High-Temperature Sensors for Army Gas Turbine Engines
Abstract
The turbine blade temperature measuring system views the rotating turbine blades of a gas turbine engine, and by measuring the emitted, infrared radiation, it produces a processed signal directly proportional to the temperature of the blades.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1974
- Accession Number
- ADA005166
Entities
People
- B. G. Buehler
- D. A. Rohy
- W. A. Compton