premixer for combustion apparatus

Inlet premixer for combustion apparatus

Combustor turbine interface for a gas turbine engine

Peripheral tunnels propeller

Retainer for suspended thermal protection elements in a gas turbine engine

Apparatus to reduce thrust oscillations in a launch vehicle

Modular transvane assembly

Trailing edge cooling for turbine blade airfoil

Counter-vortex film cooling hole design

Counter-vortex paired film cooling hole design

Replaceable orifice for combustion tuning and related method

GAS TURBINE CASING FOR ENCLOSING A GAS TURBINE COMPONENT

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

DETONATION COMBUSTOR TO TURBINE TRANSITION PIECE FOR HYBRID ENGINE

Supercharger

Cooling arrangement for a component of a gas turbine engine

Gas turbine engine exhaust duct ventilation

Rocket chamber heat exchanger

Gas turbine blade shroud

Coated bucket damper pin

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

Mistake proof identification feature for turbine blades

Coated bucket damper pin and related method

Intake housing for axial fluid flow engines

Turbulated hole configurations for turbine blades

Cooled gas turbine engine vane

First stage impulse steam turbine nozzle axially tangential holes matrix

Gas turbine engine rotor stage with seal members

2D variable-area plug nozzle

Controlled contact surface for a secondary seal in a non-contact seal assembly

Seal in a gas turbine engine having a shim base and a honeycomb structure with a number of cavities formed therein

Turbine abradable layer with nested loop groove pattern