Experimental Investigation on Fatigue Characteristics of Metal-Rubber Material at High & Low Temperature

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Experimental Investigation on Fatigue Characteristics of Metal-Rubber Material at High & Low Temperature
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Key words:金属橡胶%弹性多孔材料%高低温环境%疲劳特性%刚度衰退%累积损伤

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[6]XU Jian-dong,GUO Bao-ting,ZHU Zi-gen and LI Qi-han.The Vibration Performance of Metal-Rubber Material[J].Journal of Aerospace Power,2004,19(5):619-622.

[7]ZHANG Shi-chao,YU Hui-chen,LI Ying.Investigation on Low Cycle Fatigue Properties of Superalloy GH3044 at Elevated Temperature[J].Journal of Aeronautical Materials,2013,33(1):100-104.

[8]HE Min,FENG Da-qiang,YANG Ling,JI Hong-hu.Experimental Investigation on Combustion Characteristics of Low Calorific Value Fuel[J].Gas Turbine Experiment and Research,2013(1):43-46.

[9]LI Ying,YU Hui-chen,ZHANG Guo-dong,LI Jia-rong,WU Xue-ren.Effect of Tensile Strain Dwell on the Low Cycle Fatigue Behavior of DD6 Nickel-Based Single Crystal Super-alloy at High Temperature[J].Gas Turbine Experiment and Research,2005,18(1):14-16.

[10]XING Yang,LI Zhao-hong,GUO Hai-hong,WANG Chang-liang,CUI Jin-hui and ZHAI Zheng.Experimental Investigation on High Temperature Starting of Carrier Based Aircraft Engine[J].Journal of Propulsion Technology,2018,39(6):1234-1239.

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[17]SUN Ruijie,YAN Xiaojun,NIE Jingxu.Failure Characteristics of Directional Solidification Turbine Blade Under High Temperature Low Cycle Fatigue Load[J].Acta Aeronautica et Astronautica Sinica,2011,32(2):337-343.

[18]WANG Yan-rong,SONG Zhao-hong and HOU Gui-cang.Experimental Evaluation of High Temperature Low Cycle Fatigue/Creep Life of Turbine Blade[J].Journal of Aerospace Power,2002,17(4):407-411.

[19]LI Di,WANG Yan-rong,LIAO Lian-fang,WANG Jia-guang,WEI Fei-fei.Investigation of High and Low Cycle Fatigue Experiment for a Curved Dovetail Assembly[J].Aeroengine,2016,42(3):61-66.

[20]DONG Chengli,YU Huichen,JIAO Zehui,KONG Fantao,CHEN Yuyong.High Temperature Low Cycle Fatigue Properties and Failure Mechanism of a TiAl Alloy[J].Journal of Aeronautical Materials,2017,37(5).

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