INVESTIGATION OF AN INDEPENDENT COOLING SYSTEM FOR A GAS TURBINE,
Abstract
The necessity for experimental study on an autonomous cooling system for gas turbine rotor blades is examined. The design and technological peculiarities of a test facility for investigating a high-temperature turbine with an independent cooling system are described, and investigation problems are presented. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 22, 1969
- Accession Number
- AD0693852
Entities
People
- E. A. Manushin
- G. A. Pugin
Organizations
- National Air and Space Intelligence Center