飞机操纵面数字化互换性设计  

Digital interchangeability design of aircraft control surfaces

作　　者：李云鹏 姚雄华 高帅 LI Yunpeng;YAO Xionghua;GAO Shuai(Structure Design Institute,AVIC The First Aircraft Institute,Xi’an 710089,China)

机构地区：[1]航空工业第一飞机设计研究院结构设计研究所,西安710089

出　　处：《航空工程进展》2024年第1期169-175,共7页Advances in Aeronautical Science and Engineering

摘　　要：随着数字化装配技术的逐渐成熟和推广应用,适应数字量传递的互换性设计对于提升飞机操纵面设计效率、稳定装配质量和降低维护成本具有现实意义。以飞机操纵面的互换性设计为研究对象,针对互换性的要求分析设计要点,建立与数字化装配相协调的互换性设计流程;从操纵面的构型特征角度分析互换性设计的结构元素;提出实现操纵面互换性的技术途径,给出相应的参考指标;以某型飞机的副翼为例,对其进行互换性分析和设计,并通过实际装配进行检验。结果表明:本文建立的操纵面互换性设计流程合理可行,能够满足互换性要求。With the gradual maturity and application of digital assembly technology,the interchangeability design adapting to digital quantity transfer is of significant practical significance for improving the efficiency of aircraft control surface design,stabilizing assembly quality and reducing maintenance cost.Taking the interchangeability design of a certain type of aircraft control surface as the research object,the design points are analyzed according to the requirements of the control surface interchangeability,and the interchangeability design process coordinated with digital assembly is established.The structural elements of the interchangeability design are analyzed from the configuration characteristics of the control surface.The technical approach to realize the interchangeability of the control surface is proposed,and the corresponding reference indexes are given.Combined with the test method of aircraft interchangeability,the aileron of a certain type of aircraft is taken as an example to analyse and design the interchangeability of the control surface,which is verified by the actual assembly inspection.The results show that the design process of control surface interchangeability is feasible,which can satisfy the interchangeability requirements.

关 键 词：数字化装配 操纵面 互换性 设计流程 副翼 

分 类 号：V214.6[航空宇航科学与技术—航空宇航推进理论与工程]