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