本发明公开了一种可自动调节平稳性减速伞的降落测试装置,包括放置底座和叠加套壳,所述放置底座的上端设置有六个所述叠加套壳,六个所述叠加套壳的内部中间设置有测试容腔,所述叠加套壳的前端中间设置有探头密封套盖,本发明通过叠加套壳两端的测试风机便于吹送风力,这样经过测试风嘴块有效吹送风力到可自动调节平稳性减速伞的两侧,从而因探头密封套盖中的监控探头有效监控,可自动调节平稳性减速伞经过每个叠加套壳时,这样有效观测,而且每个叠加套壳因两端的测试风机,这样有效改变风力大小,从而便于观察不同风力对测试的影响,监控探头因照明灯体提供的照明光,使得监控更加清晰。

    The invention discloses a landing test device capable of automatically adjusting a stability brake parachute, which comprises a placement base and stacking sleeve shells, the upper end of the placement base is provided with six stacking sleeve shells, the middles of the interiors of the six stacking sleeve shells are provided with test cavities, and the middles of the front ends of the stacking sleeve shells are provided with probe sealing sleeve covers. According to the invention, the test fans at the two ends of the stacked sleeve shells are convenient to blow wind power, so that the wind power is effectively blown to the two sides of the automatically adjustable stability brake parachute through the test tuyere blocks, and the monitoring probe in the probe sealing sleeve cover is effectively monitored, so that the stability brake parachute can be automatically adjusted to pass through each stacked sleeve shell, and the observation is effective; and moreover, due to the test fans at the two ends of each superposed sleeve shell, the wind power is effectively changed, so that the influence of different wind power on the test is conveniently observed, and the monitoring probe enables the monitoring to be clearer due to the illumination light provided by the illumination lamp body.


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    Titel :

    一种可自动调节平稳性减速伞的降落测试装置


    Erscheinungsdatum :

    2024-06-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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 / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein