东北大学学报（自然科学版）

东北大学学报(自然科学版) ›› 2006, Vol. 27 ›› Issue (5): 485-488.DOI: -

• 论著 • 上一篇    下一篇

航空发动机涡轮设计集成技术

王成恩;刘震;   

  1. 东北大学教育部暨辽宁省流程工业综合自动化重点实验室;东北大学教育部暨辽宁省流程工业综合自动化重点实验室 辽宁沈阳110004;辽宁沈阳110004
  • 收稿日期:2013-06-23 修回日期:2013-06-23 出版日期:2006-05-15 发布日期:2013-06-23
  • 通讯作者: Wang, C.-E.
  • 作者简介:-
  • 基金资助:
    教育部新世纪优秀人才计划项目(NCET-04-0281);;

Integration technologies for design of aero-gas turbine

Wang, Cheng-En (1); Liu, Zhen (1)   

  1. (1) Key Laboratory of Process Industry Automation of Liaoning Province, Northeastern University, Shenyang 110004, China
  • Received:2013-06-23 Revised:2013-06-23 Online:2006-05-15 Published:2013-06-23
  • Contact: Wang, C.-E.
  • About author:-
  • Supported by:
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摘要： 航空发动机设计需要大量的计算软件,因此,设计数据和应用系统的集成具有高度科学价值和工程应用价值·采用COM组件技术,研究了航空发动机涡轮设计的多学科综合集成方法;采用代理对象封装空气动力学、热力学和结构计算程序,利用COM对象调用机制完成跨进程服务请求和响应·基于COM组件的集成系统可以实现专业计算软件注册、运行控制、数据映射、设计方案管理和知识管理等功能·系统支持可视化设计方案仿真和项目组人员在线协同,提高了设计工作效率和设计质量,缩短了设计周期·

关键词: COM组件, 发动机涡轮设计, 系统集成, 协同设计, 知识管理

Abstract: Aero-engine design involves a number of software packages, to which the integration of design data with application system is of highly technological and industrial significance. The component-based COM is introduced in integrating the multidisciplinary computing packages applicable to the design of aero-gas turbine, with the agent objects used to pack a number of aerodynamic, thermodynamic and structural computing packages so as to provide the trans-processing request-response service on the basis of COM call mechanism. The COM-based integration system provides a variety of functions, such as computing package registration, running control, parameter mapping, design specification management and knowledge management. The system can also support the visualized design simulation and on-line collaboration among single project designers, thus improving the efficiency and quality of design and shortening effectively the time required for design.

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