| 飞机铝合金蒙皮裂纹的粘接修补技术 |
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| 引用本文： | 代永朝. 飞机铝合金蒙皮裂纹的粘接修补技术[J]. 粘接, 2002, 23(3): 48-49 |
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| 作者姓名： | 代永朝 |
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| 作者单位： | 空军第一航空学院,河南省信阳市,464000 |
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| 摘 要： | 为提高飞机蒙皮裂纹的修补效能，通过优选材料合理地确定修补参数，有效地降低了裂纹附近的应力强度因子，恢复损伤结构的使用寿命。
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| 关 键 词： | 飞机 铝合金 蒙皮裂纹 粘接修补技术 材料优选 胶粘剂 |
| 修稿时间： | 2001-11-03 |
The bonding technolgy in repair of cracks on aluminium alloy skin of aircraft |
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| Dai Yongchao. The bonding technolgy in repair of cracks on aluminium alloy skin of aircraft[J]. Adhesion in China, 2002, 23(3): 48-49 |
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| Authors: | Dai Yongchao |
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| Abstract: | In order to increase the efficacy of repair for the cracks on aluminum alloy skin of aircraft,through the optimum of materials the repair parameters were determined.So that the intensive factor of the stress by craks was effectively decreased and the serviceable life of the damaged structure was renewed. |
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| Keywords: | Material optimum Repair parameter Adhesive Repair method |
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