航天推进技术研究院主办
Yuan Xiaofeng,Xu Hualong,Xu Zhigao.Design of diagnostic knowledge mining system for liquid propellant rocket engine[J].Journal of Rocket Propulsion,2008,34(03):44-48.
液体火箭发动机诊断知识挖掘系统设计
- Title:
- Design of diagnostic knowledge mining system for liquid propellant rocket engine
- Keywords:
- rocket engine; fault diagnosis; data mining
- 分类号:
- V434
- 文献标志码:
- A
- 摘要:
- 基于对液体火箭发动机的试验与故障诊断现状分析,设计了液体火箭发动机故 障诊断知识挖掘系统DKMS,以实现试车数据的全面管理和故障诊断知识的高效提取。该系 统采用C/S结构.分为数据采集子系统、试车数据管理子系统和诊断知识挖掘子系统三大部 分。DKMS系统的设计为克服发动机故障诊断知识获取的瓶颈提供了一条新的途径。
- Abstract:
- Based on the review of the tests and fault diagnosis situation of the liquid propellant rocket engine,a diagnostic knowledge mining system(DKMS)is designed for ameliorating both the fire-test data management and diagnostic knowledge acquirement.The system,based on the client/ server architecture,consists of a data sampling subsystem,a fire-test management subsystem and a diagnostic knowledge mining subsystem.In fact,the DKMS provides a new approach for overcoming the bottleneck in diagnosis knowledge acquirement of the rocket engine.
参考文献/References:
[l]刘洪刚,吴建军,陈启智.基于混合知识模型和混合推理
策略的液体发动机智能故障诊断[J].推进技术,2003,
24(3):194-197.
[2]张振鹏.液体火箭发动机故障检测与诊断中的基础问题
研究[J].推进技术,2002,23[5):353—359.
[3]胡小平,张丽娟,下艳梅,等.液体火箭发动机故障检测
和诊断中数据挖掘策略的分析[J].国防科技大学学报,
2005,27(3):1-5.
[4] Letouneau S,Famili A,Matwin S.Data Mining for Prediction
of Aircraft Component Failure[J].IEEE InteUigence
Systems:SpeciM Issue on Data Mining.Amsterdan,
Netherlands,August:Fall.1999:59-56.
[5]Blair J,Shirkhodaie A.Diagnosis and Prognosis of Bearing
Using Data Mining and Numerical Visualiztion Techniques
[C].Proceedings of the 33rd Southeastern Symposium on
System Theory.Athens Ohio U.S.A 200h 395-399.
[6]杨文献,姜节胜.基于数据挖掘的柴油机气门故障诊断技术研究[J].机械工程学报,2004,40(10):25—29.
[7]张育林,吴建军,朱恒伟,等.液体火箭发动机健康监控技
术口叼.长沙:国防科技大学出版社,1998.
[8]Yuan Xiaofeng,Xu Hualong。Chen Shuhong.An Impro—
vement on the Constrained Association Rule Mining
Algorithm[C].Proceedings of the Ist International
Conference on Distal Information Management,Bangalore
India:Dec.2006:205-208.
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备注/Memo
收稿日期:2008—03一ll;修回日期:2008--04—21。 作者简介:袁晓峰(1975一),男,博士生,工程师,主要研究领域为数据挖掘与故障诊断。