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�������պ����ѧѧ�� 2004, Vol. 30 Issue (04) :321-324    DOI:
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������, ϯƽ*
�������պ����ѧ ��е���̼��Զ���ѧԺ, ���� 100083
Parametric design of turbine blades based on feature modeling
Song Yuwang, Xi Ping*
School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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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.
Keywords�� aircraft engines   parameters   turbines   features   turbine blades     
Received 2003-11-15;


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������, ϯƽ.�����������ͼ���������ҶƬ���������[J]  �������պ����ѧѧ��, 2004,V30(04): 321-324
Song Yuwang, Xi Ping.Parametric design of turbine blades based on feature modeling[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2004,V30(04): 321-324
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