FAN CASING OR LINER WITH INTERCHANGEABLE TIP TREATMENT SEGMENTS

TURBINE SEALING RING THAT IS REMOVABLE UPSTREAM

CMC COMPONENT WITH COOLING CAVITY COVER PLATE

THERMAL BARRIER COATING FOR EDGE COMPONENT

SEALING ASSEMBLY AND GAS TURBINE

OUTER AIR SEAL (OAS) WITH IMPROVED MATING WITH FIRST STAGE CASING

TURBINE SHROUD AND TURBOMACHINE WITH COOLING CIRCUIT

SEAL SUPPORT ASSEMBLY FOR A TURBINE ENGINE

VARIABLE FLOWPATH CASINGS FOR BLADE TIP CLEARANCE CONTROL

COMPLIANT SHROUD DESIGNS WITH VARIABLE STIFFNESS

Outer Air Seal (OAS) with Improved Mating with First Stage Casing

TURBINE SHROUD ASSEMBLY WITH ANGLED COOLING HOLES

PASSIVE CONTROL OF GAS TURBINE CLEARANCES USING CERAMIC MATRIX COMPOSITES INSERTS

TRAVEL STOP FOR A TIP CLEARANCE CONTROL SYSTEM

SHROUD HANGER ASSEMBLY

Composite Component Modifications

Manufacturing of Wear Resistant Coatings

RADIALLY RETRACTABLE OUTER AIR SEAL

SHARED LOAD PATH BLADE OUTER AIR SEAL

BLADE TIP CLEARANCE CONTROL USING MATERIAL WITH NEGATIVE THERMAL EXPANSION COEFFICIENTS

SEAL SUPPORT ASSEMBLY FOR A TURBINE ENGINE

TURBINE TIP SHROUD REMOVAL FEATURE

Segmented compressor inner band for variable vanes in gas turbine engines

TURBINE WITH A SHROUD RING AROUND ROTOR BLADES AND METHOD OF LIMITING LEAKAGE OF WORKING FLUID IN A TURBINE

Variable guide vane assembly for gas turbine engine

Thrust reverser assembly for a turbojet engine

Ram air driven blade tip clearance control system for turboprop engines

Substrate Edge Configurations for Ceramic Coatings

BLEED PASSAGE ARRANGEMENT FOR A GAS TURBINE ENGINE SHROUD

Passive control of gas turbine clearances using ceramic matrix composites inserts

Turbine engine assembly comprising a casing and an aerodynamic treatment member at the blade tips, and corresponding turbine engine

Turbine vane having sealing assembly, turbine, and turbomachine including same

Turbine vane platform sealing assembly, and turbine vane and gas turbine including same

Air seal system with backside abradable layer

STRUCTURE OF COOLING TURBINE VANE SHROUD AND MANUFACTURING METHOD THEREOF

Bleed passage arrangement for a gas turbine engine shroud

Turbine ring assembly mounted on a cross-member

Turbine ring assembly for a turbomachine

Variable flowpath casings for blade tip clearance control

Variable guide vane assembly for gas turbine engine

TURBINE ENGINE WITH A ROTOR SEAL ASSEMBLY

Active clearance control of fan blade tip closure using a variable sleeve system

Shroud pin for gas turbine engine shroud

Compliant shroud designs with variable stiffness

Air seal system with backside abradable layer

Ring segment and turbomachine including same

CMC ARC SEGMENT INTERFACE GAP FLOW BLOCKER

Electrical connector arrangement for electronic component of turbomachine

Annular assembly for a turbomachine turbine

Turbine shroud assembly with pinned shroud attachment

Shroud pin for gas turbine engine shroud

Clearance control system for a gas turbine engine

Vane forward rail for gas turbine engine assembly

System for controlling blade clearances within a gas turbine engine

Compressor to minimize vane tip clearance and gas turbine including the same

Curved beams stacked structures-compliant shrouds

Turbomachine component retention

Mounting of a sealing ring on an aeronautical turbine engine

Impeller shroud assembly and method for operating same

Gas turbine engine components with metallic and ceramic foam for improved cooling

Ceramic matrix composite turbine shroud shaped for minimizing abradable coating layer

Turbine for a turbine engine

TURBINE TIP SHROUD REMOVAL FEATURE

CMC component with integral cooling channels and method of manufacture

Clearance control structure for a gas turbine engine

Turbomachine rotary assembly comprising an annular clamping part

Gas turbine engine with compressor bleed system for combustor start assist

Turbine shroud assembly

Constant cross section mandrel for CMC components

SEALING OF A TURBINE RING MADE OF A CERAMIC MATRIX COMPOSITE

Outer air seal with kerf slots

Turbomachine stator assembly comprising an inner shroud having upstream and downstream portions assembled by axial translation

STATOR APPARATUS FOR A GAS TURBINE ENGINE

Turbine shroud assembly with forward and aft pin shroud attachment

Element for distributing a cooling fluid and associated turbine ring assembly

Pin member for turbine

Compliant shroud designs with variable stiffness

Turbine engine with a rotor seal assembly

Segmented augmented turbine assembly

Turbine shroud assembly with radially and axially biased ceramic matrix composite shroud segments

Flowpath assembly for gas turbine engine

Gas turbine engine component

Seal assembly with seal arc segment

PASSIVE CONTROL OF GAS TURBINE CLEARANCES USING CERAMIC MATRIX COMPOSITES INSERTS

Variable thickness machinable coating for platform seals

Attachment of an acoustic shroud to a housing shell for an aircraft turbine engine

Airfoil assembly

Annular shroud assembly

Turbine blade tip shroud surface profiles

Outlet seal, outlet seal set, and gas turbine

Flow channel forming plate, blade and gas turbine including this, and method of manufacturing flow channel forming plate

Fairing assembly

Ring segment and turbomachine including same

Ring segment and turbomachine including same

Stator apparatus for a gas turbine engine

Gas turbine engine actuation device

Outlet guide vane assembly in gas turbine engine

Ring segment and gas turbine including the same

Inner shroud assembly for gas turbine engine variable vane system

Gas turbine ring assembly comprising ring segments having integrated interconnecting seal

Split shroud for vibration reduction

FAST RESPONSE ACTIVE CLEARANCE CONTROL SYSTEM WITH PIEZOELECTRIC ACTUATOR

Automated device for inserting sealing pads into one of the sectors of a turbine stator of a turbine

Method for manufacturing an engine component with a cooling duct arrangement and engine component

Assembly for a turbomachine turbine

Compliant retention system for gas turbine engine

Turbine shroud with containment features

Turbine shroud cooling

Method for assembling and disassembling a turbine ring assembly

Turbine with a shroud ring around rotor blades and method of limiting leakage of working fluid in a turbine

Double box composite seal assembly with insert for gas turbine engine

Turbomachine stator sector having flexible regions subjected to high stress

Silicon oxycarbide-based environmental barrier coating

Turbine engine with a shroud assembly

Environmental barrier coating

CMC shroud segment with interlocking mechanical joints and fabrication

Gas turbine engine component

Assembly for a turbomachine turbine and associated turbomachine

Systems and apparatus to control deflection mismatch between static and rotating structures

Internal turbomachine casing having improved thermal insulation

Turbine ring assembly with curved rectilinear seatings

Sealing between a rotor disc and a stator of a turbomachine

Seal assembly with reduced pressure load arrangement

Turbine ring assembly having indexed flanges

Gas turbine stator

Turbine shroud sector with cooled sealing strips

Substrate edge configurations for ceramic coatings

Turbine shroud assembly with ceramic matrix composite components having stress-reduced pin attachment

Turbine shroud ring segments with ceramic matrix composite components

Seal segment for a turbine, assembly for externally delimiting a flow path of a turbine, and stator/rotor seal

Environmental barrier coating

VANE SUPPORT SYSTEM

Thermally isolated rotor systems and methods

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

Sealing apparatus for a turbomachine, seal-carrier ring element for a sealing apparatus, and turbomachine

COATING FOR GAS TURBINE ENGINE COMPONENTS

Seal assembly with distributed cooling arrangement

Seal assembly with reduced pressure load arrangement

Ring segment and gas turbine including the same

Airfoil with cooling hole

Ceramic matrix composite heat shield for use in a turbine vane and a turbine shroud ring

Turbine engine with reused secondary cooling flow

Engine components with cooling holes having tailored metering and diffuser portions

Turbine shroud assembly with multi-piece support for ceramic matrix composite material seal segments

Turbine shroud assembly with case captured seal segment carrier

Element for distributing a cooling fluid and associated turbine ring assembly

Turbine shroud assembly with hangers for ceramic matrix composite material seal segments

SINTERED-BONDED HIGH TEMPERATURE COATINGS FOR CERAMIC TURBOMACHINE COMPONENTS

Turbine shroud assembly with pinned attachment supplements for ceramic matrix composite component mounting

Gas turbine engine flowpath component including vectored cooling flow holes

Turbine ring assembly with inter-sector sealing

Assembly with pin-mounted ceramic matrix composite material components

Unitary body turbine shrouds including shot peen screens integrally formed therein and turbine systems thereof

Vane for gas turbine engine

Turbine shroud cartridge assembly with sealing features

Turbine shroud assembly with ceramic matrix composite blade track segments and full hoop carrier

Turbine shroud assembly with case captured seal segment carrier

Turbine shroud assembly with flange mounted ceramic matrix composite turbine shroud ring

Mateface for blade outer air seals in a gas turbine engine

Turbine shroud assembly with sheet-metal sealing features

Turbomachinery sealing apparatus and method

TURBINE TIP SHROUD ASSEMBLY WITH PLURAL SHROUD SEGMENTS HAVING INTERNAL COOLING PASSAGES

Ring-segment surface-side member, ring-segment support-side member, ring segment, stationary-side member unit, and method

Boas arrangement with double dovetail attachments

Blade outer air seal arrangement and method of sealing

Impingement cooling with impingement cells on impinged surface

Aspirating face seal assembly for a rotary machine

Turbine shroud segment having a seal segment perimeter seal with separated buffer cavities

Double box composite seal assembly with fiber density arrangement for gas turbine engine

Double box composite seal assembly for gas turbine engine

Double box composite seal assembly with insert for gas turbine engine

CMC component with integral cooling channels and method of manufacture

Blade outer air seal with inward-facing dovetail hooks and backside cooling

Intersegment seal for CMC boas assembly

Axial retention geometry for a turbine engine blade outer air seal

Seal arrangement for turbine engine component

Spline for a turbine engine

Compressor section of gas turbine engine including hybrid shroud with casing treatment and abradable section

Multi-piece carrier assembly for mounting ceramic matrix composite seal segments

Shroud assembly of gas turbine

Heatshield with damper member

CERAMIC MATRIX COMPOSITE BLADE OUTER AIR SEAL

Turbine shroud with ceramic matrix composite seal segments mounted to metallic carriers

Modulated turbine component cooling

Containment case active clearance control structure

Oxidation activated cooling flow

Sealing arrangement between turbine shroud segments

Double box boas and carrier system

Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement

Airfoils and core assemblies for gas turbine engines and methods of manufacture

Turbo compressor

Shroud attaching structure, shroud assembly, and shroud element in gas turbine

Conformal seal and vane bow wave cooling

Isolation seals for gas turbine engines

Boas flow directing arrangement

Ceramic matrix composite hanger heat shield

Sintered-bonded high temperature coatings for ceramic turbomachine components

Systems and methods for manufacturing film cooling hole diffuser portion

Adaptive case for a gas turbine engine

Seal ring for turbine shroud in gas turbine engine with arch-style support

CONTROL RINGS

Intersegment seal for blade outer air seal

Sealing surface for ceramic matrix composite blade outer air seal

Heatshield for a gas turbine engine

Turbine ring assembly

CMC BOAS with internal support structure

BOAS carrier with cooling supply

Turbine shroud cooling

Non-continuous abradable coatings

Conformal seal and vane bow wave cooling

Ceramic matrix composite assembly with compliant pin attachment features

Divot pattern for thermal barrier coating

Mate face arrangement for gas turbine engine components

Unitary body turbine shroud for turbine systems

Unitary body turbine shrouds including internal cooling passages

Unitary body turbine shrouds including structural breakdown and collapsible features

Method and device for adjusting the clearance between a rotor and a concentric stator of an aircraft turbine engine

Frustic load transmission feature for composite structures

Shroud and shroud assembly process for variable vane assemblies

BOAS assemblies with axial support pins

Passive blade tip clearance control system for gas turbine engine

Compressor section of gas turbine engine including hybrid shroud with casing treatment and abradable section

Shroud sealing for a gas turbine engine

Turbine assembly with ring segments

Seal coats to prevent silicon loss during re-melt infiltration of Si containing composites

Turbine engine with floating shrouds

Seal assembly with ductile wear liner

Coating for improved surface finish

BOAS control structure with center support hook

CMC honeycomb base for abradable coating on CMC BOAS

Rotor overspeed protection assembly

Gas turbine engine arc segments with arced walls

Aspirating face seal assembly for a rotary machine

Aspirating face seal assembly for a rotary machine

Beveled coverplate

Seal assembly for a turbo machine

Cost effective manufacturing method for GSAC incorporating a stamped preform

Turbine shroud cooling

Substrate edge configurations for ceramic coatings

Retention clip for a blade outer air seal

Inter-component seals for ceramic matrix composite turbine vane assemblies

TURBINE SHROUD WITH LAPPED SEAL SEGMENTS

Turbine shroud segment with flange-facing perimeter seal

Turbine snap in spring seal

Turbine ring assembly

System and method for shroud cooling in a gas turbine engine

Passive control of gas turbine clearances using ceramic matrix composites inserts

Turbine shroud assemblies for gas turbine engines

Dual-ended brush seal assembly and method of manufacture

Blade outer air seal fin cooling assembly and method

Blade outer air seal laminate T-joint

Impingement cooling for gas turbine engine component

Containment case active clearance control structure

FEATHERSEAL FORMED OF CMC MATERIALS

Constant cross section mandrel for CMC components

Method of pressure sintering an environmental barrier coating on a surface of a ceramic substrate

Method of manufacturing BOAS enhanced heat transfer surface

Multi-piece carrier assembly for mounting ceramic matrix composite seal segments

Blade outer air seal with separate forward and aft pressure chambers

Ring segment and gas turbine

CMC component including directionally controllable CMC insert and method of fabrication

Integrated seal and wear liner

CMC BOAS intersegment seal

Turbine blade tip shroud

ADDITIVE MANUFACTURING METHOD FOR THE ADDITION OF FEATURES WITHIN COOLING HOLES

Blade outer air seal formed of laminate and having radial support hooks

Sealing assembly for a turbine rotor of a turbomachine and a turbine of a turbomachine comprising such an assembly

Axially preloaded seal

Spline seal with cooling features for turbine engines

Additively manufactured nested segment assemblies for turbine engines

Cooling hole with shaped meter

Steam turbine and method of manufacturing steam turbine

Rotor bore conditioning for a gas turbine engine

BLADE OUTER AIR SEAL REINFORCEMENT LAMINATE

Blade outer air seal with circumferential hook assembly

Structural support for blade outer air seal assembly

Turbomachinery sealing apparatus and method

Sealing surface for ceramic matrix composite blade outer air seal

Fairing assembly

Attachment block for blade outer air seal providing convection cooling

Attachment block for blade outer air seal providing impingement cooling

Turbine shroud including plurality of cooling passages

Turbine shroud segment with side perimeter seal

Seal coating

Turbine shroud segment with load distribution springs

Turbine shroud having ceramic matrix composite seal segment

AIRFOIL HAVING ANGLED TRAILING EDGE SLOTS

Component for a turbine engine with a cooling hole

Turbomachine modification apparatus and method

Fan case assembly for gas turbine engine

Hot section dual wall component anti-blockage system

Aircraft turbine engine sealing module

Attachment body for blade outer air seal

Segmented ring for installation in a turbomachine

Gas turbine engine component

Turbine shroud block segment with near surface cooling channels

COOLING ARRANGEMENT WITH CRENELLATION FEATURES FOR GAS TURBINE ENGINE COMPONENT

BOAS thermal protection

Turbine shroud with forward case and full hoop blade track

Composite component modifications