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基于UGNX的航空发动机叶片造型方法研究
引用本文:王春侠,赵保军,汪苏,单鹏. 基于UGNX的航空发动机叶片造型方法研究[J]. 机床与液压, 2005, 0(12): 27-29
作者姓名:王春侠  赵保军  汪苏  单鹏
作者单位:1. 北京航空航天大学机械工程及自动化学院,北京,100083
2. 北京航空航天大学能源与动力工程学院,北京,100083
基金项目:国家985基金计划资助项目(2004)
摘    要:对航空发动机的关键元部件之一——涡轮叶片进行了三维空间造型方法的研究。基于UGNX的自由曲面造型功能,采用双三次B样条拟合方式建立了叶片型面的空间样条曲线模型,由此来构造叶片空间型面。同时对叶片曲面造型中的几个关键问题从数学上进行了分析和探讨,验证了其造型方法的可行性,这为后续叶片加工精度分析和误差补偿提供了理论依据。

关 键 词:UGNX 叶片 曲面造型
文章编号:1001-3881(2005)12-027-3
收稿时间:2004-07-27
修稿时间:2004-07-27

Research on the Blade Modeling of Aero -engine Based on UGNX
WANG Chun-xia,ZHAO Bao-jun,WANG Su,SHAN Peng. Research on the Blade Modeling of Aero -engine Based on UGNX[J]. Machine Tool & Hydraulics, 2005, 0(12): 27-29
Authors:WANG Chun-xia  ZHAO Bao-jun  WANG Su  SHAN Peng
Affiliation:1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100083, China; 2. School of Energy Source and Engine Engineering, Beihang University, Beijing 100083, China
Abstract:The 3 - D modeling was researched for the turbine blades which are crucial parts. The blade spline modeling was established by dual cubic B spline surface based on the free surface modeling function of UGNX, and the blade space surface was constructed. Some key problems were analyzed and discussed from the point of mathematics in blade modeling for validating the feasibility of modeling and roaching method. The above analysis provides an academic basis for the continual optimization design and error compensation of blades.
Keywords:UGNX    Blades    Surface modeling
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