A control system that is used for engine main pump angle of aircraft ground testing

The utility model discloses a control system that is used for engine main pump angle of aircraft ground testing. A control system that is used for engine main pump angle of aircraft ground testing includes: the industrial computer, the step motor subassembly, the step motor subassembly with the indu...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Li Chunjing, Xin Dongdong, Zhang Ming, Tian Huichao, Li Shengyu
Format: Patent
Sprache:chi ; eng
Schlagworte:
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