The invention relates to the technical field of aircrafts, in particular to a hybrid aircraft which comprises stand columns fixedly installed on the ground and an aircraft body, a mooring rope is erected between the stand columns, driving wheels are installed at the bottom of the aircraft body, and motors for driving the driving wheels are installed on the sides, close to each other, of the driving wheels. Stabilizing supports are installed on the front face and the back of the right side of the bottom of the aircraft correspondingly, the ends, close to the aircraft, of the stabilizing supports are hinged to the aircraft, telescopic rods are hinged to the positions, located on the right sides of the stabilizing supports, of the bottom of the aircraft, one ends of the telescopic rods are hinged to the aircraft, and the other ends of the telescopic rods are hinged to the stabilizing supports. An anti-dumping device is installed at the bottom positions of the stabilizing supports. Consumption of non-renewable energy fuel oil can be converted into consumption of renewable resource electric energy, no pollution is caused to the environment, and meanwhile the use cost is low.
本发明涉及飞机技术领域,具体为一种混动飞机,包括固定安装在地面上的立柱和飞机,立柱之间架设有缆绳,飞机底部位置安装有驱动轮,驱动轮相互靠近一侧分别安装有驱动驱动轮的电机,飞机底部右侧正面和背部均分别安装有稳固支架,稳固支架靠近飞机一端与飞机铰接,飞机底部且位于稳固支架右侧位置铰接有伸缩杆,伸缩杆一端与飞机铰接,另一端与稳固支架铰接,稳固支架底部位置还安装有防倾装置,能够把不可再生能源燃油的消耗转换为可再生资源电能的消耗,不会对环境造成污染,同时使用成本也较低。
Hybrid aircraft
一种混动飞机
2021-02-19
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 |