Analysis of Oil Debris in an Aero Gas Turbine Engine

被引:3
|
作者
Mishra R.K. [1 ]
Kumar P. [1 ]
Prakash L. [1 ]
机构
[1] Regional Center for Military Airworthiness (Engines), Bangalore
关键词
Aero gas turbine engine; Debris count; Magnetic chip detector; Oil debris;
D O I
10.1007/s11668-017-0351-y
中图分类号
学科分类号
摘要
Oil debris count is an important health monitoring parameter in aero gas turbine engine. Present paper deals with the oil debris analysis collected from the bearing houses and gear box of a military gas turbine engine. Due to relative motion between stationary parts, wearing-out has taken place in turbine bearing house. Improper assembly or dimensional inaccuracies found to be the root cause of high debris generation. For wearing-out of the drive shaft in gear box, lapses in assembly procedure and improper tolerances are found to be responsible. Though high ‘g’ maneuvers of the aircraft, hard landings, missile launch and bird hit or foreign object impact can lead to such high debris in the oil circuit, utmost care needs to be taken during assembly. © 2017, ASM International.
引用
收藏
页码:1131 / 1138
页数:7
相关论文
共 50 条
  • [1] BUCKLING ANALYSIS OF AFTERBURNER LINER OF AN AERO GAS TURBINE ENGINE
    Potluri, Sri Shanti
    Patel, Surendra Kumar
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 6, PTS A AND B, 2009, : 29 - 36
  • [2] Failure analysis of an un-cooled turbine blade in an aero gas turbine engine
    Mishra, R. K.
    Thomas, Johny
    Srinivasan, K.
    Nandi, Vaishakhi
    Bhatt, R. Raghavendra
    [J]. ENGINEERING FAILURE ANALYSIS, 2017, 79 : 836 - 844
  • [3] Flow investigations in an aero gas turbine engine afterburner
    Kumar, S. Suresh
    Ganesan, V.
    [J]. Transportation - 2005, 2005, : 15 - 23
  • [4] Failure Analysis of Nozzle Guide Vane of a Low Pressure Turbine in an Aero Gas Turbine Engine
    Mishra, R. K.
    Thomas, Johney
    Srinivasan, K.
    Nandi, Vaishakhi
    Bhat, Raghavendra
    [J]. JOURNAL OF FAILURE ANALYSIS AND PREVENTION, 2014, 14 (05) : 578 - 587
  • [5] THE POTENTIAL OF CERAMICS FOR THE AERO GAS-TURBINE ENGINE
    BENNETT, A
    [J]. POWDER METALLURGY, 1986, 29 (03) : 169 - 169
  • [6] Failure Analysis of an Inter-shaft Bearing of an Aero Gas Turbine Engine
    Mishra R.K.
    Muduli S.K.
    Srinivasan K.
    Ahmed S.I.
    [J]. Journal of Failure Analysis and Prevention, 2015, 15 (2) : 205 - 210
  • [7] Failure analysis of turbine disc of an aero engine
    Witek, L
    [J]. ENGINEERING FAILURE ANALYSIS, 2006, 13 (01) : 9 - 17
  • [8] Using Lubricating Oil Filter Debris Analysis to Monitor Abnormal Wear of Aero-Engine
    Zhu, Zixin
    Zheng, Junzhong
    Chen, Dong
    [J]. ADVANCES IN POWER TRANSMISSION SCIENCE AND TECHNOLOGY, 2011, 86 : 821 - 824
  • [9] Impact of Foreign Object Damage on an Aero Gas Turbine Engine
    Mishra R.K.
    Srivastav D.K.
    Srinivasan K.
    Nandi V.
    Bhat R.R.
    [J]. Journal of Failure Analysis and Prevention, 2015, 15 (1) : 25 - 32
  • [10] Evolutionary design of gas turbine aero-engine controllers
    Chipperfield, AJ
    Fleming, PJ
    [J]. 1998 IEEE INTERNATIONAL CONFERENCE ON SYSTEMS, MAN, AND CYBERNETICS, VOLS 1-5, 1998, : 2401 - 2406