杨天策1 ,张瑞2 ,蔡景1.航空发动机机载健康管理系统设计方法[J].航空发动机,2023,49(6):6-13
Design Method of Airborne Health Management System for Aeroengine
DOI:
Key Words:health management system  model-based system engineering  requirement analysis  functional design  aeroengine
作者单位
杨天策1 ,张瑞2 ,蔡景1 1.南京航空航天大学 民航学院南京 2111062.中国航发沈阳发动机研究所沈阳 110015 
摘要点击次数: 939
全文下载次数: 785
Abstract:In order to solve the problems of unclear forward design process, ambiguous design requirements, and lack of standardiza? tion in the correspondence between requirement and design and requirement traceability of aeroengine airborne health management system, based on the comparison of the existing health management functional architecture systems at home and abroad, combined with require? ment capture, requirement analysis and function allocation in forward design, the top-down forward design process of aeroengine health management system was studied, and the forward design process platform of aeroengine health management was developed to realize the de? sign of airborne functional architecture. By introducing model-based system engineering ideas and adopting an object-oriented engineering design approach, graphical design methods such as functional objective quantification, function description and module definition were es? tablished to verify the feasibility of this design method in hardware design. By studying the design method of aeroengine airborne health management system and analyzing the composition of airborne function, an extensible process platform was established, and feasible hard? ware design models were established using the model-based design method, so as to provide a reference for the design of aeroengine air? borne health management system.
查看全文  查看/发表评论  下载PDF阅读器