Share Email Print
cover

Proceedings Paper

Optical Systems For Gas Turbine Engines
Author(s): Mark Wrigley
Format Member Price Non-Member Price
PDF $14.40 $18.00
cover GOOD NEWS! Your organization subscribes to the SPIE Digital Library. You may be able to download this paper for free. Check Access

Paper Abstract

The use of optical systems for data acquisition and transmission is becoming increasingly popular for aviation applications. Features such as weight and immunity to high levels of E.M.C. are distinct advantages over conventional electronic systems. In some cases optical transducers provide a means of measurememt which would otherwise be impossible. One such transducer is the Turbine Blade Pyrometer Transducer. This instrument determines gas turbine blade temperature by measuring emitted visible and near infrared radiation. The transducer is an engine mounted electro optical system which provides a voltage output proportional to turbine blade radiance. As such it must be designed to withstand the demanding environment of a gas turbine engine.

Paper Details

Date Published: 20 October 1986
PDF: 7 pages
Proc. SPIE 0656, Contemporary Optical Instrument Design, Fabrication, and Testing, (20 October 1986); doi: 10.1117/12.938481
Show Author Affiliations
Mark Wrigley, Negretti Aviation (United Kingdom)


Published in SPIE Proceedings Vol. 0656:
Contemporary Optical Instrument Design, Fabrication, and Testing
Leo H. J. F. Beckmann; J. David Briers; Paul R. Yoder, Editor(s)

© SPIE. Terms of Use
Back to Top