Face-lifting electronic control aviation piston engine

The utility model relates to a face-lifting electronic control aviation piston engine, which comprises an all aluminum engine, a turbocharger, an engine electronic control system, a face-lifting lit, a power output end, a propeller mounting interface, an ISG integrated starter generator and a starti...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: WEI GUOAI, ZHAI JIYAO, WANG XIN, BIAN BAOPING, DONG YALI, LI FAJUN, GUO HENGYI, DENG HAIYAN
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The utility model relates to a face-lifting electronic control aviation piston engine, which comprises an all aluminum engine, a turbocharger, an engine electronic control system, a face-lifting lit, a power output end, a propeller mounting interface, an ISG integrated starter generator and a starting interface end, wherein the all aluminum engine is provided with the turbocharger and the engine electronic control system, the all aluminum engine, the turbocharger and the engine electronic control system form a minimum structure of a jet turbocharging all aluminum engine outside an electronic control cylinder, the all aluminum engine is connected to the propeller mounting interface through the power output end, and a propeller is arranged on the propeller mounting interface so as to output power to a shaft of the propeller. The face-lifting electronic control aviation piston engine solves the problem strong dependency on abroad electronic control aviation piston engines caused by shortage of small and medium-s