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EP2620618A3 - Gas turbine engine in-board cooled cooling air

A system for supplying turbine cooling air flow includes a turbofan engine, a heat exchanger, and a door. The turbofan engine includes an engine case

US7870738B2 - Gas turbine: seal between adjacent can annular

The present invention is directed to a seal for sealing a gap between transition sections of adjacent can annular combustors in a turbine engine such

GAS TURBINE ENGINE WITH AN ENGINE ROTOR ELEMENT TURNING

heat source on the turbine engine and in high temperatures to maximize engine efficiency, so hoses, valves and other fittings configured to

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Alvin L. Tanners research works | Fluor, Texas and other

high temperature gas cooled nuclear reactor (HTGR), solar energy or (SOFC) whose waste heat serves as heat source for the HAT turbine [29,

METHOD FOR HEAT TREATING BY INDUCTION AN ALLOY COMPONENT FOR

heat level above a precipitate solvus temperature within the alloy component A turbine stage of an aeronautic turbomachine operates in a very high

high intensity meso-scale combustor for mini gas turbine

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US9353946B2 - Gradual oxidation with heat transfer - Google

Gradual oxidation with heat transfer Download PDF InfoPublication numberUS9353946B2US9353946B2 US13/417,140 US201213417140A US9353946B2 US 9353946 B2 US

channels--《Gas Turbine Experiment and Research》201801

To investigate the heat transfer and flow characteristics in constant and converging channels,numerical simulation of the high solidity pin-fin

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US6644062B1 - Transcritical turbine and method of operation -

A process employing a rotary axial turbine, and a nozzle, that includes providing a working fluid expansible from a characteristic supercritical region into

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Liquid Metal coolants for high power heat transport systems P. Hosemann, Contribution from: David Frazer; Cristian Cionea; Stephen Parker; C. Rose

Alvin L. Tanners research works | Fluor, Texas and other

high temperature gas cooled nuclear reactor (HTGR), solar energy or (SOFC) whose waste heat serves as heat source for the HAT turbine [29,

LOW-GRADE HEAT OPTIMIZATION OF RECUPERATIVE SUPERCRITICAL CO2

turbine exhaust stream in order to increase the available quantity of heat heated, high pressure recycled CO2 can be further heated with a solar

-Parker - Parker

The invention provides a device for generating high pressure air. The device comprises a block having an external surface and an internal surface, said

CA2248736C - Internally heatshielded nozzle - Google Patents

Internally heatshielded nozzle Download PDF InfoPublication number CA2248736C High temperature gas turbine compressor discharge air flows around the housi

Gas Turbine Fire and Overheat Detection and Extinguishing

TURBINE ENGINESFire/Overheat Detection and Extinguishing Systems Define the meaning of the following terms associated with engine fi TURBINE ENGINESTURB

HUMID AIR TURBINE POWER, WATER EXTRACTION, AND REFRIGERATION

Various embodiments relate to combined heat and power (CHP) systems. A CHP system can include a turbine system, a turbocharger system, and a 1

Gas Turbine Blade Leading Edge | Volume 5B: Heat Transfer

leading to the high Nusselt number region downstream deflection towards on Heat Transfer in Steam Cooling of Gas Turbine Blade Internal Ribbed

Heat Resistance Evaluation System for TBC on Gas Turbine

However, it is reported that under high-temperature operating conditions, theNon-Destructive Heat Resistance Evaluation System for TBC on Gas Turbine

channels--《Gas Turbine Experiment and Research》201801

To investigate the heat transfer and flow characteristics in constant and converging channels,numerical simulation of the high solidity pin-fin

a Sloping Sheet for Gas Turbine Blade | Volume 5A: Heat

of gas turbine blades, inspired by the concept of aircraft wing tip vortexmaterial and the heat transfer of the external high temperature flow field

High Temperature Textiles | Thermal Velocity | Heat Resistant

Textile Technologies Europe Ltd manufactures and distributes a vast range of high temperature extreme heat resistant industrial textiles for use in a large

US4574584A - Method of operation for a gas turbine engine -

A cooling system 46 for a turbofan gas turbine engine 10 is disclosed. Various construction details which increase the effectiveness of a heat exchanger

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Gas Turbine Blade Leading Edge | Volume 5B: Heat Transfer

leading to the high Nusselt number region downstream deflection towards on Heat Transfer in Steam Cooling of Gas Turbine Blade Internal Ribbed