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.
A Simplified Fuel Control Approach for Low-Cost Aircraft Gas Turbines
Sae Technical Papers
National Air Transportation Meeting ; 1973
01.02.1973
Aufsatz (Konferenz)
Englisch
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