The invention relates to an airplane and a hanging structure thereof. The hanging structure comprises a hanging body, a front mounting section and a rear mounting section, the front mounting section and the rear mounting section are arranged on the hanging body, the hanging body is connected with the front portion of an engine through the front mounting section, the hanging body is connected with the rear portion of the engine through the rear mounting section, and the front mounting section comprises a first length adjusting mechanism; and the first length adjusting mechanism is used for adjusting the distance between the hanging body and the front portion of the engine so that the pitching angle of the engine can be increased or decreased. According to the airplane and the hanging structure thereof, the attitude of the engine is improved, and the flight stability of the airplane and the safety coefficient in the take-off and landing stages can be improved.
本发明涉及一种飞机及其吊挂结构。该吊挂结构包括吊挂本体及设置在吊挂本体上的前安装节和后安装节,吊挂本体通过前安装节与发动机的前部连接,吊挂本体通过后安装节与发动机的后部连接,前安装节包括第一长度调整机构,第一长度调整机构用于调整吊挂本体与发动机的前部之间的距离,以提升或降低发动机的俯仰角度。本发明提出了一种飞机及其吊挂结构,使发动机的姿态得以改善,能提升飞机的飞行稳定性及起飞和降落阶段的安全系数。
Airplane and hanging structure thereof
一种飞机及其吊挂结构
2021-05-11
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2024
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