Adaptive on-wing gas turbine engine performance estimation

被引:0
|
作者
Luppold, Rob [1 ]
Brotherton, Tom [1 ]
Volponi, Al [2 ]
机构
[1] Intelligent Automat Corp, Poway, CA 92064 USA
[2] Pratt & Whitney, East Hartford, CT USA
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A key technological concept for producing reliable engine diagnostics and prognostics exploits the benefits of fusing sensor data, information, and/or processing algorithms. In this paper, we consider a real-time physics based model of a commercial turbofan engine called STORM: Self Tuning On-board, Real-time engine Model. The STORM system provides a means for tracking engine module performance changes in real-time. However, modeling error can have a corruptive effect on STORM's estimation of performance changes. Fusing an empirical neural network based model with STORM forms a unique hybrid model of the engine called enhanced STORM (eSTORM. This approach can eliminate the STORM engine diagnostic errors. A practical consideration for implementing the hybrid engine model, involves the application of some form of sequential model building to construct and specify the empirical elements. A methodology for constructing the empirical model (EM) in a sequential manner without the requirement for storing all of the original data has been developed. This paper describes the development of the adaptive hybrid model scheme for a commercial turbofan engine. This adaptive hybrid-modeling scheme has been implemented in real-time on an Intelligent Automation Corporation (IAC) computational platform. Model performance achieved with the automated update algorithm using real on-wing commercial aircraft engine data will be presented.
引用
收藏
页码:3691 / +
页数:3
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