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Updated: Jun 11, 2025

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Ultrasonic Fatigue Testing in the Tension-Compression Mode
Published on: March 7, 2018
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飞机级合金上的口和疲劳
Valentin Zichil1, Cosmin Constantin Grigoras1, Vlad Andrei Ciubotariu2
1Department of Engineering and Management, Mechatronics, "Vasile Alecsandri" University of Bacău, 157 Calea Mărăsesti, 600115 Bacau, Romania.
Materials (Basel, Switzerland)
|September 28, 2024
概括
缺口和低循环疲劳 (LCF) 显著降低了合金的抗拉强度和延长. 表面完整性对于飞机部件的强度至关重要,正如口和疲劳样本的机械性能降低所证明的那样.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 由于其强度与重量比,合金在航空航天领域至关重要.
- 像痕这样的表面缺陷可能会损害材料的完整性.
- 疲劳负荷可以加剧材料降解.
研究的目的:
- 研究口和低循环疲劳 (LCF) 对各种合金机械性能的综合影响.
- 建立数学模型来预测这些合金在拉伸应力下的行为.
- 突出表面完整性在航空航天应用中的重要性.
主要方法:
- 使用了六种合金类型的120个标本 (2024-T3,6061-T4,6061-T6,7075-T0,7076-T6).
- 在所有标本上使用CNC加工引入了口.
- 在拉力测试前,对60个标本进行低循环疲劳 (LCF) 预处理.
- 进行统计分析以开发预测模型.
主要成果:
- 与未划痕的标本相比,有划痕和有划痕疲劳的标本表现出明显较低的最终抗拉强度 (UTS) 和破裂时的延伸.
- LCF预处理放大了口对UTS和延长的有害影响.
- 数学模型是基于对数据的统计检查而开发的.
结论:
- 表面完整性是维持飞机组件结构完整性的关键因素.
- 切口和LCF协同降低合金的机械性能.
- 这些发现强调了需要对航空航天材料表面进行严格的质量控制.
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