Abstract：The state of aircraft flexible tooling is affected by temperature, workpiece state, assembly process and other factors, and is often in a time-varying state. Its twin model has large dynamic information and is complex to build. A modeling method of digital twin geometric model based on finite state machine is proposed in this paper. The dynamic mapping of physical tooling in digital space is realized by means of real-time data acquisition and preprocessing, definition of state and its transfer mechanism, and parameterized geometric entity modeling, which lays a foundation for virtual simulation based on digital twin model. Taking the wing and fuselage docking platform as the object, digital twin geometric models of the wing adjustment mechanisms are established to verify the effectiveness of the method.
姜珊，王仲奇，夏松，杨盼，常正平. 飞机柔性工装数字孪生几何模型构建方法[J]. 航空制造技术, 2022, 65(12): 86-91/111.
JIANG Shan, WANG Zhongqi, XIA Song, YANG Pan, CHANG Zhengping. Construction Method of Digital Twin Geometry Model for Aircraft Flexible Tooling[J]. Aeronautical Manufacturing Technology, 2022, 65(12): 86-91/111.
2022, 
