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基于知識圖譜的航空發(fā)動(dòng)機PHM仿真驗證平臺設計
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中國航空發(fā)動(dòng)機研究院

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TP182;V228

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國家科技重大專(zhuān)項(2019-I-0019-0018、2019- I-001-001)


Design of Aircraft Engine PHM Simulation and Verification Platform Based on Knowledge Graph
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    摘要:

    針對航空發(fā)動(dòng)機PHM系統功能、性能驗證要求高、驗證內容多、驗證業(yè)務(wù)復雜等實(shí)際問(wèn)題,分析了國外先進(jìn)航空發(fā)動(dòng)機PHM系統開(kāi)發(fā)驗證情況及經(jīng)驗,提出了一種基于知識圖譜技術(shù)的PHM仿真驗證平臺設計方法。該方法利用了知識圖譜在具有的半結構化、高效性、直觀(guān)等特點(diǎn),實(shí)現了發(fā)動(dòng)機PHM驗證涉及到的故障模式、故障特征、算法模型及專(zhuān)家知識等大量信息知識的有效組織與管理。在此基礎上,進(jìn)一步面向發(fā)動(dòng)機PHM驗證數據量大、計算需求高等需求,采用大數據、數據挖掘、機器學(xué)習、云服務(wù)等技術(shù),搭建了基于知識圖譜的航空發(fā)動(dòng)機PHM仿真驗證平臺,實(shí)現了數據挖掘與信息提取、專(zhuān)家知識獲取、多層級融合診斷智能導向型推理等應用。最后,以某型發(fā)動(dòng)機為對象,介紹了發(fā)動(dòng)機PHM仿真驗證情況。經(jīng)實(shí)際驗證結果分析,該文提出的PHM仿真驗證平臺能夠有效解決航空發(fā)動(dòng)機PHM系統可驗證的歷史故障樣本少、驗證功能單一等問(wèn)題。

    Abstract:

    In response to practical issues such as high requirements for functional and performance verification of the aviation engine PHM system, multiple verification contents, and complex verification business, this paper analyzes the development and verification situation and experience of advanced aviation engine PHM systems abroad, and proposes a design method for a PHM simulation verification platform based on knowledge graph technology. This method utilizes the semi structured, efficient, and intuitive characteristics of knowledge graph to effectively organize and manage a large amount of information knowledge related to engine PHM validation, including fault modes, fault features, algorithm models, and expert knowledge. On this basis, further targeting the demand for large amounts of data and high computational requirements in engine PHM verification, a knowledge graph based aviation engine PHM simulation verification platform has been established using technologies such as big data, data mining, machine learning, and cloud services. Applications such as data mining and information extraction, expert knowledge acquisition, and multi-level fusion diagnosis intelligent guided reasoning have been implemented. Finally, taking a certain type of engine as the object, the PHM simulation verification of the engine was introduced. After analyzing the actual verification results, the PHM simulation verification platform proposed in this article can effectively solve the problems of limited historical fault samples and single verification function that can be verified in the aviation engine PHM system.

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范滿(mǎn)意,羅凱,馬英杰,韓崇鵬.基于知識圖譜的航空發(fā)動(dòng)機PHM仿真驗證平臺設計計算機測量與控制[J].,2023,31(6):305-313.

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  • 收稿日期:2023-04-28
  • 最后修改日期:2023-05-14
  • 錄用日期:2023-05-15
  • 在線(xiàn)發(fā)布日期: 2023-06-15
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