Rotor unmanned aerial vehicle clears away device of fusible mass

The utility model discloses a rotor unmanned aerial vehicle clears away device of fusible mass, include gas storage conveyor components, shine subassembly, support group spare, high temperature fusioncutting subassembly and control assembly, high temperature fusion cutting subassembly passes through...

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Bibliographische Detailangaben
Hauptverfasser:	LIANG WEIFANG, GUAN JIAN, DENG XIAOKANG, YANG LIUHUI, WANG CHENLING, ZHU YANYU, LIN DONGXU, YANG SIYUAN, PAN GUOBIN, ZHENG JIANRONG, XU JIANFENG, WU HUANHUI, ZHANG JIANLIANG, LUO QINGXIONG, PENG DONGMING, ZOU ZHILUO, CAI DONGXIAO, CHI XIAOJIA, XU GUOWEI, SU YIHUI, ZHOU YANWEI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The utility model discloses a rotor unmanned aerial vehicle clears away device of fusible mass, include gas storage conveyor components, shine subassembly, support group spare, high temperature fusioncutting subassembly and control assembly, high temperature fusion cutting subassembly passes through support group spare to be connected with gas storage conveyor components, and support group spareincludes hollow insulating arm mounting bracket and install the hollow insulating arm on hollow insulating arm mounting bracket, and be equipped with the trachea in the hollow insulating arm, tracheaone end is connected with high temperature fusion cutting subassembly, and the other end is connected with gas storage conveyor components, and gas storage conveyor components, shine the subassembly and high temperature fusion cutting subassembly all is connected with support group 1. Adopt the utility model discloses a device can be solved prior art wing centre section unmanned aerial vehicle andclear away the problem that