Cooling Turbine,
Abstract
The cooling turbine containing a turbine and a compressor wheel installed on the ends of a common shaft mounted in antifriction bearings over an oil casing is distinguished by the fact that in order to intensify the bearing cooling the shaft is executed with a helical groove on the surface which is encompassed by a bearing placed on the compressor side and by a blind-end axial bore on the turbine side which connects its outlet pipe with helical groove and with the oil casing pocket by means of radial channels in the shaft. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 24, 1972
- Accession Number
- AD0753976
Entities
People
- G. I. Sokolov
- G. V. Morozov
- I. E. Orlov
- N. M. Fedoseev
- Yu Blokhin I.
Organizations
- National Air and Space Intelligence Center