Accession Number : AD0649339

Title :   TURBINE BLADE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Lubny-Gertsyk,A. L. ; Shvartsshtein,E. M.

Report Date : 23 JAN 1967

Pagination or Media Count : 6

Abstract : A turbine blade with external 'fluid-droplet' cooling is described. To improve its reliability, the blade is coated with a high-thermal-conductivity material, such as copper.

Descriptors :   (*GAS TURBINE BLADES, *COPPER COATINGS), HEAT RESISTANT ALLOYS, HEAT RESISTANT METALS, COOLING, THERMAL CONDUCTIVITY, USSR, PATENTS

Subject Categories : Coatings, Colorants and Finishes
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE