Insert element for closing an opening inside a wall of a hot gas path component of a gas turbine and method for enhancing operational behaviour of a gas turbine

Tile fastening arrangement of a gas-turbine combustion chamber

Push-lock pin

Method of casting parts using heat reservoir, gating used by such method, and casting made thereby

Gas-turbine combustion chamber with mixing air orifices and chutes in modular design

Combustor liner with reduced cooling dilution openings

Combustor having a beveled grommet

SYSTEM OF INTEGRATING BAFFLES FOR ENHANCED COOLING OF CMC LINERS

Combustion system and method of assembling the same

Pin fin arrangement for heat shield of gas turbine engine

Gas-turbine combustion chamber with a holding mechanism for a seal for an attachment

Two stage serial impingement cooling for isogrid structures

SYSTEM AND METHOD FOR PROTECTION OF HIGH TEMPERATURE MACHINERY COMPONENTS

Insert adjacent to a heat shield element for a gas turbine engine combustor

SYSTEM AND METHOD FOR ADAPTIVE IMPINGEMENT COOLING

Reverse flow combustor duct attachment

Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key

CELL STRUCTURE THERMAL BARRIER COATING

Heat Shield Element, Method and Mold for the Production Thereof, Hot-Gas Lining and Combustion Chamber

Ceramic combustor liner panel for a gas turbine engine

Method for manufacturing a ceramic composite article

Combustion liner with open cell foam and acoustic damping layers

CMC anchor for attaching a ceramic thermal barrier to metal

Ceramic combustor liner panel for a gas turbine engine

Gas turbine combustion chamber made of CMC material and subdivided into sectors

Transitional region for a combustion chamber of a gas turbine

System, method and apparatus for lean combustion with plasma from an electrical arc

Gas turbine engine combustor with CMC heat shield and methods therefor

Material mixture for producing a fireproof material, fireproof molded body and method for the manufacturing thereof

Tangential combustor with vaneless turbine for use on gas turbine engines

Various layered gas turbine engine component constructions

Coating Systems for Protection of Substrates Exposed to Hot and Harsh Environments and Coated Articles

Methods for Coating Articles Exposed to Hot and Harsh Environments

COMPONENT IN A COMBUSTION SYSTEM, AND PROCESS FOR PREVENTING SLAG, ASH, AND CHAR BUILDUP

Coating process and corrosion protection coating for turbine components

ARTICLE FOR HIGH TEMPERATURE SERVICE

Combustor tile mounting arrangement

COATING STRUCTURE AND SURFACE PROCESSING METHOD

Heat shield element arrangement and method for installing a heat shield element

COOLED HYBRID STRUCTURE FOR GAS TURBINE ENGINE AND METHOD FOR THE FABRICATION THEREOF

Machine component and gas turbine

Damage tolerant gas turbine component

Reverse flow ceramic matrix composite combustor

COMBUSTION CHAMBER BRAZED WITH CERAMIC INSERTS

Instrumented component for use in an operating environment

Heat shield element, method and mold for the production thereof, hot-gas lining and combustion chamber

Device and method for extending the service life of firing installations

Heat shield element, in particular for lining a combustion chamber wall

Hybrid turbomachinery component for a gas turbine engine

Paneled combustion liner having nodes

Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained

Compliant metal support for ceramic combustor liner in a gas turbine engine

Ceramic matrix composite structure

Method of manufacturing a thermal insulation article

Composite material part with a silicon-containing ceramic matrix protected against corrosion

Ceramic matrix composite turbine engine component

Gas turbine combustion chamber having inner and outer walls subdivided into sectors

Component in a combustion system, and process for preventing slag, ash, and char buildup

Cooling arrangement for CMC components with thermally conductive layer

Gas-turbine combustion chamber with ceramic flame tube

System, method and apparatus for lean combustion with plasma from an electrical arc

Combustion chamber wall

Matrix and Layer System

Combustion apparatus

Combustion chamber lining

Ceramic component with surface resistant to hot gas and method for the production thereof

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

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

Retaining element and heat shield element for a heat shield and combustion chamber provided with a heat shield

Floatwell panel assemblies and related systems

Brazed joint between a metal part and a ceramic part

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

Gas-turbine combustion chamber wall

Layer system with blocking layer, and production process

Thermal barrier coating for combustor panels

Environmental barrier coating for silicon-containing substrates and process therefor

Methods and apparatus for radially compliant component mounting

Attachment of a ceramic combustor can

Heat shield element, method and mold for the production thereof, hot-gas lining and combustion chamber

High-temperature layered system for dissipating heat and method for producing said system

Bolting configuration for joining ceramic combustor liner to metal mounting attachments

Annular combustion chamber of a turbomachine

Annular combustion chamber of a turbomachine

Environmental barrier coating for silicon-containing substrates and process therefor

Heat shield

Dual wall combustor liner

Gas turbine combustion chamber

Assembling an annular combustion chamber of a turbomachine

Fastening a combustion chamber inside its casing

Nickel based superalloy

Refractory component with ceramic matrix composite skeleton

Thermal shield, especially for lining the wall of a combustion chamber

Heat shield block for lining a combustion chamber wall, combustion chamber and gas turbine

Compliant metal support for ceramic combustor liner in a gas turbine engine

Ceramic tile insulation for gas turbine component

Method of making a ceramic matrix composite utilizing partially stabilized fibers

DIFFUSION BARRIER FOR ASSEMBLIES WITH METALLIC AND SILICON-CONTAINING COMPONENTS AND METHOD THEREFOR

Heat shield

Multilayered environmental barrier coating and related articles and methods

Process for in situ coating of turbo-machine components

Component, method for coating a component, and powder

Attachment system for ceramic combustor liner

Apparatus and method of detecting wear in an abradable coating system

Waffled impingement effusion method

Turbine blade for use in a gas turbine

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

Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members

Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites

SMOOTH OUTER COATING FOR COMBUSTOR COMPONENTS AND COATING METHOD THEREFOR

Environmental barrier coating for silicon-containing substrates and process therefor

Smart component for use in an operating environment

Wear monitoring system with embedded conductors

Velocity barrier layer for environmental barrier coatings

Oxidation barrier coatings for silicon based ceramics

Method of manufacturing an active cooling panel out of thermostructural composite material

Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion

Mounting system for a flame pipe or liner

Thick coated combustor liner

Optical reflector for reducing radiation heat transfer to hot engine parts

Transpiration cooling system

Plug sealing device that is not welded to the chamber wall

Foam wall combustor construction

Combustion chamber having a flexible connection between a chamber end wall and a chamber side wall

Matrix for ceramic-containing materials

Ceramic matrix composite component with corrugated wall

CMC component with cooling cavity

CMC component with cover plate

Dovetail features on panel rails or impingement sheet to hold panels

Combustor including a heat shield for a turbine engine

Combustor liner panels

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

Combustion chamber tile of a gas turbine and method for its manufacture