The invention discloses an aircraft supporting platform with a rotating function, and relates to the field of aircraft platforms. The platform comprises a platform body, an inner cavity is formed in the platform body; grooves are respectively formed in two side wall surfaces of the inner cavity; electric sliding rails are fixedly mounted in the grooves respectively; and a blocking door is fixedlymounted at the driving end of each electric sliding rail. The inner cavity is formed in the platform body to store an aircraft capable, the storage space of the aircraft is saved; through a lifting device, the function that the aircraft automatically rises under the action of a bearing box can be achieved, and the self-taking time of a user is reduced; the take-off direction of the aircraft is adjusted through a rotating device on the bearing box, so that a user can select more take-off directions; the aircraft is buffered through a damping device during landing, rigid collision between the aircraft and the platform is prevented, the platform body and the aircraft are protected, and the service life of the platform body is prolonged.
本发明公开了一种具有转动功能的飞行器支撑平台,涉及飞行器平台领域,包括平台本体,所述平台本体上开设有内腔,所述内腔两侧壁面上分别开设有凹槽,所述凹槽内分别固定安装有电动滑轨,所述电动滑轨驱动端上分别固定安装有挡门,通过在平台本体内部设置内腔,可以存放飞行器,节省了飞行器的存放空间,通过升降装置可以实现飞行器在承载箱的作用下自动上升的功能,节省使用者自取的时间,并且通过承载箱上的转动装置调节飞行器的起飞方向,使得使用者更多的起飞方位选择,通过减震装置使得飞行器降落时进行缓冲,防止飞行器与平台之间发生刚性碰撞,对平台本体以及飞行器进行防护,提高平台本体的使用寿命。
Aircraft supporting platform with rotating function
一种具有转动功能的飞行器支撑平台
2020-07-28
Patent
Electronic Resource
Chinese
IPC: | 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 / B66F HOISTING, LIFTING, HAULING, OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD , Hub-, Verhol- oder Schubvorrichtungen, soweit nicht anderweitig vorgesehen, z.B. Vorrichtungen mit unmittelbarer Krafteinwirkung auf die Last / F16F SPRINGS , Federn |
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