复合材料科学与工程 ›› 2024, Vol. 0 ›› Issue (7): 70-73.DOI: 10.19936/j.cnki.2096-8000.20240728.009

• 应用研究 • 上一篇    下一篇

双曲形复合材料构件成型精度修正技术研究

刘宝明1, 罗晨2, 王小凯3, 韩志仁2,4   

  1. 1.沈阳航空航天大学 工程训练中心,沈阳 110136;
    2.沈阳航空航天大学 航空宇航学院,沈阳 110136;
    3.中航西安飞机工业(集团)有限公司,西安 710089;
    4.沈阳航空航天大学 航空制造工艺数字化国防重点学科实验室,沈阳 110136
  • 收稿日期:2023-06-28 出版日期:2024-07-28 发布日期:2024-08-08
  • 作者简介:刘宝明(1979—),男,硕士,工程师,研究方向为飞机数字化制造和复合材料成型工艺,syliubaoming@163.com。
  • 基金资助:
    国家自然科学基金(52001217)

Study on deformation correction technology of forming accuracy of hyperbolic composite components

LIU Baoming1, LUO Chen2, WANG Xiaokai3, HAN Zhiren2,4   

  1. 1. Engineering Training Center, Shenyang Aerospace University, Shenyang 110136, China;
    2. College of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China;
    3. Avic Xi'an Aircraft Industry (Group) Company Ltd., Xi'an 710089, China;
    4. Key Laboratory of Fundamental Science for National Defense of Aeronautical Digital Manufacturing Process, Shenyang Aerospace University, Shenyang 110136, China
  • Received:2023-06-28 Online:2024-07-28 Published:2024-08-08

摘要: 双曲形复合材料构件固化变形是影响零件质量和几何精度的关键问题之一,为了提高双曲形复合材料构件成型几何精度,本文提出了一种基于试验数据的变形修正方法,详细阐述了试验数据获取、去噪和数据对齐以及基于多截面的试验数据搜索法和镜像法等关键问题;并基于CATIA/CAA二次开发技术开发了修正模块,该模块能够对双曲形复合材料构件的固化变形进行有效补偿。以某机上双曲形零件为例进行试验验证,经过该模块修正后,零件的制造误差显著减小,证明了该方法的有效性和可行性。本研究结果对于提高双曲形复合材料构件的制造精度和性能具有重要意义。

关键词: 复合材料, 变形修正, CATIA二次开发, 多截面, 数据搜索, 镜像法

Abstract: Curing deformation of hyperbolic composite components was one of the key issues affecting part quality and geometric accuracy. The deformation correction method based on experimental data was proposed by this paper in order to improve the geometric accuracy of hyperbolic composite components and key issues such as experimental data acquisition, denoising and data alignment, as well as the multi-section experimental data search method and mirror method were elaborated on. A correction module was developed based on CATIA/CAA secondary development technology, which can effectively compensate for the curing deformation of hyperbolic composite components. Experimental verification was conducted using a hyperbolic part on an aircraft, and after correction by the module, the manufacturing error of the part was significantly reduced, demonstrating the effectiveness and feasibility of the method. The results of this study are of great significance for improving the manufacturing accuracy and performance of hyperbolic composite components.

Key words: composites, deformation correction, CATIA secondary development, multiple cross-sections, data searching, mirror method

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