Abrasion test device for aircraft control connecting rod

The invention discloses an aircraft control connecting rod wear test device, which comprises a basic frame, a swing motion mechanism, a rotating shaft mechanism and an axial loading mechanism, and is characterized in that the axial loading mechanism is used for applying an axial load to a push-pull...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LI QUNFANG, LI DONGHUI, TANG CHAO, QIN ZHENGQI, LIU TIANFU, LIU FUJIA, WANG LE
Format: Patent
Sprache:chi ; eng
Schlagworte:
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