Accession Number : AD0164658
Title : Turbine Pressure Attenuation Plenum Chambers.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Tetrault,Joseph A.
Report Date : 12 FEB 1974
Pagination or Media Count : 3
Abstract : The patent relates to a turbine having a plurality of pressure attenuation plenum chambers. These chambers are located adjacent the vanes of a turbine thereby relieving the excess pressure by distributing it through a series of apertures in the plenum chamber walls.
Descriptors : *Gas turbines, *Chambers, *Patents, Distribution, Pressure
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE