FILM COOLING HOLE IN GAS TURBINE COMPONENTS

FILM COOLING HOLE IN GAS TURBINE COMPONENTS

A film-cooling hole of gas turbine components to be cooled has an inflow section which has a constant throughflow cross section and which is adjoined by a diffuser section which has a varying throughflow cross section. The widening of the diffuser region occurs only in the direction which is perpend...

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Hauptverfasser: BECK, Thomas, DAHLKE, Stefan, HOHENSTEIN, Sebastian, DIETRICH, Jens
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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
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creator BECK, Thomas
DAHLKE, Stefan
HOHENSTEIN, Sebastian
DIETRICH, Jens
description A film-cooling hole of gas turbine components to be cooled has an inflow section which has a constant throughflow cross section and which is adjoined by a diffuser section which has a varying throughflow cross section. The widening of the diffuser region occurs only in the direction which is perpendicular to the flow direction of the relatively hot medium.
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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 FILM COOLING HOLE IN GAS TURBINE COMPONENTS
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