摘要
The design of landing gear is complicated due to the numerous considered elements.And the initial elements related to each other can also be influenced by different factors.Landing gear design often involves a very large variety of configurations,especially in the conceptual design phase.However,traditional method costs more time to complete the whole procedure for suitable configurations of landing gears.Therefore,the parametric modeling of component library for landing gear based on computer aided three-dimensional interface application/component application architecutre(CATIA/CAA)is proposed.According to the analysis of the characteristics of landing gear components,a method is presented to extract the primary parameters of landing gear components so that a systematic classification can be established.Further,the related theories and methods,including receiving geometrical parameters of the components and updating the parametrical model,displaying the component parts,are also illustrated.Finally,the development technology for component library is explained.The proposed modeling method can improve the efficiency of the whole design cycle for landing gear.
The design of landing gear is complicated due to the numerous considered elements. And the initial elements related to each other can also be influenced by different factors. Landing gear design often involves a very large variety of configurations, especially in the conceptual design phase. However, traditional method costs more time to complete the whole procedure for suitable configurations of landing gears. Therefore, the parametric mod- eling of component library for landing gear based on computer aided three-dimensional interface application/compo- nent application architecutre （CATIA/CAA） is proposed. According to the analysis of the characteristics of land- ing gear components, a method is presented to extract the primary parameters of landing gear components so that a systematic classification can be established. Further, the related theories and methods, including receiving geo- metrical parameters of the components and updating the parametrical model, displaying the component parts, are also illustrated. Finally, the development technology for component library is explained. The proposed modeling method can improve the efficiency of the whole design cycle for landing gear.
基金
Supported by the National Natural Science Foundation of China(51075203,51105197)
the Nanjing University of Aeronautics and Astronautics Research Funding(NS2010023)
