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Failure Survival Aspects of a Digital Fuel Control System
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English
Abstract
The paper concerns the design of an engine mounted, electronic, digital fuel control system for a twin coupled, helicopter engine configuration. The system is described from the point of view of the failure survival requirements, and the paper highlights the contribution of the digital system to the implementation of these requirements, and the environmental design techniques adopted to achieve maximum reliability.
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Citation
Bussell, J., "Failure Survival Aspects of a Digital Fuel Control System," SAE Technical Paper 751062, 1975, https://doi.org/10.4271/751062.Also In
References
- Simonis Edward A. Perks Malcolm P. “Helicopter Engine Control - The Past 20 Years and the Next” Paper 14 presented at AGARD Conference on Power Plant Controls for AeroGas Turbine Engines Ustaoset, Norway September 1974