The invention relates to a foldable freely-combined electromagnetic catapult for an unmanned aerial vehicle, in particular to a first-order or N-order foldable freely-combined electromagnetic catapultfor an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicle launching. The electromagnetic catapult is composed of an unmanned aerial vehicle carrying trolley, a catapult device, a transmission device, a power device and a double-safety buffer device. the electromagnetic catapult for the unmanned aerial vehicle is designed by adopting a foldable free combinationmethod; various devices are freely combined according to the model of the unmanned aerial vehicle; ejection environments are diversified; ejection sites are diversified; the problem that a traditionalcatapult device is fixed in size, limited in launching power and the like is solved; all the devices are freely combined according to the model of the unmanned aerial vehicle, so that the size of thecatapult is adjustable, catapulting power is variable, and therefore, the launching requirements of different models of unmanned aerial vehicles are met.
一种可折叠自由组合式无人机电磁弹射器,具体为一阶或N阶可折叠自由组合式无人机电磁弹射器,所属无人机发射技术领域,电磁弹射器由无人机运载小车、弹射装置、传动装置、动力装置和双安全缓冲装置组成;本发明采用可折叠自由组合式的方法设计无人机电磁弹射器,根据无人机的型号将各装置进行自由组合,弹射环境多样化,弹射场地多样性,克服传统的弹射装置尺寸固定、发射动力有限等问题,根据无人机的型号将各装置进行自由组合,实现尺寸可调弹射动力可变,从而满足不同型号无人机的发射要求。
Foldable freely-combined electromagnetic catapult for unmanned aerial vehicle
一种可折叠自由组合式无人机电磁弹射器
2020-05-26
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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