Research on the Influence of Coaxial Rotor Configuration on the Propulsion of Multi-rotor UAVs

被引：0
|
作者：
Wang Hai [1 ,2 ]
Huang Qiang [1 ,2 ]
Yang Chunlai [1 ,2 ]
Zheng Yanchang [1 ,2 ]
Wen Li [3 ]
机构：
[1] Anhui Polytech Univ, Sch Mech & Automot Engn, Mid Beijing Rd, Wuhu 241000, Anhui, Peoples R China
[2] An Hui Key Lab Adv Numer Control & Servo Technol, Wuhu, Peoples R China
[3] Univ Sci & Technol China, Dept Precis Machinery & Precis Instrumentat, Hefei, Peoples R China
来源：
2018 13TH ANNUAL IEEE INTERNATIONAL CONFERENCE ON NANO/MICRO ENGINEERED AND MOLECULAR SYSTEMS (NEMS 2018) | 2018年
基金：
美国国家科学基金会;
关键词：
Coaxial rotor; micro UAVs; propulsion;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
In this paper, An experimental device for testing a coaxial rotor system was developed and a series related test experiments were carried out. The experimental device utilizes the principle of leverage to collect the propulsion generated by the rotor system by a force sensor. We can get the following conclusion through two comparison tests of the single-rotor system and coaxial rotor system: compared with a single rotor system, the configuration of the coaxial rotor can increase 34% of the thrust generated by a single rotor configuration.
引用
收藏
页码：361 / 364
页数：4
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