This paper examines some of the background that has led to the requirements for a lightweight universal fuel control for aircraft gas turbine engines. One design solution for this type of fuel control is reviewed with regard to function, adaptability, maintenance, and cost.
A Lightweight Universal Fuel Control for Aircraft Turbine Engines
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
1964-01-01
Conference paper
English
Lightweight universal fuel control for aircraft turbine engines
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