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),
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 17, 1967
- Accession Number
- AD0673924
Entities
People
- I. E. Velikovskii
Organizations
- National Air and Space Intelligence Center