The invention discloses a chord-length-variable full-wing type tilting rotor solar unmanned aerial vehicle, the unmanned aerial vehicle comprises three sections of wings, a fuselage, rotors, solar cell panels, an energy storage system and a tilting mechanism, the three sections of wings are formed by splicing wings with two chord lengths, the solar cell panels are laid on the upper surfaces of the wings, and the tilting mechanism is arranged on the fuselage. Charging an energy storage system in the wing; the four rotors are installed at the positions, close to the front edge and the rear edge, of the main wing through tilting mechanisms correspondingly, and when the front flight is switched to be vertical, the front rotor tilts upwards and the rear rotor tilts downwards. The tilt-rotor unmanned aerial vehicle combines an existing tilt-rotor unmanned aerial vehicle technology and a solar power technology, has the characteristics of a solar unmanned aerial vehicle and a tilt-rotor unmanned aerial vehicle, and has the characteristics of rapid cruise flight, long endurance, no pollution, vertical take-off and landing, hovering and the like.
本发明公开了一种变弦长全翼式倾转旋翼太阳能无人机,所述无人机包括三段机翼、机身、旋翼、太阳能电池板、能源储存系统和倾转机构,上述的三段机翼为两种弦长尺寸的机翼拼接而成,机翼上表面铺设太阳能电池板,为机翼内部的能源储存系统充电;四个旋翼通过倾转机构分别安装在主翼的靠近前缘与靠近后缘处,前飞切换垂起时前旋翼向上倾转后旋翼向下倾转。本发明结合现有的倾转旋翼无人机技术和太阳能动力技术,兼具太阳能无人机和倾转旋翼无人机的特点,具有快速巡航飞行、长航时、无污染、垂直起降、空中悬停等特点。
Variable-chord-length full-wing type tilting rotor solar unmanned aerial vehicle
一种变弦长全翼式倾转旋翼太阳能无人机
2024-01-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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