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以A320飞机为原型,对现代民用飞机的缝翼操纵系统性能设计进行了原理性的阐述和探讨。首先简单介绍了现代民机缝翼操纵系统的基本构型,然后提出了缝翼操纵系统性能初步设计所需的输入条件,通过分析缝翼操纵系统中各个机械产品的载荷要求,给出了初步设计PDU功率的方法。该性能设计思路对中国民用飞机的设计具有一定的借鉴意义。
With A320 aircraft as a prototype, the performance design of slat control system of modern civil aircraft has been principally elaborated and discussed. Firstly, the basic configuration of the modern wing control system for civil aircraft is briefly introduced. Then, the input conditions required for preliminary design of slat control system performance are proposed. By analyzing the load requirements of each mechanical product in slat control system, Design PDU power method. This design idea of the performance of China’s civil aircraft design has some reference.