Impingement Cooled Turbine Blade.

Abstract

The patent application relates to an impingement cooled turbine blade to be used with a hollow turbine shaft, using a female dovetail and having an easily removable insert for guiding and directing the cooling fluid through the hollow blade.

Document Details

Document Type
Technical Report
Publication Date
Feb 22, 1973
Accession Number
AD0164727

Entities

People

  • H. H. Ernst

Organizations

  • United States Department of the Air Force

Tags

DTIC Thesaurus Topics

  • Patent Applications
  • Patents
  • Rotor Blades (Turbomachinery)
  • Turbine Blades
  • Turbines
  • Turbomachinery

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design