TY - JOUR
T1 - Integrated design platform of conceptual multidisciplinary for aerocrafts
AU - Sun, Jian Xun
AU - Zhang, Li Qiang
AU - Chen, Jian Jiang
AU - Liu, Ji Hong
PY - 2012/1
Y1 - 2012/1
N2 - To solve the problems such as coupling, inheritance relationship, information transfer, distributed and heterogeneous design, parallel computing, data management and knowledge sharing between subjects in conceptual design process, the functional requirements of aerocraft multidisciplinary integrated design were analyzed, and a system architecture of conceptual multidisciplinary integrated design platform for aerocraft was proposed. Based on the optimization and decoupling methods of Design Structure Matrix (DSM), the digital conceptual design process under integrated platform was proposed. Furthermore, key technologies of integrated platform were described in detail. The integrated platform oriented to conceptual multidisciplinary design of aerocraft was developed under the MyEclipse3.2 environment, and the multidisciplinary design was optimized by integrating a winged missile. The results verified the effectiveness and feasibility of proposed integrated platform.
AB - To solve the problems such as coupling, inheritance relationship, information transfer, distributed and heterogeneous design, parallel computing, data management and knowledge sharing between subjects in conceptual design process, the functional requirements of aerocraft multidisciplinary integrated design were analyzed, and a system architecture of conceptual multidisciplinary integrated design platform for aerocraft was proposed. Based on the optimization and decoupling methods of Design Structure Matrix (DSM), the digital conceptual design process under integrated platform was proposed. Furthermore, key technologies of integrated platform were described in detail. The integrated platform oriented to conceptual multidisciplinary design of aerocraft was developed under the MyEclipse3.2 environment, and the multidisciplinary design was optimized by integrating a winged missile. The results verified the effectiveness and feasibility of proposed integrated platform.
KW - Aerocraft conceptual design
KW - Digital design process
KW - Integrated platform
KW - Multidisciplinary integrated design
KW - Product design
UR - https://www.scopus.com/pages/publications/84863286732
M3 - 文章
AN - SCOPUS:84863286732
SN - 1006-5911
VL - 18
SP - 1
EP - 8
JO - Jisuanji Jicheng Zhizao Xitong/Computer Integrated Manufacturing Systems, CIMS
JF - Jisuanji Jicheng Zhizao Xitong/Computer Integrated Manufacturing Systems, CIMS
IS - 1
ER -