An aircraft jacking structure comprises a support, and the support is installed on the inner side of an aircraft body skin of an aircraft and comprises a groove concaved towards the inner side of the aircraft body skin; a movable member, which is installed in the groove, and is configured to be movable in the groove; the jacking connector is constructed to be capable of forcing the movable part to move towards the inner side of the machine body skin, so that the jacking connector partially enters the groove of the support so as to be detachably installed together with the support, and when the support is separated from the jacking connector, the movable part can move towards the inner side of the machine body skin. The surfaces, facing the outer side of the aircraft body skin, of the supports and the movable parts conform to the aerodynamic configuration of the aircraft. The invention further designs an aircraft comprising the aircraft jacking structure.
一种飞机顶起结构,包括支座,该支座安装在飞机的机体蒙皮内侧,并包括朝向机体蒙皮内侧凹入的凹槽;可运动部件,该可运动部件安装在凹槽中,并且构造成能够在凹槽中运动;以及顶起接头,该顶起接头构造成能够迫使可运动部件朝向机体蒙皮内侧运动,使得顶起接头部分地进入支座的凹槽,以与支座可拆卸地安装在一起,其中,当支座与顶起接头分离时,支座和可运动部件的朝向机体蒙皮外侧的表面符合飞机的气动外形。还设计一种包括该飞机顶起结构的飞机。
Aircraft jacking structure and aircraft
一种飞机顶起结构以及飞机
2025-04-18
Patent
Electronic Resource
Chinese
IPC: | 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 / 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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