Downward electronic floating launch aviation device with integrated external power track
Downward electronic floating launch aviation device with integrated external power track
The invention relates to the technical field of aviation devices, in particular to a descending type integrated external power track electronic floating shoot aviation device. The device comprises an acceleration track gradually changing from vertical transition to transverse transition or upward inclination; in the initial state, an electric bearing vehicle is connected to the upper end of the acceleration track in a suspended mode, and an aircraft is loaded on the electric bearing vehicle; and the electric bearing vehicle is further provided with a power relay mechanism for transmitting advancing power of the electric bearing vehicle to the aircraft. The problems that in the prior art, a device is limited by the weight of an aircraft, and consequently the aircraft needs longer time and acceleration distance to take off are solved; and a large amount of energy is consumed in the early take-off acceleration stage.
一种下行式集合外动力轨道电子浮射航空装置，涉及航空装置技术领域，包括由竖向过渡渐变为横向或上倾的加速轨道，初始状态下，加速轨道的上端部悬挂连接有电动承载车，电动承载车上装载有飞行器，电动承载车上还设有将其前进的动力传递给飞行器的动力接力机构。本发明解决了传统技术中的装置受限于飞机自身的重量，导致了飞机需要更长的时间和加速距离用以起飞；以及其在前期起飞加速阶段，消耗大量的能源的问题。
Document information
Downward electronic floating launch aviation device with integrated external power track
一种下行式集合外动力轨道电子浮射航空装置
2021-07-23
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 |
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