Aircraft unlinked piston engine design

Аuthors

Zakharov S. A.¹, Gilevich D. D.¹, Kul'chikhin V. G.², Garanin I. V.^1*

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Tyumenskie Motorostroiteli,

*e-mail: garanin-nio203@yandex.ru

Abstract

Aircraft unlinked reciprocating engine design results are considered. Design alternatives are analyzed with respect to mass decreasing, reliability and effectiveness improvement. Gas generator to compressor power ratio is optimized with respect to engine output.

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