The invention relates to the technical field of unmanned aerial vehicles, and discloses an oil way refitting structure of an unmanned aerial vehicle, which comprises a wing oil tank, an oil filter, avaporizer and an engine. The wing oil tank includes a left wing oil tank and a right wing oil tank, wherein the left wing oil tank is connected with an oil filter through a gasoline electromagnetic valve and the right wing oil tank is connected with an oil filter through a gasoline electromagnetic valve; one end of the oil filter is connected with the vaporizer through the oil injection pump, andthe other end is directly connected with the vaporizer; and the vaporizer is connected with the engine. The gasoline solenoid valve is used to control the oil inlet amount of the left wing oil tank and the right wing oil tank instead of an oil tank selection switch, and the oil injection pump is selected to replace a hand pump and an oil injection pump to supply oil to the engine, meanwhile, the oil injection solenoid valve is used for controlling oil supply, and the control stability of the oil way system is improved.
本发明涉及无人机技术领域,且公开了一种无人机油路改装结构,包括机翼油箱、油滤、汽化器和发动机,所述机翼油箱包括左机翼油箱和右机翼油箱;所述左机翼油箱通过汽油电磁阀与油滤连接;所述右机翼油箱通过汽油电磁阀与油滤连接;所述油滤的一端通过注油泵与汽化器连接,另一端与汽化器直连;所述汽化器与发动机连接。本发明选用汽油电磁阀代替油箱选择开关对左、右机翼油箱的进油量进行控制,选用注油泵代替手摇泵和注油唧筒对发动机进行供油,同时通过注油电磁阀对供油进行控制,提高了该油路系统的控制稳定性。
Oil way refitting structure of unmanned aerial vehicle
一种无人机油路改装结构
2020-09-18
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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