The invention discloses a single-rotor helicopter without a balancing device. The single-rotor helicopter is provided with a rotor, a rotor shaft, a transmission device, an engine, a fuselage and thelike, and is characterized by comprising a connecting device which integrates balancing and transmission functions and integrates the balancing device and the transmission device, and the connecting device is connected to the rotor shaft and a rotating shaft of the engine. The single-rotor helicopter has the following advantages: an external balancing device which depends on an existing single-rotor helicopter, cannot be cut off all the time and is used for resisting counter torque is eliminated, and a major sudden change in the history of the single-rotor helicopter is completed; the single-rotor helicopter has the special advantage of simpler structure, the weight of the single-rotor helicopter can be reduced, the load can be increased, and the production cost can be reduced; and the application field and the application range of the single-rotor helicopter can be excavated and expanded in a multi-channel mode, and the competitiveness of the single-rotor helicopter, especially an unmanned helicopter, especially a large and medium-sized unmanned helicopter on the domestic and overseas markets is greatly improved.
本发明公开了一种无平衡装置的单旋翼直升机技术,具有旋翼、旋轴、传动装置、发动机、机身等,其技术特征在于:包括具有平衡与传动功能融合、平衡装置与传动装置一体化的联接装置,所述联接装置联接于旋轴与发动机转轴。本发明的优点是,摆脱了现有单旋翼直升机所依赖的且一直无法“割舍”的用于抵抗反力矩的外置平衡装置,完成了单旋翼直升机史上的一次重大突变;具有结构更加简单的特别优势,可使单旋翼直升机的重量变小、负荷变大,生产成本下降;可多渠道掘展单旋翼直升机的应用领域与使用范围,大幅度提高单旋翼直升机尤其是无人直升机特别是大中型无人直升机在国内外市场上的竞争力。
Single-rotor helicopter without balancing device
一种无平衡装置的单旋翼直升机技术
09.06.2020
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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