Accession Number:

AD0655350

Title:

GAS TURBINE EJECTOR,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1967-02-27

Pagination or Media Count:

7.0

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.

Subject Categories:

  • Air Conditioning, Heating, Lighting and Ventilating
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE