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A simplified fuel control approach for low cost aircraft gas turbines.Cost reduction in aircraft turbine engines may be obtained through performance reductions that are acceptable for ranges that are considerably shorter than the range for which current and costly engines were developed. Cost reduction in the fuel control for these cost engines must be achieved without significant performance reduction. This paper describes a fuel control approach that appears to meet this requirement and reviews the work that has been performed on it over the past few years.
Document ID
19730049923
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gold, H.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1973
Subject Category
Propulsion Systems
Meeting Information
Meeting: National Air Transportation Meeting
Location: Miami, FL
Start Date: April 24, 1973
End Date: April 26, 1973
Sponsors: Society of Automotive Engineers
Accession Number
73A34725
Distribution Limits
Public
Copyright
Other

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