Shape Prediction for Laser Peen Forming of Fiber Metal Laminates by Experimentally Determined Eigenstrain

Author(s):  
Zhengyu Zhang ◽  
Yongxiang Hu ◽  
Zhenqiang Yao

Laser peen forming (LPF) is a promising method to fabricate fiber metal laminates (FMLs) with its design flexibility to produce complex shapes. Eigenstrain-based modeling is a helpful method to predict deformation after LPF, while determining eigenstrain is very difficult because of its complex constituents and high-dynamic loading of process. An effective experiment-based method is proposed in this work to obtain eigenstrain induced by LPF in metal layers of FMLs. An analytical beam model is developed to relate the deflection profile generated by specific scanning strategy to equivalent bending moment. Based on the determined bending moment from the measured deflection profiles, the generated eigenstrain can be inversely calculated by the proposed beam model describing the relationship between the eigenstrain and the bending moment. Chemical etching to remove sheets layer by layer is used to obtain the relaxed deflection profile to calculate the eigenstrain in each metal layer. Furthermore, an approximate model of plate is established to predict deformation after LPF based on determined eigenstrain. The results show that the predictive deformed shape agrees very well with both experiments and finite model prediction.

Author(s):  
Zhengyu Zhang ◽  
Yongxiang Hu ◽  
Zhenqiang Yao

Fibre metal laminates are new sorts of composite materials with superior fatigue and impact properties. Forming parts from FMLs is very attractive to reduce the process cycle and labor cost. Laser peen forming (LPF) is a promising method to form FMLs with its design flexibility and adaptability to produce complex shapes. To predict the deformed shape of FMLs after laser peen forming, eigenstrain-based modelling is a helpful method with advantage in spending less computational time, but it is difficult to precisely determine eigenstrain distribution regarding material with layered structure. In the present research, an efficient and effective experiment-based method is proposed to determine eigenstrain in the metal layer of FMLs, which can avoid the complicated numerical simulation. The determined eigenstrain is assumed to be uniformly distributed in each metal layer while no plastic deformation is generated in composite layer due to its high strength yield. An analytical model is developed to relate the bending deformation to eigenstrain field. Firstly, the equivalent external bending moment applied on the samples is deduced from eigenstrain, and then the relation of deformation and bending moment is provided by a beam bending model. Chemical etching is utilized to remove metal layer by layer to calculate eigenstrain in each layer. With removal of each metal layer, the bending profiles will spring back or bend further due to change of applied moment and bending stiffness. The eigenstrain in each layer can be inversely determined by matching the residual bending profile after each etching with the developed bending model. One scanning strategy of LPF with reciprocating line and 50% overlapping rate is performed in experiments to apply laser shocks on the entire top surface of strip samples, which are prepared from glass laminate aluminum reinforced epoxy with a unidirectional orientation. Eigenstrain in the top and bottom metal layer is successively determined by the proposed analytical model and chemical etching. Finite element analysis is utilized to verify the determined eigenstrain by comparing the simulated shape with experiments and good agreement is obtained.


2018 ◽  
Vol 194 ◽  
pp. 564-574 ◽  
Author(s):  
Lu Che ◽  
Zhengong Zhou ◽  
Guodong Fang ◽  
Yunfei Ma ◽  
Wenzhe Dong ◽  
...  

2013 ◽  
Vol 7 (4) ◽  
pp. 425-438 ◽  
Author(s):  
C. Russig ◽  
M. Bambach ◽  
G. Hirt ◽  
N. Holtmann

2020 ◽  
Vol 7 (11) ◽  
pp. 116514
Author(s):  
Xiaochen Zhang ◽  
Weiying Meng ◽  
Tian Zhang ◽  
Xiao Huang ◽  
Shuai Hou

2018 ◽  
Vol 65 ◽  
pp. 301-312 ◽  
Author(s):  
Ankush P. Sharma ◽  
Sanan H. Khan ◽  
Rajesh Kitey ◽  
Venkitanarayanan Parameswaran

Scanning ◽  
2020 ◽  
Vol 2020 ◽  
pp. 1-13
Author(s):  
Xiaochen Zhang ◽  
Weiying Meng ◽  
Jiancheng Guo ◽  
Yu Zhang

Fiber metal laminates (FMLs) are a novel type of structural material that has been extensively applied in the aerospace field. These laminates are sandwich-type composite materials that comprise alternate metal and fiber-reinforced resin layers. Because of the structural characteristics of the material, it has high-impact resistance from the metal layer and increased fracture toughness and excellent fatigue and damage tolerance properties from the fiber layer. To further develop and apply this new composite material, it is essential to understand the research status on the stress analysis of each component in FMLs and the tensile strength properties of FMLs. Therefore, in this study, the current research status on the residual stress and applied stress of the component materials in FMLs and the tensile strength of the laminates is summarized. The relationship between the applied stress of each layer and the remote stress of laminates and the relationship between the tensile properties of laminates and the component material properties in laminates are clarified. Additionally, the theoretical basis and direction of development of the related models are analyzed and studied. Consequently, all of the above are aimed at laying a foundation for further investigations of the laminate theory and for the improvement of the theoretical research system.


Sign in / Sign up

Export Citation Format

Share Document