Combustion duct assembly for gas turbine

TURBINE COMPONENT THERMAL BARRIER COATING WITH CRACK ISOLATING ENGINEERED SURFACE FEATURES

D5/D5A DF-42 integrated exit cone and splash plate

Installation apparatus and related methods for coupling flow sleeve and transition piece

Heat shield for a vane assembly of a gas turbine engine

Combustor liners with rotatable air guiding caps

Calcium-magnesium alumino-silicate (CMAS) resistant thermal barrier coatings, systems, and methods of production thereof

Angled impingement inserts with cooling features

Turbomachine having a seal device

Gas turbine disassembly method

High pressure ratio twin spool industrial gas turbine engine with dual flow high spool compressor

AXISYMMETRIC OFFSET OF THREE-DIMENSIONAL CONTOURED ENDWALLS

Transition duct assembly

Hula seal

WIRE SEAL

Film cooled multi-walled structure with one or more indentations

Seal assembly in a gas turbine engine

Vane

Incident tolerant turbine vane cooling

Engine component

Combustor aft mount assembly

Exhaust mixer for wave rotor assembly

Turbine system with exhaust gas recirculation, separation and extraction

Turbine vane with load shield

Support arrangement for a transition piece of a gas turbine engine

INNER HOUSING HUB FOR A GAS TURBINE

Cooling feed orifices

Support buttress

Dual anti surge and anti rotation feature on first vane support

Angled rail holes

Airfoil profile-shaped seals and turbine components employing same

Gas turbine engine diffuser-combustor assembly inner casing

High compressor exit guide vane assembly to pre-diffuser junction

DISCOURAGER SEAL FOR A TURBINE ENGINE

First stage turbine vane arrangement

Frame segment for a combustor turbine interface

Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation

Transition duct arrangement in a gas turbine engine

Can combustion chamber

D5/D5A DF-42 double walled exit cone and splash plate

Platform cooling circuit for a gas turbine engine component

Gas turbine component with platform cooling

Sealing device for a gas turbine combustor

Sealing arrangement at the interface between a combustor and a turbine of a gas turbine and gas turbine with such a sealing arrangement

Film hole with in-wall accumulator

Casting optimized to improve suction side cooling shaped hole performance

Turbine vane with variable trailing edge inner radius

Beveled coverplate

Gas turbine engines with plug resistant effusion cooling holes

Apparatus and method incorporating a transition AFT support for a gas turbine engine

Method and tool for installation of a transition duct

Cylinder of combustor, method of manufacturing of cylinder of combustor, and pressure vessel

Gas turbine system with a transition duct having axially extending cooling channels

Quick change insert

Joint for sealing a gap between casing segments of an industrial gas turbine engine combustor

Combustor sliding joint

Gas turbine engine architecture with nested concentric combustor

Gas turbine engine end-wall component

Electrospark deposition process for oxidation resistant coating of cooling hole

Method and apparatus for attaching a transition duct to a turbine section in a gas turbine engine

Fan exit guide vane platform contouring

Technique for cooling a root side of a platform of a turbomachine part

Cooling hole for a gas turbine engine component

Combustor with ring part having protrusions and gas turbine including the combustor

Edge treatment for gas turbine engine component

Gas turbine engine stator vane platform cooling

Adjustable transition support and method of using the same

Adjustable cable for exhaust duct liner hanger

Combustor cooling structure

Cooling hole for a gas turbine engine component

Gas turbine engine component with combined mate face and platform cooling

Gas turbine engine component cooling passage and space casting core

Gas turbine transition piece aft frame assemblies with cooling channels and methods for manufacturing the same

Geared turbofan architecture

Child-mother type double-wheel rotor steam power machine

Annular combustion chamber of a gas turbine and gas turbine with such a combustion chamber

Systems and methods for variation of injectors for coherence reduction in combustion system

Ultra compact combustor having reduced air flow turns

Reduced length transition ducts

Gas turbine engine component with platform cooling circuit

AIRFOIL PORTION OF A ROTOR BLADE OR GUIDE VANE OF A TURBO-MACHINE

Combustor seal mistake-proofing for a gas turbine engine

System having layered structure and method of making the same

Gas Turbine Engine With First Turbine Vane Clocking

Combustor seal system for a gas turbine engine

Baffle with flow augmentation feature

Turbine vane arrangement

WELDED DUAL CHAMBER IMPINGEMENT TUBE

Method of repairing a transition duct side seal

Sealing device for providing a seal in a turbomachine

Structural support bracket for gas flow path

Assembly for directing combustion gas

System for sealing between combustors and turbine of gas turbine engine

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

GAS TURBINE ENGINE DUCTING ARRANGEMENT HAVING DISCRETE INSERT

Flexible component providing sealing connection

Transition support system for combustion transition ducts for turbine engines

Turbine and power generation system

Gas turbine engine with soft mounted pre-swirl nozzle

Interface assembly for a combustor

Gas turbine combustor

Impingement cooling arrangement

Transition duct assembly with modified trailing edge in turbine system

Device for cooling a wall of a component

Reverse bulk flow effusion cooling

Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier

Combustor cooling structure

Seal assembly for a gap between outlet portions of adjacent transition ducts in a gas turbine engine

Internally cooled transition duct aft frame with serpentine cooling passage and conduit

Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans

Apparatus and method for servicing gas turbine engines

Turbine engine, such as a turbojet or a turboprop engine

Regeneratively cooled transition duct with transversely buffered impingement nozzles

Cooling chamber for upstream weld of damping resonator on turbine component

Combustor assembly including a transition inlet cone in a gas turbine engine

Combustion chamber of a combustor for a gas turbine

Handheld medical diagnostic device with lancet and sample transfer

Gas turbine engine system and an associated method thereof

Stationary part sealing structure

Sealing mechanism for a regenerative gas turbine combustor

Gas turbine engine combustor with integrated combustor vane having swirler

Air regulation for film cooling and emission control of combustion gas structure

Retention pin and method of forming

Burner seal for gas-turbine combustion chamber head and heat shield

Hot streak alignment for gas turbine durability

Repair method of plate member, plate member, combustor, ring segment, and gas turbine

Transition duct with divided upstream and downstream portions

Modular turbomachine inlet assembly and related inlet transition section

Turbine shroud cooling system

Retention pin and method of forming

Gas turbine engine exhaust fluid passage duct

Gas turbine combustor exit piece with hinged connections

Gas turbine transition inlet ring adapter

Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine

Hot gas path duct for a combustor of a gas turbine

Flow sleeve assembly for a combustion module of a gas turbine combustor

Continuous combustion liner for a combustor of a gas turbine

System for providing fuel to a combustor

Systems and apparatus relating to downstream fuel and air injection in gas turbines

Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition piece

Gas turbine engine impeller system for an intermediate pressure (IP) compressor

Flow conditioner in a combustor of a gas turbine engine

Combustor seal structure and a combustor seal

Gas turbine support element permitting thermal expansion between combustor shell and rotor cover at turbine inlet

Turbine transition piece (TP) apparatus and method

Gas turbine combustion chamber having a flow sleeve with a plurality of integrated segments

Transition piece of combustor, and gas turbine having the same

Gas turbine combustor including burner having plural gaseous fuel manifolds

Combustor connection structure, combustor transition piece, designing method of combustor transition piece and gas turbine

High temperature seal assembly

Turbine nozzle guide vane assembly in a turbomachine

Deformable mounting assembly

Combustor transition

Combustor transition

Ducting arrangement for cooling a gas turbine structure

Housing structure with improved seal and cooling

Mid-turbine frame heat shield

Assembly of an axial turbomachine and method for manufacturing an assembly of this type

GAS TURBINE ENGINE WITH SHORTENED MID SECTION

Gas turbine engine with radial diffuser and shortened mid section

ELECTROSPARK DEPOSITION PROCESS FOR OXIDATION RESISTANT COATING OF COOLING HOLE

Adjustable cable for exhaust duct liner hanger

Platform cooling circuit for a gas turbine engine component

APPARATUS INCLUDING A FLOW CONDITIONER COUPLED TO A TRANSITION PIECE FORWARD END

Turbine engine combustor and stator vane assembly

Combustor and gas turbine provided with same

System and method of supplying fuel to a gas turbine

Combustor transition duct assembly with inner liner

TRANSITION DUCT FOR A GAS TURBINE

Transition duct for a gas turbine

Seal

TRANSITION PIECE FOR A GAS TURBOMACHINE

Turbine vane

COOLING SYSTEM AND METHOD FOR TURBINE SYSTEM

Fixture and method for adjusting workpiece

Convolution seal for transition duct in turbine system

FLEXIBLE SEAL FOR TRANSITION DUCT IN TURBINE SYSTEM

Transition duct with late injection in turbine system

Combustion system including a transition piece and method of forming using a cast superalloy

Transition Piece Cross Sectional Area Convergence Reduction And Selection

Systems And Apparatuses For Hot Gas Flow In A Transition Piece

Method, systems, and apparatuses for transition piece contouring

Transition nozzle combustion system

Combustor with non-circular head end

System and method for recirculating a hot gas flowing through a gas turbine

TANGENTIAL FLOW DUCT WITH FULL ANNULAR EXIT COMPONENT

System for supplying a fuel and a working fluid through a liner to a combustion chamber

Apparatus And System For Directing Hot Gas

Transition Piece Aft-Frame Seals

System for supplying a fuel and working fluid mixture to a combustor

Transition piece aft frame assembly having a heat shield

Mid-section of a can-annular gas turbine engine with a cooling system for the transition

Mid-section of a can-annular gas turbine engine with an improved rotation of air flow from the compressor to the turbine

Platform segment for supporting a nozzle guide vane for a gas turbine and nozzle guide vane arrangement for a gas turbine

Customer bleed air pressure loss reduction

Vane assembly for an axial flow turbine

Multi-channel cooling plenum

Late lean injection system transition piece

Methods and systems for cooling a transition nozzle

Combustor with acoustic liner

Component and turbomachine having a component

Radial inflow gas turbine engine with advanced transition duct

Member assembling apparatus of rotary machine

Convolution seal for transition duct in turbine system

Flexible metallic seal for transition duct in turbine system

Leaf seal for transition duct in turbine system

Transition piece aft frame with fuel injection apertures

Cooling structure for recovery-type air-cooled gas turbine combustor

Flashback resistant tubes for late lean injector and method for forming the tubes

MULTI-FLUID TURBINE ENGINE

Transition nozzle

FILM COOLED COMBUSTION LINER ASSEMBLY

Turbine system

AERO-DERIVATIVE GAS TURBINE ENGINE WITH AN ADVANCED TRANSITION DUCT COMBUSTION ASSEMBLY

Casing for a gas turbine engine

Transition piece of combustor, gas turbine having the same, and producing method for transition piece

Transitional region for a secondary combustion chamber of a gas turbine

Turbomachine seal assembly

Seal end attachment

Two stage serial impingement cooling for isogrid structures

Ceramic matrix composite combustor vane ring assembly

Support assembly for transition duct in turbine system

Support assembly for transition duct in turbine system

Methods and systems for cooling a transition nozzle

Brazed turbine seal

COMBUSTOR ASSEMBLY FOR USE IN A TURBINE ENGINE AND METHODS OF ASSEMBLING SAME

Methods and systems for transferring heat from a transition nozzle

Flow Machine

HINGE SEAL

Seal assembly for gas turbine

MOUNT DEVICE FOR TRANSITION DUCT IN TURBINE SYSTEM

System for mounting combustor transition piece to frame of gas turbine engine

Impingement sleeve and methods for designing and forming impingement sleeve

COMBUSTION LINER AND TRANSITION PIECE

Load member for transition duct in turbine system

INJECTOR APPARATUS

Turbine combustion system transition piece side seals

Turbine combustion system transition seals

Turbine combustion system coupling with adjustable wear pad

Inspection system for a combustor of a turbine engine

TWO-PIECE SIDE SEAL WITH COVERS

Hula seal with preferential cooling having spring fingers and/or adjacent slots with different widths

Method of forming a multi-panel outer wall of a component for use in a gas turbine engine

Method of fabricating a nearwall nozzle impingement cooled component for an internal combustion engine

Interface between a combustor basket and a transition of a gas turbine engine

GAS TURBINE ENGINE TRANSITION DUCTS

Communicating structure between adjacent combustors and turbine portion and gas turbine

Turbine combustion system cooling scoop

Method of sealing combustor liner and turbine nozzle interface

Aft frame and method for cooling aft frame

Impingement sleeve and methods for designing and forming impingement sleeve

Combustor mixing joint with flow disruption surface

Method and apparatus for mounting transition piece in combustor

Combustor assembly for use in a turbine engine and methods of fabricating same

Thermally isolated wall assembly

System for sealing a gap between a transition and a turbine

METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER IN COMBUSTOR

SUPPORT BETWEEN TRANSITION PIECE AND IMPINGEMENT SLEEVE IN COMBUSTOR

TRANSITION PIECE IMPINGEMENT SLEEVE FOR A GAS TURBINE

Damage-repairing method of transition piece and transition piece

ASSEMBLY AND METHOD FOR PREVENTING FLUID FLOW

SYSTEM FOR DAMPING VIBRATION IN A GAS TURBINE ENGINE

Transition duct

Combustor assemblies for use in turbine engines and methods of assembling same

Mounting/dismounting jig for combustor tail pipe and tail pipe installation method

Transition piece between combustor liner and gas turbine

METHOD OF REPAIRING A TRANSITION PIECE OF A GAS TURBINE ENGINE

Seal arrangement

Turbine transition component formed from a two section, air-cooled multi-layer outer panel for use in a gas turbine engine

Turbine transition component formed from an air-cooled multi-layer outer panel for use in a gas turbine engine

Transition Piece Sealing Assembly With Seal Overlay

Transition Piece Sealing Assembly

Gas turbine engine systems involving cooling of combustion section liners

Shim for sealing transition pieces

Tunable transition duct side seals in a gas turbine engine

Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece

Turbomachine including a ceramic matrix composite (CMC) bridge

TURBOMACHINE HAVING AN ANNULAR COMBUSTION CHAMBER

Transitional region for a combustion chamber of a gas turbine

Apparatus and method for mixing fuel in a gas turbine nozzle

Combustor liner assembly with enhanced cooling system

FUEL INJECTION ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME

Stepped inlet ring for a transition downstream from combustor basket in a combustion turbine engine

Guide vane system for a turbomachine having segmented guide vane carriers

COMBUSTOR TRANSITION PIECE WITH DILUTION SLEEVES AND RELATED METHOD

Cooling arrangement for a turbine component

Compressed air plenum for a gas turbine engine

Seal assembly for controlling fluid flow

Fan downstream guide vanes of a turbofan engine

Mesh cooled conduit for conveying combustion gases

Replaceable orifice for combustion tuning and related method

Damping resonator with impingement cooling

Liner aft end support mechanisms and spring loaded liner stop mechanisms

Spring loaded seal assembly for turbines

Cooled conduit for conveying combustion gases

System for cooling turbine combustor transition piece

GAS TURBINE COOLING

Reduced Pressure Loss Transition Support

Height ratios for a transition piece of a combustor

Combustor liner cooling at transition duct interface and related method