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在民用飞机研发过程中,构型差异管理是适航验证类试验/试飞过程中进行的必要动作,用以评估当前设计构型能否满足试验/试飞进行的要求以及试验/试飞的适航代表性。从单机设计构型要求、适航验证类试验/试飞要求、型号设计构型、单机设计构型以及实物状态的角度出发,分析了适航验证类试验前后飞机的各类构型差异,并提出了构型差异管理模型。
In the development of civil aircraft, configuration variance management is a necessary action in the airworthiness verification test / flight test to assess whether the current design configuration meets the requirements of the test / flight test as well as the airworthiness representative of the test / test flight Sex. From the design requirements of stand-alone design, test / test requirements of airworthiness certification test, model design configuration, stand-alone design configuration and physical condition, the differences of various types of aircraft before and after airworthiness verification test are analyzed, The configuration difference management model.