TURBOCOOLER,
Abstract
The object of the invention is a turbocooler for systems of conditioning air in hermetically sealed sections of flying apparatuses which contains operating wheels of a turbine and a blower turning on gas bearings. An immovable axis is designed as a hollow with a supporting disk in the middle part, serving together with the face surfaces of the wheels of the turbine and the blower as a supporting bearing, to which gas is conducted from input piping of the turbine through a hollow axis. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 16, 1966
- Accession Number
- AD0644639
Entities
People
- G. I. Voronin
- V. I. Slotin
Organizations
- National Air and Space Intelligence Center