Radiation Pyrometer for Gas Turbine Blades

720159

02/01/1972

Event
1972 Automotive Engineering Congress and Exposition
Authors Abstract
Content
Advances in the development of radiation pyrometry for measuring the blade temperature in gas-turbine engines are reported. In this system, engine-mounted sensor heads collect thermal radiation from either a spot or a reasonably large area of the turbine blade. High-temperature fiber optics transmit the radiation to a remote detector housing where the photons are converted into an electrical signal by a silicon photovoltaic cell. A signal processor measures and displays on a real-time basis three temperature characteristics of the turbine blades with response better than 10 ms in most cases. Recent developments include smaller electronics, practical sensor heads, and 5000 h fiber optics. Importance of measuring the blade temperature, potential uses of the data, and actual engine tests are described.
Meta TagsDetails
DOI
https://doi.org/10.4271/720159
Pages
14
Citation
Rohy, D., Duffy, T., and Compton, W., "Radiation Pyrometer for Gas Turbine Blades," SAE Technical Paper 720159, 1972, https://doi.org/10.4271/720159.
Additional Details
Publisher
Published
Feb 1, 1972
Product Code
720159
Content Type
Technical Paper
Language
English