Invention Grant
- Patent Title: Method for prediction of key performance parameter of an aero-engine transition state acceleration process based on space reconstruction
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Application No.: US16629752Application Date: 2018-06-27
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Publication No.: US11436395B2Publication Date: 2022-09-06
- Inventor: Shuo Zhang , Xiaoyu Sun , Jibang Li , Ximing Sun
- Applicant: Dalian University of Technology
- Applicant Address: CN Dalian
- Assignee: Dalian University of Technology
- Current Assignee: Dalian University of Technology
- Current Assignee Address: CN Dalian
- Agency: Muncy, Geissler, Olds & Lowe, P.C.
- International Application: PCT/CN2018/093077 WO 20180627
- International Announcement: WO2020/000248 WO 20200102
- Main IPC: G01M15/00
- IPC: G01M15/00 ; G06F30/27 ; G06N20/10 ; G06K9/62 ; G06N5/00 ; G06F119/08 ; G06F30/15

Abstract:
A method for prediction of key performance parameters of an aero-engine transition state acceleration process based on space reconstruction. Aero-engine transition state acceleration process test data provided by a research institute is used for establishing a training dataset and a testing dataset; dimension increase is conducted on the datasets based on the data space reconstruction of an auto-encoder; model parameters optimization is conducted by population optimization algorithms which is represented by particle swarm algorithm; and random forest regression algorithm performing well on high-dimensional data is used for carrying out regression on transition state performance parameters, which realizes effective real-time prediction from the perspective of engineering application.
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