The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 17, 2020

Filed:

Dec. 27, 2016
Applicant:

Harbin Institute of Technology, Harbin, CN;

Inventors:

Zhubin He, Harbin, CN;

Kun Zhang, Harbin, CN;

Haihui Zhu, Harbin, CN;

Shijian Yuan, Harbin, CN;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B32B 3/00 (2006.01); B32B 15/00 (2006.01); B32B 37/00 (2006.01); B32B 38/00 (2006.01); B32B 37/12 (2006.01); B32B 38/18 (2006.01); B32B 3/26 (2006.01); B32B 15/01 (2006.01); B23P 15/00 (2006.01);
U.S. Cl.
CPC ...
B32B 38/0004 (2013.01); B23P 15/00 (2013.01); B32B 3/266 (2013.01); B32B 15/01 (2013.01); B32B 37/12 (2013.01); B32B 38/0012 (2013.01); B32B 38/1841 (2013.01); B23P 2700/12 (2013.01);
Abstract

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.


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