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Lamination manufacturing method for large-size and complex-structure metal components

机译:大型复杂结构金属零件的层压制造方法

摘要

A lamination manufacturing method for large-sized metal components with complicated structures is provided, relating to a part manufacturing method to solve the problem that traditional machining, entire plastic forming and the existing additive manufacturing method are difficult to manufacture large-sized metal components with complicated special-shape structure and high-performance requirement. The manufacturing method includes the steps: step 1. obtaining a three-dimensional digital model of a large-sized metal component with complicated structure, and dividing the model into a plurality of slice layers; step 2. selecting the actually available metal sheet corresponding to the thickness of each slice layer divided in step 1, and machining each metal sheet to obtain a shaped sheet consistent with the model of each slice layer in step 1; step 3. stacking the shaped sheets obtained through machining of step 2 according to the order of the corresponding slice layers in step 1; and step 4. obtaining a required large-sized metal component with complicated structure after all the shaped sheets are connected into a whole. The present invention is used for shaping large-sized components with complicated deep cavity and inner hole structures.
机译:本发明提供一种结构复杂的大型金属零件的层压制造方法,涉及一种零件制造方法,以解决传统的机加工,整体塑性成形以及现有的增材制造方法难以制造复杂的大型金属零件的问题。异型结构和高性能要求。该制造方法包括以下步骤:步骤1,获得结构复杂的大型金属零件的三维数字模型,并将该模型分为多个切片层;步骤2,选择与步骤1中划分出的各切片层的厚度相对应的实际可用的金属片,并对各金属片进行机械加工,得到与步骤1中的各切片层的模型相符的成型片。步骤3.根据步骤1中相应的切片层的顺序堆叠通过步骤2的机加工获得的成型片。步骤4,将所有成型片连接成一个整体,得到所需的结构复杂的大型金属零件。本发明用于成形具有复杂的深腔和内孔结构的大型部件。

著录项

  • 公开/公告号US10589504B2

    专利类型

  • 公开/公告日2020-03-17

    原文格式PDF

  • 申请/专利权人 HARBIN INSTITUTE OF TECHNOLOGY;

    申请/专利号US201616094626

  • 申请日2016-12-27

  • 分类号B32B3;B32B15;B32B37;B32B38;B32B37/12;B32B38/18;B32B3/26;B32B15/01;B23P15;

  • 国家 US

  • 入库时间 2022-08-21 11:30:51

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