The invention relates to the technical field of aircraft design, in particular to a fixed hinge type flap actuator mounting structure which comprises a swing device, one end of the swing device is connected with a wing back rest, the other end of the swing device is connected with a flap control surface, and the swing device is used for retracting and releasing the flap control surface; the method has the effect of solving the problem that the flexibility and lightweight design of the system are limited.
本申请涉及飞行器设计技术领域,尤其涉及一种固定铰链式襟翼作动器安装结构,包括摆动装置,所述摆动装置一端与机翼后梁连接,另一端与襟翼舵面连接,所述摆动装置用于将襟翼舵面收放;本申请具有解决限制了系统的灵活性和轻量化设计的效果。
Fixed hinge type flap actuator mounting structure
一种固定铰链式襟翼作动器安装结构
2024-12-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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