An integration system for investment casting mould design of aeroengine turbine blade
turbine blade、mould design、information integration、information management、product master model、design process、data flow
5
TP391.7;TG249.5(计算技术、计算机技术)
National High-tech R&D Program863 Program2006AA04Z144;Key Technologies R&D Program2006BAF04B02
2008-07-23(万方平台首次上网日期,不代表论文的发表时间)
共5页
114-118