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根据机上测量,用于预测和补偿薄壁零件加工变形的自适应优化方法
Long Wu1,2, Aimin Wang1, Kang Wang1
1Digital Manufacturing Institute, Beijing Institute of Technology, Beijing 100081, China.
Sensors (Basel, Switzerland)
|January 23, 2024
概括
本研究介绍了一种使用机上测量 (OMM) 和代用刚度模型 (SSM) 的代优化补偿方法,以减少薄壁航空航天部件的加工变形. 该方法可以考虑变化的刚性和预测错误,改善工件质量.
科学领域:
- 制造业 工程 制造工程
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
背景情况:
- 薄壁合金零件在航空航天领域至关重要,但在削过程中容易变形.
- 机械加工诱导的变形减少了这些关键部件的通过率.
- 现有的方法往往无法解释动态刚度变化和模型不准确性.
研究的目的:
- 开发一种代优化补偿方法,以减轻薄壁零件的加工变形.
- 通过考虑时间变化的工件刚度和预测模型错误来提高错误补偿的准确性.
- 为了提高薄壁航空航天部件的制造产量.
主要方法:
- 开发了替代度模型 (SSM),其中包含来自离散节点的度信息.
- 实现间歇机上测量 (OMM) 以实时监控错误.
- 引入了用于代模型改进的间层和间部分校正系数.
- 在关键节点上利用加工变形模拟和信息提取.
主要成果:
- 成功建立了SSM,可以捕捉跨切割层的离散节点的刚性.
- 通过间歇性OMM证明了对预测模型错误的抑制.
- 在深度和部分之间实现了对预测模型错误的代校正.
- 通过在薄壁部件上进行多次实验验证,验证了该方法的可行性.
结论:
- 提出的代优化补偿方法有效地解决了薄壁部件的加工变形.
- 将OMM和SSM与新型校正系数集成,可以显著提高准确性.
- 这种方法提高了由薄壁合金制造的航空航天部件的通过率和可靠性.
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