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Blank Panel Design of Integral Wing Skin Panels Based on Feature Mapping Methods
A blank panel design algorithm based on feature mapping methods for integral wing skin panels with supercritical airfoil surface is presented.The model of a wing panel is decomposed into features,and features of the panel are decomposed into information of location,direction,dimension and Boolean types.Features are mapped into the plane through optimal surface development algorithm.The plane panel is modeled by rebuilding the mapped features.Blanks of shot-peen forming panels are designed to identify the effectiveness of the methods.
作 者： Wang Junbiao Zhang Xianjie 作者單位： School of Mechatronics,Northwestern Polytechnic University 刊 名： 航空制造技術(shù) ISTIC 英文刊名： AERONAUTICAL MANUFACTURING TECHNOLOGY 年，卷(期)： 2007 ""(z1) 分類號： V2 關(guān)鍵詞： Feature mapping Integral wing panel Blank panel design【Blank Panel Design of Integral Wing 】相關(guān)文章：
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