Accession Number : ADD009476

Title :   Gas Turbine Cycle Providing a High Pressure Efflux.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON DC

Personal Author(s) : Reh,Frank J

Report Date : 14 May 1968

Pagination or Media Count : 3

Abstract : This invention relates to a system for developing propulsive thrust by the reaction of a flow of energized fluid and in particular is concerned with a gas turbine cycle of operation for developing the propulsive thrust.

Descriptors :   *Patents, *Thrust, *Gas turbines, Propulsion systems, Compressors, High pressure compressors, Cycles, Inventions

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE