NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A New Method to Measure Temperature and Burner Pattern Factor Sensing for Active Engine ControlThe determination of the temperatures of extended surfaces which exhibit non-uniform temperature variation is very important for a number of applications including the "Burner Pattern Factor" (BPF) of turbine engines. Exploratory work has shown that use of BPF to control engine functions can result in many benefits, among them reduction in engine weight, reduction in operating cost, increase in engine life, while attaining maximum engine efficiency. Advanced engines are expected to operate at very high temperature to achieve high efficiency. Brief exposure of engine components to higher than design temperatures due to non-uniformity in engine burner pattern can reduce engine life. The engine BPF is a measure of engine temperature uniformity. Attainment of maximum temperature uniformity and high temperatures is key to maximum efficiency and long life. A new approach to determine through the measurement of just one radiation spectrum by a multiwavelength pyrometer is possible. This paper discusses a new temperature sensing approach and its application to determine the BPF.
Document ID
19990052760
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ng, Daniel
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1999
Subject Category
Instrumentation And Photography
Report/Patent Number
E-11675
NAS 1.15:209090
NASA/TM-1999-209090
Report Number: E-11675
Report Number: NAS 1.15:209090
Report Number: NASA/TM-1999-209090
Funding Number(s)
PROJECT: RTOP 274-00-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available