Separating mechanism and aircraft

The embodiment of the invention provides a separating mechanism and an aircraft. The separating mechanism comprises a socket, plug and a separating traction piece, wherein the socket is used for being arranged on a first separating piece, the plug is in plug-in connection with the socket along the a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ZHANG TAO, CHANG XINYUE, YANG CHUNLEI, CHENG LINGXIAO, NIAN YONGSHANG, WEI MIN, JIANG KAI, LI XUESI, WANG JINING, FAN JIAORONG, SHI RUOCHONG, CONG ENBO, WANG ZHIHONG, CHEN JUNJIE, DONG HAO, WAN GUIBIN, WANG LIHUA, SU ZHONGWEI, REN XINYU, LI SUOLAN, SUN RUNYU
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The embodiment of the invention provides a separating mechanism and an aircraft. The separating mechanism comprises a socket, plug and a separating traction piece, wherein the socket is used for being arranged on a first separating piece, the plug is in plug-in connection with the socket along the axial direction, and the separating traction piece comprises a plug connecting piece, a separating connection rod and a separating inhaul cable; the plug connecting piece is connected with the plug, one end of the separating connection rod is rotationally connected with the plug connecting piece, and the separating connection rod and the plug connecting piece rotate relatively in a plane where the axis of the socket is located; the other end of the separating connection rod is rotationally connected with the separating inhaul cable, and the separating connection rod and the separating inhaul cable rotate relatively in the plane where the axis of the socket is located; the separating inhaul cable is used for being co