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