Accession Number : AD0686236

Title :   THE MEASUREMENT OF THE INITIAL GAS TEMPERATURE IN GT (GAS TURBINE) BASED ON INDIRECT PARAMETERS,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kantor,S. A. ; Arsenev,L. V.

Report Date : 26 DEC 1968

Pagination or Media Count : 15

Abstract : The results of an investigation regarding the possible measurement of the initial gas temperature in a gas turbine through indirect parameters such as the final temperature of the gas after the turbine and the degree of expansion, are presented. The theoretical concepts supporting the application of this method and the corresponding technical approaches are included. (Author)

Descriptors :   (*GAS TURBINES, *TEMPERATURE CONTROL), TEMPERATURE, AUTOMATIC, PRESSURE, VELOCITY, GAS FLOW, EFFICIENCY, EXPERIMENTAL DESIGN, MEASUREMENT, HYDRAULIC EQUIPMENT, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE