Abstract An optimal design of the starter-generator integrated into aircraft engines is studied. The authors give a review for modern designs and technical solutions of the problem.
Comparison of two configurations of a starter-generator integrated into the aircraft engine
Russian Aeronautics ; 60 , 3 ; 463-468
2017-07-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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