GAS TURBINE EJECTOR,
Abstract
The article discusses a gas turbine ejector for drawing off vapors of a refrigerant in systems of conditioning flying apparatuses which consists of an expansion nozzle and a diffusor. For the purpose of reducing size and weight, the mixing chamber and diffusor are designed in the form of ring-type slits profiled along the radius while the plane of symmetry of the expanding slit-type nozzle, which consists of two parts, is placed together with the plane of symmetry of the mixing chamber designed from two profiled plates.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 27, 1967
- Accession Number
- AD0655350
Entities
People
- A. N. Yakushen
- L. Ya. Klimov
- P. A. Kogan
- Yu. A. Yushkin
Organizations
- National Air and Space Intelligence Center