Methods of protecting metallic components against corrosion using chromium-containing thin films

Methods for depositing coatings on aerospace components

Heat shield, systems and methods

STEAM TURBINE APPARATUS

Turbine Engine With Rotating Detonation Combustion System

METHODS FOR ADDITIVELY MANUFACTURING TURBINE ENGINE COMPONENTS VIA BINDER JET PRINTING WITH GAMMA PRIME PRECIPITATION HARDENED NICKEL-BASED SUPERALLOYS

Gas turbine hot part and gas turbine

Variable nozzle unit and turbocharger

Integrated casting core-shell structure for making cast component with novel cooling hole architecture

Thermal barrier coating film, turbine member, and thermal barrier coating method

Silicon-Based Materials Containing Indium and Methods of Forming the Same

ENGINE COMPONENT WITH SET OF COOLING HOLES

Segregated cooling air passages for turbine vane

TEST SPECIMEN FOR A GAS TURBINE ENGINE

Low bending stress structural strut and attachment

METHOD FOR ADDITIVE MANUFACTURING BY MEANS OF A POROUS AUXILIARY STRUCTURE, COMPONENT AND DEVICE

Turbine vane cooling arrangement

Platform flow turning elements for gas turbine engine components

Turbine shroud cooling

Systems, methods, and anodes for enhanced ionic liquid bath plating of turbomachine components and other workpieces

Compressor diffuser and gas turbine

Flow channel for a turbomachine

Method for producing turbine blade

Thermal insulation coating member, axial flow turbine, and method for producing thermal insulation coating member

Platforms with leading edge features

Labyrinth seal with variable tooth heights

Turbine engine airfoil assembly

Ring of turbojet vanes including an acoustic treatment structure

Aircraft propulsion system comprising a member covered with a grooved structure

TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES

Exhaust assembly mounting configuration

Unducted thrust producing system

Composite fan blade with leading edge sheath and energy absorbing insert

Gas turbine cooling arrangement with cooling manifold guides

DOUBLE WALL SERVICE TUBE WITH ANNULAR AIRFLOW PASSAGE

Gas turbine engine airfoil

Systems and methods for compacting composite components

Conduit with damping fingers

Housing for a gas turbine compressor

Dehydrogenation processing method for turbine blades

OSCILLATING WELDING METHOD

Coated casting core and manufacture methods

Turbocharger with progressively variable A/R ratio

COMPONENT FOR A TURBINE ENGINE WITH A FILM-HOLE

Thermal caulking method, thermal caulking device, and caulked material

STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS

Gas turbine engine cooling air manifolds with spoolies

Rotary machine

Intersector sealing tab for an aircraft turbine engine

Airfoil having forward flowing serpentine flow

Stainless steel alloys and turbocharger kinematic components formed from stainless steel alloys

High oxidation-resistant alloy and gas turbine applications using the same

METHOD OF FABRICATING A TURBINE BLADE

Brush seal with sliding backing plate

Flow path forming plate, vane including this flow path forming plate, gas turbine including this vane, and manufacturing method of flow path forming plate

METHOD FOR PREPREGGING TACKIFIER FOR CMC ARTICLES

Heat shield for signature suppression system

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Fiber blank woven as a single piece by three-dimensional weaving to make a closed box-structure platform out of composite material for a turbine engine fan

Additive-based electroforming manufacturing methods and metallic articles produced thereby

LONG DISTANCE TRANSMISSION OF OFFSHORE POWER

Impingement tubes for gas turbine engine assemblies with ceramic matrix composite components

Aircraft incorporating a thrust recovery system using cabin air

Jet engine with deflector

Turbine nozzle

Insert assembly, airfoil, gas turbine, and airfoil manufacturing method

Systems and methods for inspecting blades or vanes in turbomachinery

Steam turbine cooling unit

THERMALLY DRIVEN SPRING VALVE FOR TURBINE GAS PATH PARTS

INTER-TURBINE DUCTS WITH MULTIPLE SPLITTER BLADES

Systems, methods, and anodes for enhanced ionic liquid bath plating of turbomachine components and other workpieces

Turbine shroud segment with buffer air seal system

Sliding baffle inserts

Slotted ceramic coatings for improved CMAS resistance and methods of forming the same

Combustion section heat transfer system for a propulsion system

Retention assembly for gas turbine engine components

Coated turbine component and method for forming a component

Fluidic machining method and system

System and method for near wall cooling for turbine component

Turbine engine component with deflector

Systems and methods for manufacturing film cooling hole diffuser portion

Plenum for cooling turbine flowpath components and blades

Hybrid thermal barrier coating

Turbine center frame with centering element and spacer element

Gas turbine engine component having engineered vascular structure

Flow passage forming plate, flow passage forming member assembly and vane including the same, gas turbine, manufacturing method of flow passage forming plate, and modification method of flow passage forming plate

NICKEL-BASED SUPERALLOY COMPONENTS AND ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS

ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS

Turbine cooling arrangement

Gas turbine engine component having vascular engineered lattice structure

Component for a gas turbine engine

Centrifugal compressor curved diffusing passage portion

EXHAUST SECTION FOR AN AIRCRAFT GAS TURBINE ENGINE

Turbocharger having a meridionally divided turbine housing and a variable turbine nozzle

Turbine shroud segment with flange-facing perimeter seal

GAS TURBINE ENGINE WITH FILM HOLES

CMC components having microchannels and methods for forming microchannels in CMC components

System and methods of inspecting a component

Gas expander

Gas turbine rotor having structure for adjusting axial clearance, and gas turbine having same

Method of providing cooling structure for a component

PRESSURE REGULATED PISTON SEAL FOR A GAS TURBINE COMBUSTOR LINER

Seal shoe for a hydrostatic non-contact seal device

Turbomachine thermal management

Turbine blade, gas turbine, intermediate product of turbine blade, and method of manufacturing turbine blade

Conduit connection assembly

VARIABLE VANE SEGMENT

Bonding strength enhancement for ceramic coating on high temperature alloy

Fan inlet diffuser housing with conductive composite body

Particle removal device for gas turbine and gas turbine including the same

Vane cooling system

Clad article and method for forming clad article

Flow control structures for turbomachines and methods of designing the same

Tip leakage flow directionality control

Ceramic matrix composite components reinforced for managing multi-axial stresses and methods for fabricating the same

CERAMIC COATING DEPOSITION

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Turbocharger

Thermally compliant heatshield

Coating methods and apparatus

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

Turbine airfoil with thin trailing edge cooling circuit

Ceramic matrix composite turbine exhaust assembly for a gas turbine engine

Airfoil turn caps in gas turbine engines

Reconfigurable maintenance apparatus

High-pressure distributor blading having a variable-geometry insert

TURBINE ENGINE WITH AN EXTENSION INTO A BUFFER CAVITY

Alignment apparatus for coupling diaphragms of turbines

Rotatable vanes

Silicon-based materials containing indium and methods of forming the same

METHOD OF BRAZING AND BRAZED ARTICLE

Blade, cut-back of blade or vane and gas turbine having the same

Selective thermal coating of cooling holes with air flow

Method of melt infiltration utilizing a non-wetting coating for producing a ceramic matrix composite

CMC ply assembly, CMC article, and method for forming CMC article

Components having channels for impingement cooling

Gas turbine engine test stand

Method for positioning core by soluble wax in investment casting

Reverse flow engine architecture

COOLING ASSEMBLY FOR A TURBINE ASSEMBLY

Additive manufactured seal for insert compartmentalization

Airfoil trailing edge segment

Measuring total pressure of a fluid in a turbo machine

Leading edge hybrid cavities and cores for airfoils of gas turbine engine

Motorized apparatus for use with rotary machines

Turbomachine seal system

MULTI-JOINT TOOLS WITH CYLINDRICAL SEGMENTS

Brush seal assembly and method

Turbine Engine Comprising a Lobed Mixer Having Scoops

TURBOMACHINE BLADE SYSTEM

REACTION-TYPE STEAM TURBINE

LARGE AREA RATIO COOLING HOLES

Gas turbine engine article with panel retained by preloaded compliant member

Airfoil with sealed baffle

Airfoil with airfoil piece having radial seal

Airfoil with panel having perimeter seal

Airfoil with seal between endwall and airfoil section

Airfoil with retention pocket holding airfoil piece

Turbine engine component with geometrically segmented coating section and cooling passage

Airfoil with tie member and spring

Airfoil with geometrically segmented coating section

Nozzle maintenance apparatus and method

Minidisk balance flange

THREADED COUPON FOR REPAIR OF SUPERALLOY PART

IN-SITU LASER MACHINING USING MIRRORED OPTICS

Method of manufacturing and inspecting gas washed components in a gas turbine engine

Geared turbofan gas turbine engine architecture

Air metering for blade outer air seals

W-seal shield for interrupted cavity

Manufacture and installation of diffuser flow mixing lobes

Turbine wheel assembly with ceramic matrix composite components

HYBRID COMPONENT AND METHOD OF MAKING

Vane comprising an assembled platform and blade

Bleed valve assembly for a gas turbine engine

Bleed valve assembly for a gas turbine engine

Multi-ply seal

System and method for maintenance of a turbine assembly

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

Methods and features for CMC component repairs

Ceramic matrix composites having monomodal pore size distribution and low fiber volume fraction

System and method for sealing internal channels defined in a component

Method for Scaling Turbomachine Airfoils

Anti-icing apparatus for a nose cone of a gas turbine engine

Retaining ring end gap features

Turbomachine provided with a vane sector and a cooling circuit

Discharge flow duct of a turbine engine comprising a VBV grating with variable setting

GAS TURBINE ENGINE SEALING ARRANGEMENT

Silicon-based materials containing indium and methods of forming the same

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

Internal turbine component electroplating

Gas turbine engine airfoil with showerhead cooling holes near leading edge

Centrifugally activatable seal for a rotary machine and method of assembling same

Floating non-contact seal vertical lip

Turbine blade trailing edge with low flow framing channel

ROTATING BRUSH SLEA WITH BRISTLE SHIELD

Cooling circuit for a multi-wall blade

Cooling circuit for a multi-wall blade

Cooling circuit for a multi-wall blade

Cooling circuit for a multi-wall blade

Engine component with porous section

Blade and gas turbine including the same

INTERNAL COOLING SYSTEM WITH INSERT FORMING NEARWALL COOLING CHANNELS IN AN AFT COOLING CAVITY OF A GAS TURBINE AIRFOIL INCLUDING HEAT DISSIPATING RIBS

Impingement system for an airfoil

Impingement system for an airfoil

TURBOFAN ENGINE COMPRISING AN OVERPRESSURE FLAP AT A FAIRING BEING LOCATED AT THE SECONDARY FLOW CHANNEL

Turbofan engine comprising a fairing being located in the secondary flow channel and having a separate end element

Air metering baffle assembly

Turbine comprising turbine stator vanes of a ceramic matrix composite attached to a turbine case

Direct drive aft fan engine

Engine with face seal

Method of assembly of bi-cast turbine vane

Coating methods and apparatus

Turbine vane with coupon having corrugated surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the sixth stage of a turbine

Cooling system for a gaspath component of a gas powered turbine

Coupon for hot gas path component having manufacturing assist features

COUPON FOR HOT GAS PATH COMPONENT HAVING MANUFACTURING ASSIST FEATURES

Fuel Nozzle of Gas Turbine Combustor and Manufacturing Method Thereof, and Gas Turbine Combustor

Face seal assembly and an associated method thereof

Ni-based alloy having excellent high-temperature creep characteristics, and gas turbine member using the same

Ceramic matrix composite articles having different localized properties and methods for forming same

METHODS AND THIN WALLED REINFORCED STRUCTURES FOR ADDITIVE MANUFACTURING

INLET PARTICLE SEPARATOR SYSTEM WITH PRE-CLEANER FLOW PASSAGE

Airfoil with cast features and method of manufacture

Methods for repairing airfoil trailing edges to include ejection slots therein

METHODS FOR REPAIRING A DAMAGED COMPONENT OF AN ENGINE

CUSTOMIZED BLEND LIMIT FOR GAS TURBINE ENGINE AIRFOILS

METHODS FOR REPAIRING FILM HOLES IN A SURFACE

Impingement cooling system for a gas turbine engine

VARIABLE GEOMETRY TURBOCHARGER TURBINE

METHOD OF MANUFACTURING AND INSPECTING GAS WASHED COMPONENTS IN A GAS TURBINE ENGINE

Turbine component and methods of making and cooling a turbine component

Turbine component and methods of making and cooling a turbine component

Exhaust diffuser

Side channel blower, especially for a vehicle heater

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

Flexible support structure for a geared architecture gas turbine engine

Systems and methods for determining turbomachine engine safe start clearances following a shutdown of the turbomachine engine

Turbine vane gusset

REFRACTORY METAL CORE AND COMPONENTS FORMED THEREBY

CASTING SYSTEM FOR INVESTMENT CASTING PROCESS

Internal rib with defined concave surface curvature for airfoil

Intermediate central passage spanning outer walls aft of airfoil leading edge passage

Toothed component optimization for gas turbine engine

HIGH TEMPERATURE COATING FOR SILICON NITRIDE ARTICLES

Methods for fabricating cast components with cooling channels

Turbomachine including clearance control system

Ingestion seal

Gas turbine engine having a vane assembly

Diffuser of a thermal energy machine and thermal energy machine

Inflow contour for a single-shaft arrangement

LONG, CONTINUOUS ENGRAVING ALONG A ROW OF COOLING HOLES

Turbomachine blade assembly

Seawater Electrolysis Hydrogen Recovery And Power Generation System

Austenitic heat resistant steel and turbine component

Method of manufacturing a component and component

ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT

Article, component, and method of making a component

Ceramic matrix composite

Downhole wet gas compressor processor

Geared turbofan gas turbine engine architecture

Gas turbine engine assemblies with ceramic matrix composite components having undulated features

Gas turbine engine turbine vane baffle and serpentine cooling passage

Turbine shroud with sealed box segments

Gas turbine engine transition duct and turbine center frame

Turbine engine guide vane

APPARATUS FOR MACHINING COMPONENTS OF GAS TURBINE ENGINES

INTEGRATED GAS TURBINE INLET SILENCER AND BLEED HEAT SYSTEM

Internally cooled airfoil

Closed trapped vortex cavity pilot for a gas turbine engine augmentor

TRANSITION-TO-TURBINE SEAL ASSEMBLY

Guide vane made from composite material, comprising staggered attachment flanges for a gas turbine engine

Transition duct assembly

APPARATUS AND METHOD FOR FORMING APPARATUS

Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoil

Ceramic matrix composites having monomodal pore size distribution and low fiber volume fraction

Vane coating apparatus

Link setting assembly and method

Dual snapped cover plate with retention ring attachment

Turbine disc interstage coupling with retention ring features

Retaining ring axially loaded against segmented disc surface

Retaining ring groove submerged into disc bore or hub

Component for a turbine engine with a film hole

Physical vapor deposition on doublet airfoil substrates:controlling the coating thickness

Method for carrying out a sound test of atleast one component and endoscope device used for the same

Method of producing thermal spray powder, manufacture apparatus of thermal spray powder, and thermal spray powder produced by the producing method

GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

AXIAL TURBOMACHINES WITH ROTARY HOUSING AND FIXED CENTRAL ELEMENT

A GUIDE VANE MADE OF COMPOSITE MATERIAL FOR A GAS TURBINE ENGINE, AND IT'S METHOD OF FABRICATION

METHOD FOR TREATING A COMPOSITE PART

Nozzle segment for a gas turbine engine with ribs defining radially spaced internal cooling channels

Turbine airfoil having near-wall cooling insert

METHOD FOR MANUFACTURING A TURBINE ASSEMBLY

Turbine assembly for hydrokinetic torque converter, and method for making the same

EXHAUST SYSTEM FOR GAS TURBINE ENGINE

COMPONENT OF A MOLYBDENUM ALLOY AND METHOD FOR FORMING AN OXIDATION PROTECTION LAYER THEREFOR

System and Method for Rejuvenating Coated Components of Gas Turbine Engines