淡江大學機構典藏:Item 987654321/112693
English  |  正體中文  |  简体中文  |  Items with full text/Total items : 62805/95882 (66%)
Visitors : 3944360      Online Users : 686
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/112693


    Title: Improvement for Reducing Vibration in Gas Turbine Engine Testing
    Authors: Hung, C.-C;Lo, M.-C;Li, Y.-H.
    Keywords: Hydraulic oil film;Oil film damping;Rotary machine;Vibration reduction
    Date: 2017-12-09
    Issue Date: 2018-02-03 02:11:24 (UTC+8)
    Abstract: In the study, fluid film damper is used for solving unexpectedly vibration phenomena, which was happened
    in air-breathing engine ground testing. Squeeze film damper, one kind of oil film damper, is vital for
    reducing the engine vibration and rotor shaft unbalance. It has already been applied in this kind of engine,
    however, the unexpected vibration still existed in the ground testing. In order to reduce the unbalance force,
    several treatments, for lower unbalance, are used for correcting vibration problem. Nevertheless,
    experimental results indicate the improvement is limited. However, with coating solid lubricant for
    enhancing squeeze film damping, which significantly decreases vibration problem. This study successfully
    provides an effective method to enhance the function of damper. Vibration during the operation of rotary
    machine is expected to be reduced to improve the stability, precision and increase the life of rotary
    machine. This technology can be applied to either gas turbine engine in military defense or
    machining tool for better product quality.
    Relation: 02-12
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

    Files in This Item:

    There are no files associated with this item.

    All items in 機構典藏 are protected by copyright, with all rights reserved.


    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback