Accession Number : AD0673924

Title :   TEMPERATURE ERRORS IN MEASURING THE DIAMETER OF THE ROTOR OF A COMPRESSOR AND A GAS TURBINE ENGINE (TEMPERATURNYE POGRESHNOSTI IZMERENIYA DIAMETRA KOLES ROTORA KOMPRESSORA I TURBINY GTD),

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Velikovskii,I. E.

Report Date : 17 NOV 1967

Pagination or Media Count : 10

Abstract : The error caused by thermal expansion of rotor wheels in gas turbines during length measurements is investigated. To account for the differential expansion of the various blade and wheel elements of the rotor, a compound expansion coefficient is derived. It is shown that to minimize thermal expansion errors the measuring instrument and the turbine rotor must reach thermal equilibrium and that a composite measuring scale with an effective expansion coefficient equal to alpha pr of the rotor should be used. Curves are given showing error versus rotor length for different delta alpha's between the rotor and the measuring scale. (Author)

Descriptors :   (*GAS TURBINES, USSR), TEMPERATURE, DISTRIBUTION, GAS TURBINE ROTORS, COMPRESSOR ROTORS, THERMAL EXPANSION, AXIAL FLOW COMPRESSOR BLADES, MEASUREMENT, ERRORS, MATHEMATICAL ANALYSIS

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE