Cooling arrangement

The present invention relates to cooling arrangements for use within gas turbine engines. Cooling air enters a cooling path from a supply at The path follows a serpentine path consecutively through a number of components to be cooled, including guide vanes blades a shroud and a shaft A valve is prov...

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1. Verfasser:	Dailey, Geoffrey M
Format:	Patent
Sprache:	eng
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creator	Dailey, Geoffrey M
description	The present invention relates to cooling arrangements for use within gas turbine engines. Cooling air enters a cooling path from a supply at The path follows a serpentine path consecutively through a number of components to be cooled, including guide vanes blades a shroud and a shaft A valve is provided at the downstream end of the path The setting of the valve modulates the flow and pressure of air along the path without wholly preventing it.
format	Patent
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title	Cooling arrangement
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