Research on the Performance State Assessment of Aero-Engine Compressor Driven by Realistic Digital Aero-Engine Structure Model

被引:0
|
作者
Wu, Xin [1 ]
Wei, Xiaolong [1 ]
Xu, Haojun [1 ]
He, Weifeng [1 ]
Zhou, Liucheng [1 ]
Hou, Yuanhan [1 ]
Wang, Yixuan [1 ]
机构
[1] Air Force Engn Univ, Natl Key Lab Aerosp Power Syst & Plasma Technol, Xian 710000, Peoples R China
基金
中国国家自然科学基金;
关键词
Three-dimensional displays; Blades; Aircraft propulsion; Aerodynamics; Solid modeling; Geometric modeling; Image coding; 3-D reconstruction; aerodynamic performance; compressor; digital aero-engine; simulation evaluation; RECONSTRUCTION;
D O I
10.1109/TIM.2024.3427794
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
In this article, research on the performance state assessment of compressor with damaged blades driven by realistic digital engine structural model is conducted, and a real-time aerodynamic performance simulation method for damaged compressor based on heuristic end-to-end in situ 3-D reconstruction is proposed. We present a heuristic coarse-to-fine 3-D reconstruction framework (HeurisRecon). Heuristic gated recurrent unit (GRU) is designed to introduce the prior knowledge of intact compressor drawn geometric model into the 3-D reconstruction of damaged blade. Based on the drawn geometric model, 2-D-3-D pose estimation method is adopted to solve the problem that structure from motion (SFM) cannot correctly estimate the camera extrinsics of borescope in the narrow internal space of aero-engine, while avoiding the cumulative error caused by the registration between damaged blade 3-D reconstruction model and compressor drawn geometric model. A high-performance image feature extraction network (TCNet) based on the feature interaction between transformer and convolutional neural network (CNN) is designed to provide multilevels of image features with rich semantic information for coarse-to-fine 3-D reconstruction. Transformer is used to achieve adaptive fusion in the back projection process from feature maps to feature volume. The realistic 3-D model of compressor with damaged blades obtained through our in situ reconstruction method is used for aerodynamic performance simulation evaluation. A simplified implicit difference scheme and $k{-}\varepsilon $ turbulence model are adopted to solve Navier-Stokes (N-S) equations in simulation. Experimental results verify that the proposed in situ 3-D reconstruction method can provide high-fidelity 3-D model for the aerodynamic performance simulation evaluation. This research provides a new idea for the performance state assessment of aero-engine in service and can be used to support the battle damage repair and assessment of aero-engine.
引用
收藏
页码:1 / 1
页数:13
相关论文
共 50 条
  • [1] Assessment of Turbulence Model Predictions for an Aero-Engine Centrifugal Compressor
    Bourgeois, Jason A.
    Martinuzzi, Robert J.
    Savory, Eric
    Zhang, Chao
    Roberts, Douglas A.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2011, 133 (01):
  • [2] Research on Aero-engine Analytical Linearization model
    Song Han-qiang
    Li Ben-wei
    Lin Xue-sen
    Li Jin-fei
    2016 IEEE INFORMATION TECHNOLOGY, NETWORKING, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (ITNEC), 2016, : 976 - 980
  • [3] Failure Analysis of Compressor Blades of Aero-Engine
    Madhav, S.
    Roy, Manish
    JOURNAL OF FAILURE ANALYSIS AND PREVENTION, 2022, 22 (03) : 968 - 982
  • [4] Failure Analysis of Compressor Blades of Aero-Engine
    S. Madhav
    Manish Roy
    Journal of Failure Analysis and Prevention, 2022, 22 : 968 - 982
  • [5] Bayesian assessment on MTBF of aero-engine
    Dong H.
    Wan L.
    Yang Y.
    Yi X.
    1978, Beijing University of Aeronautics and Astronautics (BUAA) (32): : 1978 - 1983
  • [6] Design and Research of Aero-Engine State Monitoring System
    Yan, Wen
    Niu, Wei
    Zhao, Jianping
    2023 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL I, APISAT 2023, 2024, 1050 : 869 - 879
  • [7] Research on an aero-engine structure parametric design system
    Guo, Shufen
    1996, (11):
  • [8] Digital Twin-driven Aero-engine Assembly Technology
    Sun H.
    Yan J.
    Wei X.
    Chang Z.
    Zhongguo Jixie Gongcheng/China Mechanical Engineering, 2020, 31 (07): : 833 - 841
  • [9] Digital twin–driven aero-engine intelligent predictive maintenance
    Minglan Xiong
    Huawei Wang
    Qiang Fu
    Yi Xu
    The International Journal of Advanced Manufacturing Technology, 2021, 114 : 3751 - 3761
  • [10] Fouling Behavior of Aero-engine Compressor Blades Surface
    Yu Haifeng
    Chen Wei
    Cheng Li
    Zhang Wenjun
    CHINA SURFACE ENGINEERING, 2021, 34 (05) : 188 - 197