Small composite wing unmanned aerial vehicle power testing device and testing method thereof
Small composite wing unmanned aerial vehicle power testing device and testing method thereof
- Neue Suche nach: WANG LEI
- Neue Suche nach: AI XINWEI
- Neue Suche nach: ZHANG XU
- Neue Suche nach: ZHANG BOSHI
- Neue Suche nach: WANG LEI
- Neue Suche nach: AI XINWEI
- Neue Suche nach: ZHANG XU
- Neue Suche nach: ZHANG BOSHI
The invention relates to a small composite wing unmanned aerial vehicle power testing device and a testing method thereof. The small composite wing unmanned aerial vehicle power testing device comprises a platform support, a plurality of power mounting units and a push-pull force testing unit; theplatform support is a cubic frame and comprises an upper frame, stand columns and a lower frame, a first cross beam is arranged in the middle of the upper frame, two second cross beams are arranged at the front end of the upper frame, and a bottom plate is installed at the rear end of the upper frame; the plurality of power mounting units are fixedly mounted on the upper frame; and the two ends of the push-pull force testing unit are respectively connected with the middle positions of the two second cross beams and airborne equipment, and the push-pull force testing unit is fixedly arranged on the bottom plate. The small composite wing unmanned aerial vehicle power testing device and the testing method thereof have the advantages of being high in accuracy, easy and convenient to operate, convenient to install, capable of achieving power performance testing of various motors and matched propellers and the like. According to the small composite wing unmanned aerial vehicle power testing device and the testing method thereof, the technical problems that an existing power testing device is large in measurement error, small in application range and complex in installation process can be solved.
本发明涉及一种小型复合翼无人机动力测试装置及其测试方法，其中，小型复合翼无人机动力测试装置包括：一平台支架，为立方体框架，包括上框架、立柱和下框架，在上框架中间设置第一横梁，前端设置两根第二横梁，后端安装一底板；多个动力安装单元，固定安装于所述上框架上；一推拉力测试单元，其两端分别连接两根所述第二横梁的中部位置以及一机载设备，固定安装于所述底板上。本发明小型复合翼无人机动力测试装置及其测试方法具有精确度高、操作简便、便于安装且能够实现多种电机及配套螺旋桨的动力性能测试等特点。本发明小型复合翼无人机动力测试装置及其测试方法能解决现有动力测试装置存在测量误差大、应用范围小、安装过程复杂的技术问题。
Dokumentinformationen
Small composite wing unmanned aerial vehicle power testing device and testing method thereof
小型复合翼无人机动力测试装置及其测试方法
2021-08-03
Patent
Elektronische Ressource
Chinesisch
| 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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