DU Jian-jing, WEI Zhen-wei, ZHAO Wen-xia, LIU Chang-kui. Cracking Analysis of High Pressure Fuel Pump of Aero-engine[J]. Failure Analysis and Prevention, 2019, 14(3): 179-183. DOI: 10.3969/j.issn.1673-6214.2019.03.008
    Citation: DU Jian-jing, WEI Zhen-wei, ZHAO Wen-xia, LIU Chang-kui. Cracking Analysis of High Pressure Fuel Pump of Aero-engine[J]. Failure Analysis and Prevention, 2019, 14(3): 179-183. DOI: 10.3969/j.issn.1673-6214.2019.03.008

    Cracking Analysis of High Pressure Fuel Pump of Aero-engine

    • After two long-time tests, the high pressure fuel pump was found to have cracks on the oil-out by fluorescence detection. The failure reasons of the fuel pump were studied by macroscopic observation, metallographic analysis, scanning electron microscopy, energy dispersive spectroscopy and micro-hardness analysis. The results show the crack initiated from the R corner of the oil-out and the crack is fatigue crack. The results of stress analysis show that there was stress concentration at the R corner. In addition, there was pitting corrosion at the R corner surface, increasing stress concentration and promoting the initiation of the fatigue crack.
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