TURBINE BLADE TIP GEOMETRY SYSTEM AND METHOD FOR GAS TURBINE ENGINE

METHODS AND APPARATUS TO IMPROVE FAN OPERABILITY CONTROL USING SMART MATERIALS

TURBOFAN ENGINE HAVING ANGLED INLET PRE-SWIRL VANES

MIXER VANES

VIBRATIONAL DAMPING ASSEMBLY FOR A TURBOMACHINE EXHAUST DIFFUSER

Methods and apparatus to improve fan operability control using smart materials

Vortex restart structures for turbulated passages

Layout for asymmetric cast trips in long passages

TURBOFAN ENGINE HAVING ANGLED INLET PRE-SWIRL VANES

System and method for turbomachine with local vortex generator array

Turbine blade and gas turbine

Compressor bleed air channels having a pattern of vortex generators

METHODS AND APPARATUSES FOR REDUCING ENGINE NOISE

TURBOFAN ENGINE HAVING ANGLED INLET PRE-SWIRL VANES

Components for gas turbine engines

Gas turbine air bleed arrangement with an inlet

Turbine and turbocharger including the turbine

Method of reducing turbine wheel high cycle fatigue in sector-divided dual volute turbochargers

System and method for turbomachine with local vortex generator array

Mixer vanes

Mixer vanes having a waveform profile

Combustor dilution hole

Turbine exhaust case mixer

Purging configuration for combustor mixing assembly

Stator blade for a centrifugal compressor

Gas turbine engine

ENGINE COMPONENT ASSEMBLY

Turbine shroud cooling

Moving blade for a wheel of a turbine engine

Monolithic diffuser and deswirl flow structure for gas turbine engine

Method, system and apparatus for reducing fluid drag

Inlet cowl for a turbine engine

Assisted engine start bleed system

Erosion-resistant coating with patterned leading edge

External turning vane for IFS-mounted secondary flow systems

Airfoil with cooling passage circuit through platforms and airfoil section

Turbine engine airfoil and method

Diffuser-deswirler for a gas turbine engine

Gas turbine engines including tangential on-board injectors and methods for manufacturing the same

Inter-turbine ducts with flow control mechanisms

Turbine engine component and method of cooling

Turbine engine with a swirler

Turbine engine component including an axially aligned skin core passage interrupted by a pedestal

Gas turbine engine

Internally cooled airfoil

Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor

Vortex generators for turbine engine exhaust

Guide vane for a turbomachine

Article having ceramic wall with flow turbulators

Trip strips for augmented boundary layer mixing

Wall comprising a film cooling hole

GAS PATH DUCT FOR A GAS TURBINE ENGINE

Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air

Case for gas turbine engine

Turbine and gas turbine

Labyrinth seal

Inlet diffusers for jet engines, jet engines, jet aircraft, and methods for diffusing incoming air of jet engines

Platforms with leading edge features

Inter-turbine ducts with flow control mechanisms

Combustor and gas turbine including the same

Involute trapped vortex combustor assembly

AIR SWIRLERS

Turbine airfoil with internal cooling channels having flow splitter feature

Turbine airfoil with turbulating feature on a cold wall

Baseless vortex generator

Mechanical component

EXHAUST ASSEMBLY WITH VORTEX GENERATOR

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

Blockage-resistant vane impingement tubes and turbine nozzles containing the same

Diffuser-deswirler for a gas turbine engine

Airfoil cooling structure

Turbofan nacelle assembly with flow disruptor

Exhaust stream mixer

Diffuser pipe with vortex generators

Turbine engine assembly with a component having a leading edge trough

Cooling structure for vane

Turbine engine part with non-axisymmetric surface

Guide vane assembly for a rotary machine and methods of assembling the same

Article having ceramic wall with flow turbulators

Solid rocket motor with vortex inducing feature

Manufacture and installation of diffuser flow mixing lobes

Inlet cowl for a turbine engine

Turbine

Bleed air heat ejectors

Engine component assembly

Impeller-mounted vortex spoiler

Turbomachine including clearance control system

Methods and articles relating to ionic liquid bath plating of aluminum-containing layers utilizing shaped consumable aluminum anodes

System and method for mixing tempering air with flue gas for hot SCR catalyst

Air shredder insert

Forward flowing serpentine vane

Cooling circuit for a multi-wall blade

Cooling circuit for a multi-wall blade

Method and assembly for forming components having an internal passage defined therein

Engine component with film cooling

Baffle insert for a gas turbine engine component and method of cooling

Baffle insert for a gas turbine engine component and component with baffle insert

Baffle insert for a gas turbine engine component

Gas turbine engine component with a baffle insert

Engine component with film cooling

Fastback turbulator

Mixing chambers for turbine wheel space cooling

System and method for creating a fluidic barrier from the leading edge of a fan blade

System and method for creating a fluidic barrier with vortices from the upstream splitter

Methods of creating fluidic barriers in turbine engines

System and method for a fluidic barrier on the low pressure side of a fan blade

Cooling channels for gas turbine engine component

Article, airfoil component and method for forming article

Vortex Tube Supplying Superheated Vapor for Turbine Power Generation

Gas turbine stator with winglets

Turbomachine diffuser including flow mixing lobes and method

Turbine engine component including an axially aligned skin core passage interrupted by a pedestal

Turbine bucket cooling

Blade outer air seal cooling passage

Turbine airfoil turbulator arrangement

Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same

Gas turbine engine component cooling passage turbulator

SUPERSONIC COMPRESSOR

Anti-icing system for an aircraft

Gas turbine engine airfoil cooling configuration with pressure gradient separators

Turbine engine nozzle having confluent streams and including a core cowl with overlapping flaps

Fluid injector for cooling a gas turbine engine component

Gas turbine engine with disk having periphery with protrusions

Hot part of gas turbine, gas turbine including the same, and manufacturing method of hot part of gas turbine

Cooling for gas turbine engine components

Gas turbine sealing

Fuel/air mixing system for fuel nozzle

Gas turbine engine exhaust mixer

Platforms with leading edge features

METHOD OF FORMING TURBULATORS ON A TURBOMACHINE SURFACE AND APPARATUS

Film hole with protruding flow accumulator

Dual-walled ceramic matrix composite (CMC) component with integral cooling and method of making a CMC component with integral cooling

Engine nacelle

Internal cooling of engine components

Turbine blades and methods of forming turbine blades having lifted rib turbulator structures

Gas turbine engine component having shaped pedestals

Gas turbine engine component cooling channels

Gas turbine engine component having curved turbulator

Gas turbine engine component having tip vortex creation feature

Turbomachine vane including an antivortex fin

Airfoil with improved cooling

Method of reducing manufacturing variation related to blocked cooling holes

Baffle with flow augmentation feature

Turbine airfoil with an internal cooling system having trip strips with reduced pressure drop

FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE

Exhaust stream mixer

Diffuser with strut-induced vortex mixing

Three-dimensional printing process, swirling device and thermal management process

Inducer and diffuser configuration for a gas turbine system

Power generation using buoyancy-induced vortices

Intake arrangement in gas turbine power plant

Vortex generators placed in the interblade channel of a compressor rectifier

Augmented cooling system

Cooled wall

Turbomachine element

Turbine blade

Air swirlers

Arrangement for sealing an open cavity against hot gas entrainment

Hydraulic bearing for a stationary gas turbine

Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles

Exhaust diffuser

Method of manufacturing a cooled turbine blade with dense cooling fin array

Airfoil with variable trip strip height

Steam turbine stationary blade and steam turbine

Turbine blade of a gas turbine with swirl-generating element and method for its manufacture

Gas turbine engine airfoil internal cooling features

Trailing edge cooling configuration for a gas turbine engine airfoil

Exhaust diffuser including flow mixing ramp for a gas turbine engine

AERODYNAMIC ELEMENT OF TURBINE ENGINE

Turbine engine and aerodynamic element of turbine engine

COOLING PEDESTAL ARRAY

Surface area augmentation of hot-section turbomachine component

Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle

Method and apparatus for turbo-machine noise suppression

Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling

Apparatus to apply a variable surface texture on an airfoil

Air fuel premixer having arrayed mixing vanes for gas turbine combustor

System and method of monitoring turbine engines

Turbine component including airfoil with contour

Exhaust diffuser adjustment system for a gas turbine engine

Jet flow nozzle and jet engine

Transitional region for a secondary combustion chamber of a gas turbine

STATOR FOR SUPERSONIC COMPRESSOR

VORTEX GENERATORS

Diffuser pipe and assembly for gas turbine engine

Apparatus for controlling a boundary layer in a diffusing flow path of a power generating machine

Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals

Supersonic engine inlet diffuser with deployable vortex generators

Gas turbine engine and pulse detonation combustion system

Turbine seal fin leakage flow rate control

FLOW DISCHARGE DEVICE

System and method for supplying fuel

Airflow control device and airflow control method

Engine pylon comprising a vortex generator, and method for the production thereof

TURBINE BLADE WITH IMPROVED TRAILING EDGE COOLING

Turbomachine with axial compression or expansion

Oscillatory vorticity generator and applications thereof

Plasma actuated vortex generators

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

SYSTEM AND METHOD TO ELIMINATE A HARD RUB AND OPTIMIZE A PURGE FLOW IN A GAS TURBINE

Turbine blade tip with vortex generators

TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY OF IMPINGEMENT NOZZLES

Gas turbine engine and combustor

Combustor liner assembly with enhanced cooling system

Gas turbine engine including a stator vane for directing hot combustion gases onto rotor blades

COMBUSTOR TRANSITION PIECE WITH DILUTION SLEEVES AND RELATED METHOD

Recessed metering standoffs for airfoil baffle

Seal assembly

Seal assembly

Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine

FLOW MIXING VENT SYSTEM

Shroud vortex remover

Heat transfer enhancement in internal cavities of turbine engine airfoils

Systems and apparatus relating to compressor operation in turbine engines

Boundary layer energiser

Boundary layer energiser

High efficiency turbine system

Vortex chambers for clearance flow control

Turbine section architecture for gas turbine engine

Gas turbine engine exhaust mixer

Heat transfer passage

Systems and apparatus relating to turbine engines and seals for turbine engines

Passive boundary layer control elements

Wind turbine blade with submerged boundary layer control means comprising crossing sub-channels

Recessed metering standoffs for airfoil baffle

Burner including non-uniformly cooled tetrahedron vortex generators and method for cooling

Blade cooling structure of gas turbine

Wind turbine blade with submerged boundary layer control means

Gas turbine engine with fluid mixing arrangement

Engine noise

Ingestion resistant seal assembly

Gas turbine engine assemblies with vortex suppression and cooling film replenishment

Casing of a gas turbine engine having a radial spoke with a flow guiding element

Fastener assembly with cyclone cooling

Mechanical acoustic noise generator system for scramjet engine

Nacelle assembly with turbulators

Blade

Turbine blade tip cooling system

Turbine airfoil with near wall multi-serpentine cooling channels

Cooled turbine blade for a gas turbine and use of such a turbine blade

Gas turbine engine mixing duct and method to start the engine

Compressor for an internal combustion engine

Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes

Wind turbine blade with anti-noise devices

Ring seal for a turbine engine

Vane wheel of turbine comprising a vane and at least one cooling channel

Turbine blade trip strip orientation

Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade

Turbine airfoil cooling system with axial flowing serpentine cooling chambers

Turbine airfoil cooling system with near wall vortex cooling chambers

Flow control systems

Leaned deswirl vanes behind a centrifugal compressor in a gas turbine engine

Gas turbine engine mixing duct and method to start the engine

Counterrotating turbofan engine

System for introducing fuel to a fluid flow upstream of a combustion area

Turbine heat shield with ribs

Vortex dissipation device for a cooling system within a turbine blade of a turbine engine

Vortex cooling system for a turbine blade

Turbomachine nozzle cover for reducing jet noise

Method of improving the flow conditions in an axial-flow compressor, and axial-flow compressor for carrying out the method

Mitigation of rotating stall in turbine exhaust section using inner flow control vanes

Deswirl system for gas turbine engine

Gas turbine intake for aircraft engine and method of inspection thereof