Gas turbine engine with outer case ambient external cooling system

A thermal barrier/cooling system for controlling a temperature of an outer case of a gas turbine engine. The thermal barrier/cooling system includes an internal insulating layer supported on an inner case surface, the internal insulating layer extending circumferentially along the inner case surface...

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Hauptverfasser: MUNSHI MRINAL, SHTEYMAN YEVGENIY, GRABER DARYL, LEE CHING-PANG, PORTER MATTHEW R, FINNERAN JOHN, LEAGON JONATHAN M
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creator MUNSHI MRINAL
SHTEYMAN YEVGENIY
GRABER DARYL
LEE CHING-PANG
PORTER MATTHEW R
FINNERAN JOHN
LEAGON JONATHAN M
description A thermal barrier/cooling system for controlling a temperature of an outer case of a gas turbine engine. The thermal barrier/cooling system includes an internal insulating layer supported on an inner case surface, the internal insulating layer extending circumferentially along the inner case surface and providing a thermal resistance to radiated energy from structure located radially inwardly from the outer case. The thermal barrier/cooling system further includes a convective cooling channel defined by a panel structure located in radially spaced relation to an outer case surface of the outer case and extending around the circumference of the outer case surface. The convective cooling channel forms a flow path for an ambient air flow cooling the outer case surface.
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subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title Gas turbine engine with outer case ambient external cooling system
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