Method for manufacturing metallic object in which additive manufacturing and plastic deformation are employed in combination
US-2016339522-A1 · Nov 24, 2016 · US
US12447529B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12447529-B2 |
| Application number | US-202118247951-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 15, 2021 |
| Priority date | Oct 15, 2020 |
| Publication date | Oct 21, 2025 |
| Grant date | Oct 21, 2025 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
The present invention relates to a method for manufacturing a heterogeneous composite material thin plate and a heterogeneous composite material thin plate manufactured by same, the method comprising the steps of: (a) ball-milling an aluminum or aluminum alloy powder and a carbon nanotube powder so as to prepare a composite powder; (b) preparing a multi-layered billet comprising the composite powder, the multi-layered billet characterized by comprising a core layer and two or more shell layers surrounding the core layer, wherein the core layer is made of the composite powder or an aluminum alloy, the shell layers excluding the outermost shell layer are made of the composite powder, and the outermost shell layer is made of (i) an aluminum or aluminum alloy powder or (ii) the composite powder; and (c) rolling the multi-layered billet so as to form a thin plate shape.
Opening claim text (preview).
The invention claimed is: 1. A method of manufacturing a heterogeneous composite material thin plate, the method comprising: (a) preparing a composite powder by ball-milling an aluminum or aluminum alloy powder and a carbon nanotube powder; (b) manufacturing a multilayer billet containing the composite powder and comprising a core layer and two or more shell layers surrounding the core layer, wherein the core layer is made of the composite powder or an aluminum alloy, each of the shell layers excluding the outermost shell layer is made of the composite powder, and the outermost shell layer is made of (i) an aluminum or aluminum alloy powder or (ii) the composite powder; and (c) shaping the multilayer billet into a thin plate by rolling. 2. The method of claim 1 , wherein the core layer is made of the composite powder, and the respective composite powders comprised in the core layer and each of the shell layers excluding the outermost shell layer differ in composition. 3. The method of claim 1 , wherein the multilayer billet comprises: the core layer; a first shell layer surrounding the core layer; and a second shell layer surrounding the first shell layer. 4. The method of claim 3 , wherein the multilayer billet comprises: a can-shaped first billet serving as the second shell layer; a second billet placed in the first billet and serving as the first shell layer; and a third billet placed in the second billet and serving as the core layer. 5. The method of claim 1 , wherein in the (b) manufacturing, the multilayer billet is subjected to spark plasma sintering under conditions: a temperature in a range of 280° C. to 600° C., a pressure in a range of 30 MPa to 100 MPa, and a duration in a range of 1 second to 30 minutes. 6. A heterogeneous composite material thin plate manufactured by the method of claim 1 .
Processes characterised by the sequence of their steps · CPC title
Micron size particles, i.e. above 1 micrometer up to 500 micrometer · CPC title
Carbon nanotube · CPC title
Aluminium · CPC title
Use of plasma · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.