The technique of controlling engine acceleration has made possible gas turbine controls with simple hydromechanics and a minimal number of inputs into the electronics. This paper describes a control and electrical power generation system developed for an unmanned aircraft gas turbine, and the results obtained from the development engine running carried out with it.

Issue Section:
Research Papers
Topics:
Control systems, Fuels, Gas turbines, Engines, Aircraft, Electric power generation, Electronics, Fluid mechanics
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Copyright © 1988
 by ASME
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