Method of Testing Regulators which Control Temperature of Gases and Nozzle of Turbojet Engines,
Abstract
The proposed invention is in the field of study and refinement of regulators for gas turbine engines on Electrical model stands. The known methods of testing regulators have not enabled one to test and refine the aggregates of the system which regulates gas turbine engines which have a controllable jet nozzle.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 03, 1975
- Accession Number
- ADA006839
Entities
People
- A. A. Artemev
- A. N. Dobrynin
Organizations
- National Air and Space Intelligence Center