The cycloid propeller duct power device comprises an engine, a cycloid propeller system, supports, cover plates and a flow guide cover, the supports comprise the first support and the second support, the first support and the second support are installed at the two ends of the cycloid propeller system respectively, and the cover plates comprise the first cover plate and the second cover plate. The first cover plate and the second cover plate are installed on the two sides of the cycloidal propeller system respectively, the fairings comprise the first fairings and the second fairings, the first fairings and the second fairings are installed at the two ends of the support respectively, and the engine is installed in the first fairings and connected with the cycloidal propeller system. The cycloid propeller duct power device is arranged on the aircraft, and the market vacancy is filled.
一种摆线桨涵道动力装置及应用其的飞行器,包括发动机、摆线桨系统、支架、盖板和导流罩,所述支架包括第一支架与第二支架,所述第一支架与第二支架分别安装在摆线桨系统的两端,所述盖板包括第一盖板与第二盖板,所述第一盖板与第二盖板分别安装在摆线桨系统的两侧,所述导流罩包括第一导流罩与第二导流罩,所述第一导流罩与第二导流罩分别安装在所述支架的两端,所述发动机安装在第一导流罩内,且与摆线桨系统连接,将摆线桨涵道动力装置在飞行器上,填补了市场的空缺。
Cycloid propeller duct power device and aircraft applying cycloid propeller duct power device
一种摆线桨涵道动力装置及应用其的飞行器
2022-09-02
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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