CMC ply overlap ingestion restrictor

Gas turbine engine with compliant layer for turbine shroud mounts

Intercomponent seal for a gas turbine engine

Apparatus, turbine nozzle and turbine shroud

Impingement holes for a turbine engine component

Gas turbine engine with a turbine blade tip clearance control system

Turbomachine module

Variable thickness core for gas turbine engine component

Stator heat shield for a gas turbine, gas turbine with such a stator heat shield and method of cooling a stator heat shield

System and method for an assembled ring shroud

Core component having toroidal structures

Axial flowing cooling passages for gas turbine engine components

Full hoop blade track with interstage cooling air

Gas turbine engine with health monitoring system

Gas turbine engine components with optimized leading edge geometry

Cooled containment case using internal plenum

Gas turbine engine blade outer air seal profile

Article having multi-layered coating

METHOD AND SYSTEM FOR VARYING TIP CLEARANCE GAP USING AN ACTUATED SHROUD

System and method for cooling turbine shroud

Segmented micro-channel for improved flow

System and method for cooling turbine shroud trailing edge

Seal segment low pressure cooling protection system

Method of sizing a cavity in a part

TURBINE ABRADABLE LAYER WITH AIRFLOW DIRECTING PIXELATED SURFACE FEATURE PATTERNS

Blade outer air seal with integrated air shield

Method and apparatus for cooling gas turbine engine component

Embedded cap probe

Housing structure of a turbomachine with heat protection shield

Thermal management article

High response turbine tip clearance control system

Run-in coating for an outer air seal of a turbomachine

Blade outer air seal with seal arc segment having secondary radial supports

Compliant shroud for gas turbine engine clearance control

Pin supported CMC shroud

Impingement tubes for CMC seal segment cooling

RING SEGMENT COOLING STRUCTURE AND GAS TURBINE HAVING THE SAME

Device and method for influencing the temperatures in inner ring segments of a gas turbine

SHROUDED TURBINE BLADE

Ceramic matrix composite component and process of producing a ceramic matrix composite component

Cooling hole patterned surfaces

Multi-piece shroud hanger assembly

Leaf seal reach over spring with retention mechanism

Shroud assembly for a gas turbine engine

Shroud assembly for a gas turbine engine

Blade outer air seal

Shrouds and methods for forming turbine components

Multi-flow cooling passage chamber for gas turbine engine

Turbine shroud with sealing features

Gas turbine tip clearance control assembly

Adaptive blade tip seal assembly

Gas turbine compressor with adaptive blade tip seal assembly

SEAL ARRANGEMENT FOR COMPRESSOR OR TURBINE SECTION OF GAS TURBINE ENGINE

Ceramic matrix composite ring shroud retention methods-finger seals with stepped shroud interface

Ceramic matrix composite materials with rare earth phosphate fibers and methods for preparing the same

Coated seal slot systems for turbomachinery and methods for forming the same

Turbine band anti-chording flanges

Using inserts to balance heat transfer and stress in high temperature alloys

Ceramic matrix composite including silicon carbide fibers in a ceramic matrix comprising a max phase compound

Turbine shroud assembly

Turbine abradable layer with composite non-inflected bi-angle ridges and grooves

BLADE OUTER AIR SEAL COMPONENT WITH VARYING THERMAL EXPANSION COEFFICIENT

Blade outer air seal fin cooling assembly and method

Cooling channels for gas turbine engine component

Blade outer air seal for a gas turbine engine

Turbine shroud assembly and method for loading

System and method for supporting a turbine shroud

Flexibly mounted ceramic matrix composite seal segments

Turbine shroud having ceramic matrix composite seal segment

Overlapping herringbone filmhole patterned surfaces

Turbine shroud segment with side perimeter seal

Seal segment for a gas turbine engine

MANUFACTURING OF TURBINE SHROUD SEGMENT WITH INTERNAL COOLING PASSAGES

Axial Flow Turbine

Shroud assembly for gas turbine engine

Blade or vane row and gas turbine

Motive air conditioning system for gas turbines

Turbine shroud with movable attachment features

Turbine shroud with clamped flange attachment

Turbine shroud segment with integrated cooling air distribution system

Turbine shroud segment with load distribution springs

Turbine shroud segment with buffer air seal system

Turbine shroud segment with flange-facing perimeter seal

Gas turbine rapid response clearance control system with annular piston

Turbine component thermal barrier coating with depth-varying material properties

Method for integral joining infiltrated ceramic matrix composites

Turbine component thermal barrier coating with crack isolating engineered groove features

Fire containment coating system for titanium

Machinable CMC insert

Machinable CMC insert

Machinable CMC insert

Machinable CMC insert

Shroud cartridge having a ceramic matrix composite seal segment

Pressure activated seals for a gas turbine engine

Split line flow path seals

Monolithic ceramic rods to enable cooling holes in CMC

Blade and shroud with socket for a compressor of an axial turbomachine

Support assembly for a gas turbine engine

Heat exchanger seal segment for a gas turbine engine

Support assembly for a gas turbine engine

System for thermally shielding a portion of a gas turbine shroud assembly

Shroud retention system with retention springs

Wall cooling arrangement for a gas turbine engine

Shroud retention system with keyed retention clips

Cam-follower active clearance control

Method of making a turbine shroud

Composite keystoned blade track

Blade outer air seal mount

Retention clip for a blade outer air seal

System for thermally isolating a turbine shroud

Turbine shroud segment assembly with expansion joints

SILICON OXYCARBIDE-BASED ENVIRONMENTAL BARRIER COATING

Method for additively constructing internal channels

Blade outer air seals with channels

Control rings

Seal arrangement for turbine engine component

Turbomachine having a seal device

Compliant attachment for an organic matrix composite component

Axial skin core cooling passage for a turbine engine component

Surface-aided melt infiltration for producing a ceramic matrix composite

Meter plate for blade outer air seal

Blade outer air seal cooling passage

Keystoned blade track

Full hoop blade track with flanged segments

Seal for a gas turbine engine assembly

Seals for a gas turbine engine assembly

Gas turbine engine brush seal with supported tip

Seal

Shroud assembly and shroud for gas turbine engine

Energy damping system for gas turbine engine stationary vane

Heat shields for air seals

Shroud assembly and shroud for gas turbine engine

MANUFACTURING OF TURBINE SHROUD SEGMENT WITH INTERNAL COOLING PASSAGES

Wrapped dog bone seal

Static axial brush seal with dual bristle packs

System for cooling a turbine engine

Turbine ring assembly with sealing

Turbine ring assembly with inter-sector connections

Compliant rail hanger

TURBINE

System for cooling a turbine shroud

Multi-element inner shroud extension for a turbo-machine

Turbine engine component with diffuser holes

Turbocharger turbine containment structure

Turbine shroud with axially separated pressure compartments

Floating panel for a gas powered turbine

Engine component

Segmented turbine shroud with sealing features

Tapered gas turbine segment seals

Axially divided inner ring for a turbomachine and guide vane ring

Tortuous cooling passageway for engine component

Blade tip clearance control system including BOAS support

Gas turbine engine airfoil component platform seal cooling

BOAS thermal protection

Blade outer air seal having angled retention hook

Seals for gas turbine engines

CMC turbine components and methods of forming CMC turbine components

Blade outer air seal made of ceramic matrix composite

Seal for gas turbine engine

Plug seal for gas turbine engine

Feather seal

Casing structure with connection tabs

Wall for a hot gas channel in a gas turbine

Turbine shroud assembly

Sliding seal

Protective panel and frame therefor

Blade outer air seal with cooling holes

Gas turbine engine component providing prioritized cooling

BOAS with radial load feature

Blade track assembly with turbine tip clearance control

Shroud assembly for a turbine engine

Clearance control assembly

Hot gas path component

Waveguide

Mini blind stator leakage reduction

COOLING FEATURE FOR A TURBINE ENGINE COMPONENT

Turbine shroud sealing architecture

Hanger system for a turbine engine component

Reversible flow blade outer air seal

Self-opening cooling passages for a gas turbine engine

Stiffness controlled abradeable seal system and methods of making same

Gas turbine engine ceramic component assembly and bonding material

Blade outer air seal support structure

Turbine blade or vane having a stepped and beveled platform edge

Internal shroud for a compressor of an axial-flow turbomachine

Additive process for an abradable blade track used in a gas turbine engine

Stator shroud systems

PASSIVE CONTROL OF GAS TURBINE CLEARANCES USING CERAMIC MATRIX COMPOSITES INSERTS

Turbine shroud with locating inserts

Gas turbine engine with seal inspection features

Multi-piece seal

Segmented seal

Turbine shroud with biased blade track

Shroud segment retainer

Carriers for turbine components

Gas turbine ring segment cooling apparatus

Thermally protected seal assembly

Gas turbine nozzles with embossments in airfoil cavities

Double-jet film cooling structure and method for manufacturing same

Beveled coverplate

Dual-ended brush seal assembly and method of manufacture

Actively cooled blade outer air seal

Rapid response clearance control system for gas turbine engine

Flexible feather seal for blade outer air seal gas turbine engine rapid response clearance control system

Smart active clearance control between a rotor blade and a shroud

Inner stage turbine seal for gas turbine engine

Aerodynamic track fairing for a gas turbine engine fan nacelle

Compressor case snap assembly

Ceramic coating system and method

Air-driven particle pulverizer for gas turbine engine cooling fluid system

Cost effective manufacturing method for GSAC incorporating a stamped preform

Adjustable blade outer air seal apparatus

Arcuate directionally solidified components and manufacture methods

Method of manufacturing gas turbine engine element having at least one elongated opening

Mid-turbine frame and gas turbine engine including same

Multi-lobed cooling hole

Turbine ring for a turbomachine

Gas turbine engine component having shaped pedestals

Annular ring assembly for shroud cooling

Actuator for gas turbine engine blade outer air seal

Assembly for sealing a gap between components of a turbine engine

Composite turbine components adapted for use with strip seals

Cooling hole for a gas turbine engine component

Gas turbine engine component cooling channels

Additive manufacturing method for the addition of features within cooling holes

Edge treatment for gas turbine engine component

Contoured blade outer air seal for a gas turbine engine

Gas turbine engine seal assembly

Gas turbine engine component having variable width feather seal slot

Gas turbine engine stator vane assembly with split shroud

Gas turbine engine component paired film cooling holes

Coating for isolating metallic components from composite components

Turbine shroud with sealed blade track

Segmented turbine shroud with seals

Gas turbine engine component with combined mate face and platform cooling

Gas turbine engine component having curved turbulator

Low leakage duct segment using expansion joint assembly

Fan case

METHODS OF MANUFACTURING A SHROUD ABRADABLE COATING

Flow distribution blading comprising an improved sealing plate

Shroud assembly for turbine engine

Dual walled seal assembly

Casing arrangement for a gas turbine

Repair material preform

Turbine casing made of two materials

Blade outer air seal with cored passages

Flow deflector arrangement

Forward step honeycomb seal for turbine shroud

Turbine shroud segment with inter-segment overlap

Hybrid blade outer air seal for gas turbine engine

Turbine rotor blades with platform cooling arrangements

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

Sealing device for providing a seal in a turbomachine

Method for manufacturing a turbomachine casing from a composite material and associated casing

Gas turbine

Gas turbine

Corrosion-resistant abradable covering

Multipurpose electrical discharge machining tool for a ring sector

Ceramic matrix composite component and method of forming thereof

Turbine engine stator wall covered in an abradable coating

Inner ring of a fluid flow machine and stator vane array

Tapered thread for gas turbine shroud

Microchannel exhaust for cooling and/or purging gas turbine segment gaps

Re-use of internal cooling by medium in turbine hot gas path components

Arrangement for cooling a component in the hot gas path of a gas turbine

Thermal management article and method of forming the same, and method of thermal management of a substrate

Seal between static turbine parts

Sealing element of an axial turbomachine

Shroud assembly and seal for a gas turbine engine

Method for applying heat resistant protection components onto a surface of a heat exposed component

Carrier ring

Method for disassembly and assembly of a rotor of a gas turbine

Methods for removing barrier coatings, bondcoat and oxide layers from ceramic matrix composites

Dovetail retention system for blade tracks

Seal member, turbine, and gas turbine

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Blade track assembly, components, and methods

Turbomachine, sealing segment, and guide vane segment

Blade outer air seal assembly and support

Shroud block segment for a gas turbine

Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement

Blade track assembly with turbine tip clearance control

Segment of an abradable ring seal for a turbomachine, and process for the manufacture of such a piece

Piece of abradable material for the manufacture of a segment of an abradable ring seal for a turbomachine, and process for the manufacture of such a piece

SHROUD ARRANGEMENT FOR A FLUID FLOW MACHINE

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

Dual source cooling air shroud arrangement for a gas turbine engine

Shroud arrangement for a gas turbine engine

Shroud arrangement for a gas turbine engine

Stator component with segmented inner ring for a turbomachine

Gas turbine thermal shroud with improved durability

Gas turbine shroud assemblies

Blade track assembly with turbine tip clearance control

Method and apparatus for fabrication and repair of thermal barriers

Twist prevention for turbomachinery

CMC turbine engine component

Active turbine or compressor tip clearance control

Blade outer air seal surface

Consumable assembly mistake proofing tool for a gas turbine engine

Cooling structure for turbomachine