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《China Mechanical Engineering》 2009-05
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Structural Layout Optimization Method of Aircraft Wing Based on Ant Colony Algorithm

Wang Wei1 Yang Wei1,2 Mu Penggang11.Northwestern Polytechnical University,Xi'an,7100722.Chengdu Aircraft Design & Research Institute,Chengdu,610041  
Aiming to study the optimal number of spars in the aircraft wing conceptual design process,this paper offered a new layout optimization method in detail for practical aircraft engineering,the problem of layout optimization was decomposed into two subsystem problems: sizing optimization and topology optimization.The matured criteria method was used to solve the first problem and the latter was transfered to the 0/1 program problem of N spars which was solved by ground structure approach combined an improved ant colony algorithm.With the introduction of the past ant-route database,the unnecessary repeated computation of objection can be avoided and therefore the effectiveness was improved greatly.Finally,the optimal number of wing spars and the optimal size of component of wing were achieved simultaneously when the ant colony reached convergence.The numerical example shows that the method proposed is effective and feasible for solving complex optimization and has good efficiency in the cutting of weight.
【CateGory Index】: V224
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