NOZZLE ASSEMBLY FOR A SMALL GAS TURBINE,

Abstract

An Author Certificate has been issued for a nozzle assembly for a small gas turbine with nozzles having an annular cross section whose leading or trailing edges are intersected by the corresponding edges of the preceding nozzle. To secure a uniform supply of the working fluid to the inlet section of the rotor blades, the nozzles are arranged in two or several rows. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 29, 1969
Accession Number
AD0694811

Entities

People

  • I. F. Vainbaum
  • L. S. Arinushkin
  • O. N. Emin
  • V. I. Dumov
  • Yu. N. Mikhailov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Assembly
  • Gas Turbines
  • Trailing Edges
  • Turbines

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Fluid Mechanics and Fluid Dynamics.
  • Internal Combustion Engine (ICE) Technology.