飞机五性一体化协同工作平台框架设计  

Research on Aircraft Five Qualities Integration Design Environment

作　　者：严拴航[1] 梁力[1] 薛海红[1] 

机构地区：[1]中国航空工业集团公司第一飞机设计研究院,西安710089

出　　处：《航空工程进展》2014年第2期257-262,268,共7页Advances in Aeronautical Science and Engineering

基　　金：国防科工局技术基础科研项目(Z052013B003)

摘　　要：通过对比国内外可靠性、维修性、测试性、安全性和保障性工作现状,归纳了国内在飞机研制过程中五性一体化的设计特点以及在工程应用方面存在的问题与差距,给出飞机研制过程中开展五性一体化设计的流程和数据、工作及工具接口协同需求,然后对五性一体化协同设计平台进行了初步构想(包括平台建设原则、平台规划和平台建设中需要突破的关键技术等内容),为解决飞机研制过程中五性设计优化、整合及综合权衡以及数据共享等提供技术支持。The state-of-art of five qualities（reliability, maintainability, testability, safety and supportability） home and abroad are compared, and the five qualities integration design characteristics and engineering applica- tion problems such as data, activities and tools integration etc are summarized. On the basis of that, five quali- ties integration design program and design requirements during aircraft development are studied. Five qualities integration environment is preliminary built, including environment building rules, environment schedule and the required key techniques, all of which are described in detail, which provide technology support for five quail ties design and optimization, integration, integrated balance and data sharing during the process of the aircraft development.

关 键 词：五性一体化 飞机 流程 协同设计 

分 类 号：V37[航空宇航科学与技术—航空宇航推进理论与工程]