基于构型项目分类的民机系统适航符合性证据体系结构研究  

Research on Configuration Item Classification Based on Civil Aircraft System Airworthiness Compliance Evidence System Structure

作　　者：卢艺[1,2] 郝莲[1] 李承立[1] 张曙光[2] 

机构地区：[1]上海飞机设计研究院,上海201210 [2]北京航空航天大学,北京100191

出　　处：《民用飞机设计与研究》2017年第3期26-30,4,共5页Civil Aircraft Design & Research

摘　　要：民机型号合格审定程序要求型号申请人通过系统性规划和实施型号研制过程,向局方提出正确、完整和可追溯的适航符合性证据,用"设计保证"确保产品符合适航规章要求。基于系统工程中"双V模型"(Validation&Verification,简称"双V模型")理论,以"研制规划保证回路"和"研制过程回路"为两条核心路径,辨识了证据体系与构型管理、民机系统研制过程及型号合格审定过程之间的接口关系,以飞机、系统和设备层级下的构型项目类型为框架,提出了以"规划保证"、"需求定义"、"逻辑/物理方案实现"、"确认数据"和"验证数据"五个维度构成的符合性证据体系,明确了证据链数据间的传递关系。Civil aircraft type certification procedure requires the type applicant to submit correct, complete and traceable airworthiness compliance evidences to the certification authority, following the systematic planning and implementation of type development processes. Such evidences show the development assurance on products against airworthiness regulation requirements. Based on the Vee model theory of the system engineering, this paper chooses the development planning and assurance loop and development process loop as two core routines to identify the in- terfaces of evidence system with the configuration management, system development and type certification proces- ses. Using the configuration item type classification under the aircraft, system and equipment levels as a frame- work, a compliance evidence system consisted by five dimensions of plan assurance, requirement definition, logi- cal/physical solution, validation data and verification data is proposed, which specifies the transferring relationship between the data links.

关 键 词：型号合格审定 适航要求 符合性证据体系 构型项目 

分 类 号：V221.91[航空宇航科学与技术—飞行器设计]