涡轮叶片导管快速建模

李吉星; 席平

doi:10.13700/j.bh.1001-5965.2015.0386

涡轮叶片导管快速建模

doi: 10.13700/j.bh.1001-5965.2015.0386

李吉星,
席平^,

北京航空航天大学机械工程及自动化学院, 北京100083

详细信息

作者简介:
李吉星男,博士研究生。主要研究方向:计算机辅助设计与制造、几何形状分析等。Tel.:010-82316747 E-mail:li_jixing@buaa.edu.cn;席平女,博士,教授,博士生导师。主要研究方向:飞行器辅助设计与制造、复杂曲线曲面造型等。Tel.:010-82316768 E-mail:xiping@buaa.edu.cn

通讯作者:
席平,Tel.:010-82316768 E-mail:xiping@buaa.edu.cn

中图分类号: TP391.7;V232.4
计量
- 文章访问数: 1212
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- 被引次数: 0
出版历程
- 收稿日期: 2015-06-11
- 网络出版日期: 2016-06-20

Rapid modeling of impingement pipe in turbine blade

LI Jixing,
XI Ping^,

School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 导管是涡轮叶片冲击冷却的核心部件。为实现复杂冷却结构叶片导管的快速建模,提出了创成式导管快速建模方法。首先应用截形法构建适应叶片内腔几何形状的管身截面线以创建管身,然后应用截交包络裁剪法与特征等弧长阵列方法保证了导管冲击孔与导管突起的建模稳定性与建模效率,并构建了突起定位迭代公式,保证了导管与叶片内腔的配合精度。最后采用UG Open API工具开发了导管快速建模程序,验证了所提方法的可行性。
- 导管 /
- 参数化设计 /
- 涡轮叶片 /
- 建模 /
- UG Open API
Abstract: Impingement pipe is the core component of the impingement cooling in turbine blade. In order to realize the rapid modeling of impingement pipe in turbine blade with complex cooling structure, a generative rapid modeling method was proposed.Firstly, the body of pipe was created by section curves which suits the shape of channel in blade and generated by curves created by insect-shape method. Then by using envelope surface trimming method and along-curve array method, the modeling stability and efficiency of cooling hole and hump are guaranteed.And the fitting precision between impingement pipe and blade is guaranteed by an iterative formula about protrude position.Finally, a rapid impingement pipe modeling program was developed based on UG Open API, and the modeling result validated the feasibility of the proposed method.
- impingement pipe /
- parametric design /
- turbine blade /
- modeling /
- UG Open API

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参考文献(14)

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