摘要
基于C/S架构,采用UML建模和可复用面向对象技术,开发了航空发动机典型故障信息管理系统。该系统以结构化和网络化的形式保存典型故障模式的基本信息、详细分析信息和相应的故障信息,并提供了方便的查询和输出的功能,具有可用性、灵活性和易扩展性的特征。
Based on C/S structure, a typical aeroengine failure information management system is developed by use of UML modeling and reusable object - oriented technology. The system includes the basic information, detailed analysis and related information of failure mode, which are all hierarchically stored in networks. This system has convenient inquiry and output functions, ensuring its usability,flexibillty and extensibility.
出处
《航空发动机》
2005年第2期55-58,共4页
Aeroengine
