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| 某型发动机压气机第1级整流叶片疲劳试验研究 | |
| 引用本文： | 万利,李舜酩,金业壮.某型发动机压气机第1级整流叶片疲劳试验研究[J].航空发动机,2008,34(3):15-17. |
| 作者姓名： | 万利 李舜酩 金业壮 |
| 作者单位： | 1. 南京航空航天大学能源与动力学院,南京,210016;沈阳黎明航空发动机(集团)有限责任公司,沈阳,110043 2. 南京航空航天大学能源与动力学院,南京,210016 3. 沈阳航空工业学院航宇学院,沈阳,110136 |
| 摘 要： | 对某型发动机压气机第1级整流叶片进行了疲劳试验研究.确定了圆柱形榫头叶片的试验装夹方式,进行了2种工艺叶片振动疲劳强度试验的对比,根据对比结果,优化了加工工艺,进行了首批研制检验.对计算和试验结果进行了分析. |
| 关 键 词： | 航空发动机 叶片 疲劳试验 |
Fatogie Test of an Aeroengine compressor IGVs |
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| Authors: | WAN Li LI Shun-ming JIN Ye-zhuang |
| Institution: | WAN Li1.2,LI Shun-ming1,JIN Ye-zhuang3 (1.College of Energy , Power Engineering,Nanjing University of Aeronautics , Astronautics,Nanjing 210016,China,2.Shengyang Liming Aeroengine Group Corporation.Ltd.Shengyang 110043,3.College of Aeronautics , Aerospace Engineering,Shenyang Institute of Aeronautical Engineering,Shenyang 110136,China) |
| Abstract: | The fatigue test of an aeroengine compressor IGVs was introduced.The fastness method for IGVs with columned rabbet was determined.The comparative vibration fatigue test for two IGVs were completed with and without fine polishing and finish,and the optimized process was selected.The first batch of IGVs was tested and inspected.The results of the test and calculation were studied. |
| Keywords: | aeroengine compressor IGVs fatigue test |
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