变室翼领先边缘的地面强度测试技术
Shanshan Li1, Xianmin Chen1, Zhigang Wang1
1National Key Laboratory of Strength and Structural Integrity, Aircraft Strength Research Institute of China, Xi'an 710065, China.
Biomimetics (Basel, Switzerland)
|August 28, 2024
概括
一种新的地面强度测试技术准确地评估了飞机前端的变形. 该方法在模拟飞行条件下精确测量变形和结构强度,提高飞机性能.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 材料科学 材料科学 材料科学
背景情况:
- 变形翼技术对于提高飞机飞行性能至关重要.
- 在飞行条件下监测全尺寸的可变曲面前边具有重大挑战.
- 准确评估变形和结构强度对于操作完整性至关重要.
研究的目的:
- 引入和验证一个新的基于地面的强度测试技术,用于可变斜率前边.
- 在模拟实际操作期间精确评估变形模式和结构强度.
- 为测试和评估变形翼组件提供科学证据和技术支持.
主要方法:
- 基于动力学理论的数值模拟来分析运动特征.
- 为模拟变形和空气动力学负载而设计和建造跟踪负载测试装置.
- 多点协调控制系统和多传感器代方法,用于准确的实验控制和加载精度.
主要成果:
- 开发的技术在运动测试中实现了4.59%的平均偏斜角度误差.
- 强度测试显示,负载大小的平均误差为0.54%,负载方向的平均误差为0.24%.
- 该方法准确模拟飞行条件,捕捉前沿形状,变形和拉伸曲线.
结论:
- 拟议的地面强度测试技术有效地模拟了变形翼的飞行条件.
- 该技术提供了关于前沿形状变化和结构反应的准确数据.
- 这项研究提供了一种可靠的方法来测试和评估可变曲率前端,支持未来的航空航天技术进步.
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