An Infrared Technique for Measuring Cycle-Resolved Transient Combustion-Chamber Surface Temperatures in a Fired Engine

860240

03/01/1986

Event
SAE International Congress and Exposition
Authors Abstract
Content
An optical technique for measuring transient combustion chamber surface temperatures in a fired engine has been developed. The spectral region from 3.6 to 4.0 microns was found to be suitable for making optical measurements through the methane-air flame. The experimental apparatus was capable of making simultaneous time-resolved measurements of infrared gas absorption, gas emission and surface radiation during a single engine cycle.
The effects of engine operating conditions on gas absorption and gas emission were investigated. Measurements of “simulated” deposits at temperatures ranging from 569 K to 944 K indicated that the technique was accurate within 7 K at the higher temperatures.
Meta TagsDetails
DOI
https://doi.org/10.4271/860240
Pages
12
Citation
Bethel, S., and Anderson, C., "An Infrared Technique for Measuring Cycle-Resolved Transient Combustion-Chamber Surface Temperatures in a Fired Engine," SAE Technical Paper 860240, 1986, https://doi.org/10.4271/860240.
Additional Details
Publisher
Published
Mar 1, 1986
Product Code
860240
Content Type
Technical Paper
Language
English