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Updated: Jan 31, 2026

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Ultrasonic Fatigue Testing in the Tension-Compression Mode
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一种在高温空气动力疲劳负荷下对航空发动机外的测试方法.
Changjian Zhao1, Feng Yang1,2, Xiaohui Wang3
1China Academy of Launch Vehicle Technology, Beijing 100076, China.
The Review of scientific instruments
|January 30, 2026
概括
这项研究开发了一种用于高温空气动力学疲劳测试航空发动机外的模型. 优化的系统设计确保了精确的疲劳负载控制,提高了航空发动机的可靠性.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
背景情况:
- 航空发动机外需要严格的测试,以确保在操作压力下可靠性.
- 高温空气动力疲劳测试对于评估发动机启停周期期间的外性能至关重要.
研究的目的:
- 建立一个数学模型来模拟复合航空发动机外的地面高温空气动力疲劳测试.
- 分析测试系统参数的灵敏度,并研究温度-压力相互作用.
主要方法:
- 开发一个数学模型来模拟测试条件.
- 数字模拟和与实验数据的比较.
- 压缩和加热系统的灵敏度分析.
- 评估空气泄漏对负载控制的影响.
主要成果:
- 数字结果与实验数据有很强的一致性.
- 发现压力变化显著影响温度控制.
- 温度变化对压力控制的影响最小.
- 评估了空气泄漏对疲劳负载控制的影响.
结论:
- 通过优化热/压系统设计,可以实现精确的疲劳负载调节.
- 适当选择控制参数对于可靠的航空发动机外疲劳测试至关重要.
- 开发的模型有助于预测和提高航空发动机可靠性.
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