TEMPERATURE FIELD OF A TURBINE ROTOR COOLED BY VAPOR PASSING THROUGH CIRCULAR CHANNELS IN THE BLADE SHAFTS

Abstract

The paper presents the results of investigations of the stationary and nonstationary temperature fields in a cooled rotor of a steam turbine. The derived data can be used in creating and constructing powerful promising turbogenerator sets for supercritical steam parameters.

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Document Details

Document Type
Technical Report
Publication Date
May 03, 1967
Accession Number
AD0660443

Entities

People

  • D. A. Pereverzev
  • L. V. Povolotskii
  • N. B. Chirkin

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Coefficients
  • Computations
  • Cooling
  • Efficiency
  • Equations
  • Experimental Data
  • Foreign Technology
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Steam Turbines
  • Thermal Conductivity
  • Translations
  • Turbine Blades
  • Turbines
  • Turbogenerators

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerodynamics.
  • Electrical Engineering