Accession Number:

AD0649339

Title:

TURBINE BLADE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Lubny-Gertsyk,A. L.
• Shvartsshtein,E. M.

Report Date:

1967-01-23

Pagination or Media Count:

6.0

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