邹尧,蔡豫晋. 长桁类复材零件固化变形数值模拟与验证[J]. 航空制造技术, 2020, 63(23/24): 94-101. ZOU Yao, CAI Yujin. Numerical Simulation and Verification of Curing Deformation for Stringer Shaped Composite Parts. Aeronautical Manufacturing Technology, 2020, 63(23/24): 94-101.
ZOU Yao, CAI Yujin. Numerical Simulation and Verification of Curing Deformation for Stringer Shaped Composite Parts[J]. Aeronautical Manufacturing Technology, 2020, 63(23/24).
邹尧,蔡豫晋. 长桁类复材零件固化变形数值模拟与验证[J]. 航空制造技术, 2020, 63(23/24): 94-101. ZOU Yao, CAI Yujin. Numerical Simulation and Verification of Curing Deformation for Stringer Shaped Composite Parts. Aeronautical Manufacturing Technology, 2020, 63(23/24): 94-101. DOI: 10.16080/j.issn1671-833x.2020.23/24.094.
ZOU Yao, CAI Yujin. Numerical Simulation and Verification of Curing Deformation for Stringer Shaped Composite Parts[J]. Aeronautical Manufacturing Technology, 2020, 63(23/24). DOI: 10.16080/j.issn1671-833x.2020.23/24.094.
Numerical Simulation and Verification of Curing Deformation for Stringer Shaped Composite Parts
Based on the micromechanical model and resin shrinkage theory
a numerical simulation model of composite curing deformation was established. This model is used to simulate the U-shaped and V-shaped typical parts and the variable curvature stringer of the canard. During the curing process
the maximum deformation simulation results of the U-shaped and V-shaped typical parts were 11.413mm and 1.908mm
and the maximum deformation results measured by the test were 9.148mm and 1.802mm
respectively. Tracking and monitoring the stringer of the canard
and based on the four locating holes of the parts
the accuracy of the curing deformation value between numerical simulation and actual production is 95.6%
which fully verified the accuracy of the numerical simulation model. Using the deformation result
the stringer tooling compensation surface is established
and the error between the simulation profile and the design profile is controlled within 4%
which meets the requirements of engineering application.