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Fault Analysis of Certain Aero鄄Engine Turbine Blades Broken
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    Abstract:

    The certain enging was disassembled and inspected because of its turbine blades being invalidated at
    ground starting. In this paper, it records the fault condition, takes computational analysis of clearance between low
    pressure first stage turbine working blades and low pressure first stage guide blades of the fault engine, takes metallur鄄
    gical analysis and workpiece processing analysis and durability testing and mutuality dimension chain computing for
    engine broken blades. Taking systems analysis for blades broken reason by fault tree, it finds out the reason of engine
    blades invalidated and advances improving advices.

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  • Received:
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  • Online: November 28,2016
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