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    • Deformation Control of Laser Forming Connection of Thin-walled Structure Based on Temperature Difference Tensile Method

    • In the field of achieving lightweight and efficient indicators in modern aircraft, experts have studied the deformation control technology of TA15 thin-walled structure laser forming connection. The temperature difference stretching method is used to effectively suppress deformation and provide a solution for the integration of aircraft structures.
    • Vol. 45, Issue 10, Pages: 1491-1495(2025)   

      Received:19 October 2024

      Revised:2024-11-26

      Accepted:02 December 2024

      Published:20 October 2025

    • DOI: 10.15980/j.tzzz.T20240421     

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  • XUAN M H,WU B,WANG F Y,et al. Deformation control of laser forming connection of thin-walled structure based on temperature difference tensile method[J]. Special Casting & Nonferrous Alloys,2025,45(10):1 491-1 495. DOI: 10.15980/j.tzzz.T20240421.
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相关作者

Niu Jianping 中国航发西安航空发动机有限公司
Yin Dongmei 中国航发西安航空发动机有限公司
Wang Lin 中国航发西安航空发动机有限公司
Yong Kunxuan 中国航发西安航空发动机有限公司

相关机构

AECC Xi’an Aero-Engine Co.,Ltd.
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