The dynamics of the joint operation of the heat engine and the generator during the electric starter launch of gas turbine aircraft engines.

Abstract

The dynamic modes of joint operation of the heat engine and the generator are considered, the method of calculating these modes is given, the conditions for reliable operation of the aerodrome electrical unit when launching heavy gas turbine aircraft engines (AI-20) are defined. The results obtained allowed to synthesize the automatic control system of the new airfield unit APA-4. Figures 5. Bibliographic references 4.