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A Simplified Fuel Control Approach for Low-Cost Aircraft Gas Turbines
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English
Abstract
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.
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Citation
Gold, H., "A Simplified Fuel Control Approach for Low-Cost Aircraft Gas Turbines," SAE Technical Paper 730388, 1973, https://doi.org/10.4271/730388.Also In
References
- Seldner K. Gold H. “Computer and Engine Performance Study of a Generalized Parameter Fuel Control for Jet Engines.” NASA TN D-5871 June 1970
- Batterton P. G. Gold H. “Experimental Test Results of a Generalized-Parameter Fuel Control.” NASA TN D-7198 March 1973
- Seldner K. Geyser L. C. Gold H. Walker D. Burgner G. “Performance and Control Study of a Low-Pressure-Ratio Turbojet Engine for a Drone Aircraft.” NASA TM X-2537 April 1972