Method and system for providing a splitter to improve the recovery of compressor discharge casing

Stationary vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such stationary vane assembly

Combustor and gas turbine having the same

Preferential cooling of gas turbine nozzles

Tangential combustor with vaneless turbine for use on gas turbine engines

Assembly for directing combustion gas

TRANSITION SUPPORT SYSTEM FOR COMBUSTION TRANSITION DUCTS FOR TURBINE ENGINES

Radial turbine engine floating ring seal

Sealing between a combustion chamber and a turbine nozzle in a turbomachine

GAS TURBINE TRANSITION PIECE AIR BYPASS BAND ASSEMBLY

TUNABLE TRANSITION PIECE AFT FRAME

TURBOMACHINE NOZZLE

Plates having cooling channels, and method for welding the plates and increasing a dimension of the cooling channels adjacent the welded section

Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine

Gas turbine

Turbulated aft-end liner assembly and cooling method

One-stage stator vane cooling structure and gas turbine

Impingement cooling plate for a hot gas duct of a thermal machine

THERMAL MACHINE

Gas turbine having an improved cooling architecture

APPARATUS AND METHOD FOR TURBINE ENGINE COOLING

Combustor interface sealing arrangement

Circumferentially self expanding combustor support for a turbine engine

Gas turbine transition duct profile

Gas turbine

SEAL

Combustor turbine interface for a gas turbine engine

Seal system between transition duct exit section and turbine inlet in a gas turbine engine

Impingement cooled transition piece aft frame

Acoustically stiffened gas turbine combustor supply

SEAL PART

Gas turbine combustor exit duct and hp vane interface

Seals for a turbine engine, and methods of assembling a turbine engine

Combustor-transition-piece guide jig and method of detaching and attaching combustor of gas turbine

Cooling structure for gas turbine transition duct

Turbine stator nozzle cooling structure

GAS TURBINE

Combustor-turbine seal interface for gas turbine engine

Expansion hula seals

System and method for cooling a wall of a gas turbine combustor

Gas turbine: seal between adjacent can annular combustors

Feeding film cooling holes from seal slots

Sealing segment and sealing-segment arrangement

Thermally decoupled can-annular transition piece

Gas turbine combustor exit duct and HP vane interface

Method and apparatus for gas turbine engine temperature management

Methods and apparatus for robotically inspecting gas turbine combustion components

METHODS AND APPARATUS INVOLVING COOLING FINS

Seal structure for gas turbine combustor

Transition duct assemblies and gas turbine engine systems involving such assemblies

TURBULATED AFT-END LINER ASSEMBLY AND RELATED COOLING METHOD

Gas turbine having a combustion oscillation suppressing device

Structural attachment system for transition duct outlet

Cooling of turbine components using combustor shell air

Method and apparatus for cooling a transition piece

Method and apparatus to enhance transition duct cooling in a gas turbine engine

COOLING APPARATUS FOR COMBUSTOR TRANSITION PIECE

Forward sleeve retainer plate and method

Gas turbine engine

High temperature-resistant sealing assembly, especially for gas turbines

Platform cooling of turbine vane

Maintenance method of a gas turbine unit and gas turbine unit

Methods, apparatus and systems concerning the circumferential clocking of turbine airfoils in relation to combustor cans and the flow of cooling air through the turbine hot gas flowpath

Integrated combustor and stage 1 nozzle in a gas turbine and method

Heat shield sealing for gas turbine engine combustor

Modular transvane assembly

Gas turbine transition duct

Combustor assembly comprising a combustor device, a transition duct and a flow conditioner

Turbine transition duct apparatus

Axial diffusor for a turbine engine

Gas turbine transition duct apparatus

Device for attaching a combustion chamber

Flow device for turbine engine and method of assembling same

Separation-resistant inlet duct for mid-turbine frames

Jig

Contoured Impingement Sleeve Holes

Canted outlet for transition in a gas turbine engine

Transition with a linear flow path for use in a gas turbine engine

Transition with a linear flow path with exhaust mouths for use in a gas turbine engine

Transition duct aft end frame cooling and related method

Gas turbine transition piece having dilution holes

Method of refurbishing a seal land on a turbomachine transition piece and a refurbished transition piece

Gas turbine transition duct coupling apparatus

COMBUSTOR STRUCTURE

Combustion liner for a gas turbine engine including heat transfer columns to increase cooling of a hula seal at the transition duct region

Exhaust system

Combustor transition piece aft end cooling and related method

Impingement cooling device

Aft frame with oval-shaped cooling slots and related method

Transition piece mounting bracket and related method

High-temperature member for use in gas turbine

Optimizing the angular positioning of a turbine nozzle at the outlet from a turbomachine combustion chamber

Apparatus comprising a CMC-comprising body and compliant porous element preloaded within an outer metal shell

Combustor seal having multiple cooling fluid pathways

GAS TURBINE

Cooling apparatus for combustor transition piece

TRANSITION PIECE IMPINGEMENT SLEEVE AND METHOD OF ASSEMBLY

Replaceable orifice for combustion tuning and related method

Insulator bushing for combustion liner

High temperature seal for a turbine engine

Transition scrolls for use in turbine engine assemblies

Altering a natural frequency of a gas turbine transition duct

Combustor end cap assembly

COMBUSTOR SPRING CLIP SEAL SYSTEM

TURBINE NOZZLE SEGMENT AND ASSEMBLY

Gas turbine with a gap blocking device

Transition duct assembly

Transition duct cooling feed tubes

AIR COOLED GAS TURBINE COMPONENTS AND METHODS OF MANUFACTURING AND REPAIRING THE SAME

Airflow distribution to a low emissions combustor

Systems and methods for cooling gas turbine engine transition liners

Internal manifold air extraction system for IGCC combustor and method

INLET FILM COOLING OF TURBINE END WALL OF A GAS TURBINE ENGINE

Gas turbine engine systems involving cooling of combustion section liners

Turbulated aft-end liner assembly and cooling method

Stage one nozzle to transition piece seal

Apparatus and method for controlling the secondary injection of fuel

Seal structure for gas turbine combustor

Turbomachine, especially gas turbine

Wavy CMC wall hybrid ceramic apparatus

Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon

Sealing apparatus and gas turbine having same

Brazed joint between a metal part and a ceramic part

Joint between a metal part and a ceramic part based SiC and/or C

Turbine component

Method and apparatus to facilitate cooling turbine engines

Impingement jets coupled to cooling channels for transition cooling

Transition-to-turbine seal apparatus and transition-to-turbine seal junction of a gas turbine engine

Hot gas duct and duct splitter arrangement

Repaired vane assemblies and methods of repairing vane assemblies

Transition support system for combustion transition ducts for turbine engines

Low leakage spring clip/ring combinations for gas turbine engine

Turbine component with repaired seal land and related method

Airfoil, sleeve, and method for assembling a combustor assembly

DETONATION COMBUSTOR TO TURBINE TRANSITION PIECE FOR HYBRID ENGINE

Transition duct for a gas turbine engine

Method and apparatus for reducing stresses induced to combustor assemblies

Transition duct for gas turbine engine

Seal system for an interturbine duct within a gas turbine engine

Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine

Gas turbine combustor

Door seal for a turbomachine

Seal part

Fluid flow distributor apparatus for gas turbine engine mid-frame section

Combustor spring clip seal system

Convex sealing bottom for a twin-shaft turbine

Forward sleeve retainer plate and method

Methods and system for reducing pressure losses in gas turbine engines

Gas turbine transition duct

Wireless terminal location using apparatus and methods employing carrier diversity

HPT aerodynamic trip to improve acoustic transmission loss and reduce noise level for auxiliary power unit

Axial diffusor for a turbine engine

Methods and apparatus for assembling gas turbine engines

Gas turbine engine transitions comprising closed cooled transition cooling channels

Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions

Combustor turbine interface

METHODS AND APPARATUS FOR ASSEMBLING TURBINE ENGINES

Methods and apparatus for assembling turbine engines

Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine

Transition piece for gas turbine

Gas turbine engine with purge air pump and guide

Combustion transition duct providing stage 1 tangential turning for turbine engines

GAS TURBINE INTERMEDIATE STRUCTURE AND A GAS TURBINE ENGINE COMPRISING THE INTERMEDIATE STRUCTURE

Support system for transition ducts

On-line system and method for processing information relating to the wear of turbine components

Turbine, fixing device for blades and working method for dismantling the blades of a turbine

Gas turbine combustor barrier structures for spring clips

Method of manufacturing a duct for a gas turbine engine

Cooled transition duct for a gas turbine engine

Cooling system for a transition bracket of a transition in a turbine engine

Cooled gas turbine transition duct

Seal usable between a transition and a turbine vane assembly in a turbine engine

Integrated turbine vane support

Wireless terminal location using apparatus and methods employing carrier diversity

Platform cooling arrangement for the nozzle guide vane stator of a gas turbine

Coupled parametric design of flow control and duct shape

Duct with integrated baffle

Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle

Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine

Inlet film cooling of turbine end wall of a gas turbine engine

Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine

Multi-zone tubing assembly for a transition piece of a gas turbine

Combustion liner having improved cooling and sealing

Combustion liner seal with heat transfer augmentation

Gas turbine engine transition liner assembly and repair

System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor

Transition duct apparatus having reduced pressure loss

Apparatus and method for reducing the heat rate of a gas turbine powerplant

Cooling structure of gas turbine tail pipe

Manufacturing method for frame body and frame body

Method of refurbishing a transition duct for a gas turbine system

Turbine combustor transition piece having dilution holes

Sealing arrangement

Cooling and sealing design for a gas turbine combustion system

Forming gas turbine transition duct bodies without longitudinal welds

Gas turbine combustor sliding joint

Combustion chamber intermediate part for a gas turbine

Seal element for sealing a gap and combustion turbine having a seal element

Transition duct honeycomb seal

Transition duct cooling system

Instrumented transition alignment fixture and method

Repair of combustion turbine components

Exit stator mounting

Transition duct support bracket wear cover

Combustor with additively manufactured combustor body having aft frame with heat transfer augmentation

Additively manufactured combustor liner v-band cooling ring

Additively manufactured combustor with adaptive cooling passage

Gas turbine engine with combustor section mounted modulated compressor air cooling system

Magnetic aft frame side seals

Magnetic sealing arrangement for a turbomachine

Transition duct system with straight ceramic liner for delivering hot-temperature gases in a combustion turbine engine

Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines