Accession Number : AD0164727

Title :   Impingement Cooled Turbine Blade.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Ernst,H. H.

Report Date : 22 FEB 1973

Pagination or Media Count : 9

Abstract : The patent application relates to an impingement cooled turbine blade to be used with a hollow turbine shaft, using a female dovetail and having an easily removable insert for guiding and directing the cooling fluid through the hollow blade.

Descriptors :   *Turbine blades, *Cooling, Patents, Impingement, Inserts, Gas turbines

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE