Design and Realization of Aircraft Engine Wire Fault Detection Database

被引：0
|
作者：
Shi, Xudong [1 ]
Zhang, Zhenzhen [1 ]
Liu, Xiaolin [1 ]
机构：
[1] Civil Aviat Univ China, Aeronaut Automat Coll, Tianjin, Peoples R China
来源：
MICRO NANO DEVICES, STRUCTURE AND COMPUTING SYSTEMS | 2011年 / 159卷
关键词：
aircraft engine wire; fault detection; joint time-frequency domain reflection; database design;
D O I：
10.4028/www.scientific.net/AMR.159.274
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：
The engine is the core part of an airplane and its wire performance has a direct important impact on the safety. The detection of the engine wire fault costs much time and effort in the maintenance nowadays. Based on that, the technical data are well determined in the database of the fault diagnosis on airplane engine wire is presented in this paper. And furthermore, the function and operation of the database are given too. The time can be reduced and the efficiency can be improved significantly in maintenance by utilizing the database presented in this paper.
引用
收藏
页码：274 / 278
页数：5
相关论文
共 50 条
  • [31] Design and Realization of Fault Restoration System
    Wang Zhi-gang
    Li Qiang
    Li Chunhui
    Xue Lei
    [J]. PROCEEDINGS OF THE 2015 INTERNATIONAL INDUSTRIAL INFORMATICS AND COMPUTER ENGINEERING CONFERENCE, 2015, : 270 - 274
  • [32] Active aircraft fault detection and isolation
    Glavaski, S
    Elgersma, M
    [J]. IEEE SYSTEMS READINESS TECHNOLOGY CONFERENCE: 2001 IEEE AUTOTESTCON PROCEEDINGS, 2001, : 692 - 705
  • [33] Classification of aircraft maneuvers for fault detection
    Oza, NC
    Tumer, K
    Tumer, IY
    Huff, EM
    [J]. MULTIPLE CLASSIFIER SYSTEMS, PROCEEDING, 2003, 2709 : 375 - 384
  • [34] Research on engine fault diagnosis and realization of intelligent analysis system
    Chen Guojin
    Zhu Miaofen
    Wang Yaka
    Hu Yihuai
    Liu Bin
    [J]. 2006 IEEE INTERNATIONAL SYMPOSIUM ON INDUSTRIAL ELECTRONICS, VOLS 1-7, 2006, : 1789 - +
  • [35] Robust fault detection filter design with applications to steer-by-wire vehicles
    Gadda, Christopher D.
    Laws, Shad M.
    Gerdes, J. Christian
    [J]. PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION 2007, VOL 16: TRANSPORTATION SYSTEMS, 2008, : 215 - 223
  • [36] Research and Design on the Database Used for Aircraft Conceptual Design
    Wei Chenglong
    Liu Hu
    [J]. PROCEEDINGS OF THE 2012 INTERNATIONAL CONFERENCE ON COMMUNICATION, ELECTRONICS AND AUTOMATION ENGINEERING, 2013, 181 : 357 - 363
  • [37] Data-driven Fault Detection, Isolation and Estimation of Aircraft Gas Turbine Engine Actuator and Sensors
    Naderi, E.
    Khorasani, K.
    [J]. 2017 IEEE 30TH CANADIAN CONFERENCE ON ELECTRICAL AND COMPUTER ENGINEERING (CCECE), 2017,
  • [38] Hybrid Kalman filter approach for aircraft engine in-flight diagnostics: Sensor fault detection case
    Kobayashi, Takahisa
    Simon, Donald L.
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2007, 129 (03): : 746 - 754
  • [39] Least squares support vector machine for class imbalance learning and their applications to fault detection of aircraft engine
    Xi, Peng-Peng
    Zhao, Yong-Ping
    Wang, Pei-Xiao
    Li, Zhi-Qiang
    Pan, Ying-Ting
    Song, Fang-Quan
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 84 : 56 - 74
  • [40] Data-driven fault detection, isolation and estimation of aircraft gas turbine engine actuator and sensors
    Naderi, E.
    Khorasani, K.
    [J]. MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2018, 100 : 415 - 438
12345