Research on Machining Deformation of 7050 Aluminum Alloy Aircraft Rib Forging

Author:

Liu Yaoqiong,Gong Hai,He Yongbiao,Zhang Tao,Sun Yanjie,Liu Xiaolong

Funder

national natural science foundation of china

state key laboratory of high performance complex manufacturing

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering

Reference23 articles.

1. Branco, R., Costa, J. D., Borrego, L. P., Wu, S. C., Long, X. Y., & Antunes, F. V. (2020). Effect of tensile pre-strain on low-cycle fatigue behaviour of 7050–T6 aluminium alloy. Engineering Failure Analysis, 114, 104592.

2. Miller, W. S., Zhuang, L., Bottema, J., et al. (2000). Recent development in aluminium alloys for the automotive industry. Materials Science and Engineering A-Structural Materials Properties Microstructural And Processing, 280(1), 37–49.

3. Ma, H. (2010). Study on distrotion control technology for aero structure based on slotting method. Nanjing University of Aeronautics and Astronautics.

4. Han, S., Yinfei, Y., Bo, C., & Xiaowei, Z. (2016). Evaluation of residual stress in depth profile of 7055-T7751 pre-stretched aluminum alloy plate. Machine Building & Automation, 45(1), 18–21.

5. Nervi, S. (2005). A mathematical model for the estimation of the effects of residual stresses in aluminum plates. Washington University.

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