The invention belongs to the technical field of aircraft ground facility design, and particularly relates to an aircraft launching and taking-off device which comprises a support, a take-off device and a take-off device. The yaw angle adjusting seat is connected to the support and can rotate relative to the support, and a plurality of locking supporting columns distributed around the rotation center of the yaw angle adjusting seat are arranged on the yaw angle adjusting seat; the yaw angle locking rod is adjustable in length, one end of the yaw angle locking rod can be connected to the positioning supporting column in a sleeving mode at any angle, and the other end of the yaw angle locking rod can be connected to any locking supporting column in a sleeving mode at any angle; the pitching support is hinged to the yaw angle adjusting seat; the pitching angle adjusting electric push rod is connected between the yaw angle adjusting seat and the pitching bracket so as to drive the pitching bracket to pitch around a hinged part relative to the yaw angle adjusting seat; the aircraft launching and takeoff slide rail is arranged on the pitching bracket; the aircraft launching takeoff booster rocket bracket is connected to the pitching support and can slide in the horizontal direction and the vertical direction of the pitching support.
本申请属于飞行器地面设施设计技术领域,具体涉及一种飞机发射起飞装置,包括:支座,其上具有定位支柱;偏航角度调整座,连接在支座上,能够相对于支座旋转,偏航角度调整座上具有环绕偏航角度调整座旋转中心分布的多个锁定支柱;偏航角度锁定杆,长度可调,一端能够以任意角度套接至定位支柱上,另一端能够以任意角度套接至任意一个锁定支柱上;俯仰支架,铰接在偏航角度调整座上;俯仰角度调整电动推杆,连接在偏航角度调整座、俯仰支架之间,以能够带动俯仰支架相对于偏航角度调整座绕铰接部位进行俯仰;飞机发射起飞滑轨,设置在俯仰支架上;飞机发射起飞助推火箭托架,连接在俯仰支架上,能够沿俯仰支架水平、竖直方向滑动。
Airplane launching takeoff device
一种飞机发射起飞装置
2022-04-12
Patent
Elektronische Ressource
Chinesisch
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 |
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