The invention discloses a rotor wing speed testing device of an electric unmanned helicopter, relates to the technical field of rotor wing speed testing of electric unmanned helicopters, and solves the problems that most of speed testing devices can only carry out one detection mode, the functionality is very single, and rapid detection is not facilitated. The rotor speed testing device of the electric unmanned helicopter comprises a base block, a fixed supporting column is fixedly welded to the upper end of the base block, a movable square column is movably arranged in the fixed supporting column, a measuring frame mechanism is fixedly welded to the upper end of the movable square column, and a wiring mechanism is movably arranged on one side of the upper end of the measuring frame mechanism. A first movable side plate on one side of the interior of a movable open cavity and a second movable side plate on the other side of the interior of the movable open cavity are poked inwards, so that a connection type spring between the second movable side plate and the second movable side plate stretches and elastically extrudes, and at the moment, an inserting block can be disengaged from the interior of a third clamping groove; therefore, the integral first movable side plate and the second movable side plate can be pulled upwards.

    本发明公开了一种电动无人直升机的旋翼速度测试装置,涉及电动无人直升机的旋翼速度测试技术领域,解决了的测速装置大部分只能进行一种检测方式,功能性十分单一,不利于快速的检测问题。一种电动无人直升机的旋翼速度测试装置,包括底座块,所述底座块的上端固定焊接有固定支柱,所述固定支柱的内部活动设置有活动方柱,所述活动方柱的上端固定焊接有测量架机构,所述测量架机构上端的一侧活动设置有接线机构。本发明通过向内侧拨动活动开腔内部一侧的第一活动侧板和另一侧的第二活动侧板,使得第二活动侧板对之间的连接型弹簧伸张弹性进行挤压,这时插装块可从第三卡槽内部脱出,从而使得整体的第一活动侧板以及第二活动侧板可向上拉动。


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    Titel :

    Rotor speed testing device of electric unmanned helicopter


    Weitere Titelangaben:

    一种电动无人直升机的旋翼速度测试装置


    Beteiligte:
    WU XINGGANG (Autor:in) / REN YAN (Autor:in) / CHEN XINYU (Autor:in) / ZHANG MENG (Autor:in) / CUI TONG (Autor:in)

    Erscheinungsdatum :

    2023-05-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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