Parametric design of turbine blades based on feature modeling
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摘要: 针对航空发动机涡轮气冷叶片的结构特点,提出了叶片参数化建模的特征分类形式.然后,利用特征造型技术开发涡轮叶片的参数化设计系统;并以直背涡轮叶片为具体实例阐述了该参数化模块的开发过程,为航空发动机典型结构件的参数化奠定了基础.Abstract: Considering the geometric features of the air-cooled turbine bladesof the aircraft engines, the methods to sort the features in the parametric modeling of the blades were advanced. A parametric design system was developed with feature-based modeling technology. The development of the parametric module wasinstanced by the parametric design of a straight-back air-cooled turbine blade, which is the basis of the parameterization of the configuration accessory in the aircraft engines.
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Key words:
- aircraft engines /
- parameters /
- turbines /
- features /
- turbine blades
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[1] 朱 凯,王荣桥.叶片设计中用户自定义特征的分析与实现[J].机械设计与制造,2003,2(1):30~32 Zhu Kai, Wang Rongqiao. The analysis and realization of user-defined features in the design of blades[J]. Machine Design and Manufacturing, 2003, 2(1):30~32(in Chinese) [2] 赵 纬. 并行工程环境下基于特征的航发工作叶片设计与分析 . 北京:北京航空航天大学能源与动力工程学院, 1998 Zhao Wei. The design and analysis of aircraft engine blades based on features under the concurrent environment . Beijing:School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, 1998(in Chinese) [3] 齐从谦,崔琼瑶. 基于参数化技术的CAD创新设计方法研究[J]. 中国机械工程, 2003,14(8):681~683 Qi Congqian, Cui Qiongyao. Research on innovation design method of CAD based on parametric technology[J]. Mechanical Engineering of China, 2003, 14(8):681~683(in Chinese) -
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