CN104668893A - Lattice material processing flow - Google Patents
Lattice material processing flow Download PDFInfo
- Publication number
- CN104668893A CN104668893A CN201310634526.0A CN201310634526A CN104668893A CN 104668893 A CN104668893 A CN 104668893A CN 201310634526 A CN201310634526 A CN 201310634526A CN 104668893 A CN104668893 A CN 104668893A
- Authority
- CN
- China
- Prior art keywords
- dot matrix
- truss structure
- lattice material
- aluminum alloy
- alloy plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Punching Or Piercing (AREA)
Abstract
The invention relates to a processing flow, in particular to a lattice material processing flow. The lattice material processing flow includes steps of material selecting, blanking, stamping forming, finishing, cleaning, drying, inspecting and packaging. The lattice material processing flow is simple in steps and convenient to operate, and the processed lattice material is high in quality.
Description
Technical field
The present invention relates to a kind of processing process, especially a kind of processing process of lattice material.
Background technology
Owing to having high-strength light, lattice material meaning is applied in space flight and satellite structure as structure.The research and development of lattice material was less than 20 years.The result of initial research mainly concentrates on the aspect such as topological characteristic, manufacturing process, Elasticity behavior, plastic yielding feature, structure multifunctional exploitation of lattice material.
Summary of the invention
The present invention is intended to study the manufacturing process of lattice material, and provide a kind of processing process of lattice material, be a kind of processing process of high-quality, its step is simple, easy to operate, can the lattice material of production high-quality, and its technical scheme adopted is as follows:
A processing process for lattice material, its step is followed successively by:
A) selection: material selection 5052 aluminum alloy plate materials;
B) blanking: by above-mentioned aluminum alloy plate materials, size is cut on request;
C) stamping: first laminboard layer aluminum alloy plate materials to be processed into the thin plate with hexagonal hole, then hole plate to be put into jet-bedding, obtain dot matrix truss structure through stamping;
D) repair: dot matrix truss structure is repaired, revise distortion, remove burr;
E) clean: pickling is carried out to dot matrix truss structure, removes surface impurity and greasy dirt;
F) dry: dot matrix truss structure is put into drying oven and dries, in drying oven, adopt nitrogen protection;
G) check: test to welding product, it is qualified to check whether;
H) pack: product is packed on request, puts in storage.
Tool of the present invention has the following advantages: step is simple, easy to operate, is the processing process of the lattice material of a high-quality.
Accompanying drawing explanation
Fig. 1: processing process figure of the present invention;
Detailed description of the invention
Below in conjunction with accompanying drawing and example, the invention will be further described, is easier to it will be appreciated by those skilled in the art that thus makes more explicit defining to protection scope of the present invention to make advantages and features of the invention.
A kind of step of processing process of lattice material is followed successively by:
A) selection: material selection 5052 aluminum alloy plate materials;
B) blanking: by above-mentioned aluminum alloy plate materials, size is cut on request;
C) stamping: first laminboard layer aluminum alloy plate materials to be processed into the thin plate with hexagonal hole, then hole plate to be put into jet-bedding, obtain dot matrix truss structure through stamping;
D) repair: dot matrix truss structure is repaired, revise distortion, remove burr;
E) clean: pickling is carried out to dot matrix truss structure, removes surface impurity and greasy dirt;
F) dry: dot matrix truss structure is put into drying oven and dries, in drying oven, adopt nitrogen protection;
G) check: test to welding product, it is qualified to check whether;
H) pack: product is packed on request, puts in storage.
Describe the present invention by way of example above, but the invention is not restricted to above-mentioned specific embodiment, all any changes of doing based on the present invention or modification all belong to the scope of protection of present invention.
Claims (1)
1. a processing process for lattice material, is characterized in that, the step of described processing process is followed successively by:
A) selection: material selection 5052 aluminum alloy plate materials;
B) blanking: by above-mentioned aluminum alloy plate materials, size is cut on request;
C) stamping: first laminboard layer aluminum alloy plate materials to be processed into the thin plate with hexagonal hole, then hole plate to be put into jet-bedding, obtain dot matrix truss structure through stamping;
D) repair: dot matrix truss structure is repaired, revise distortion, remove burr;
E) clean: pickling is carried out to dot matrix truss structure, removes surface impurity and greasy dirt;
F) dry: dot matrix truss structure is put into drying oven and dries, in drying oven, adopt nitrogen protection;
G) check: test to welding product, it is qualified to check whether;
H) pack: product is packed on request, puts in storage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310634526.0A CN104668893A (en) | 2013-12-02 | 2013-12-02 | Lattice material processing flow |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310634526.0A CN104668893A (en) | 2013-12-02 | 2013-12-02 | Lattice material processing flow |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104668893A true CN104668893A (en) | 2015-06-03 |
Family
ID=53304756
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310634526.0A Pending CN104668893A (en) | 2013-12-02 | 2013-12-02 | Lattice material processing flow |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104668893A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106124327A (en) * | 2016-06-13 | 2016-11-16 | 中国科学院力学研究所 | A kind of metal lattice sandwich plate containing Embedded defect and mechanical property test method thereof |
| CN106216496A (en) * | 2016-08-05 | 2016-12-14 | 宁波金特信钢铁科技有限公司 | A kind of preparation method of high-strength light dot matrix metal material |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060236545A1 (en) * | 2003-08-13 | 2006-10-26 | Technische Universitat Dresden | Method for producing internally or externally profiled rings and arrangement therefor |
| CN101195197A (en) * | 2007-12-18 | 2008-06-11 | 西安交通大学 | Honeycomb ring shaped dot matrix shaping method |
| CN102390011A (en) * | 2011-08-02 | 2012-03-28 | 罗键 | Integrated near-net-shape forming processing and manufacturing method for honeycomb runner cold plate |
| CN102990300A (en) * | 2012-11-21 | 2013-03-27 | 中国航空工业集团公司北京航空制造工程研究所 | Preparation method of titanium alloy three-dimensional lattice sandwich structure |
| CN102990299A (en) * | 2012-11-21 | 2013-03-27 | 中国航空工业集团公司北京航空制造工程研究所 | Preparation method for X-type titanium alloy three-dimensional lattice sandwich structure |
-
2013
- 2013-12-02 CN CN201310634526.0A patent/CN104668893A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060236545A1 (en) * | 2003-08-13 | 2006-10-26 | Technische Universitat Dresden | Method for producing internally or externally profiled rings and arrangement therefor |
| CN101195197A (en) * | 2007-12-18 | 2008-06-11 | 西安交通大学 | Honeycomb ring shaped dot matrix shaping method |
| CN102390011A (en) * | 2011-08-02 | 2012-03-28 | 罗键 | Integrated near-net-shape forming processing and manufacturing method for honeycomb runner cold plate |
| CN102990300A (en) * | 2012-11-21 | 2013-03-27 | 中国航空工业集团公司北京航空制造工程研究所 | Preparation method of titanium alloy three-dimensional lattice sandwich structure |
| CN102990299A (en) * | 2012-11-21 | 2013-03-27 | 中国航空工业集团公司北京航空制造工程研究所 | Preparation method for X-type titanium alloy three-dimensional lattice sandwich structure |
Non-Patent Citations (1)
| Title |
|---|
| 曾嵩等: "金属点阵材料的研究进展", 《材料导报A》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106124327A (en) * | 2016-06-13 | 2016-11-16 | 中国科学院力学研究所 | A kind of metal lattice sandwich plate containing Embedded defect and mechanical property test method thereof |
| CN106216496A (en) * | 2016-08-05 | 2016-12-14 | 宁波金特信钢铁科技有限公司 | A kind of preparation method of high-strength light dot matrix metal material |
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Legal Events
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150603 |
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| WD01 | Invention patent application deemed withdrawn after publication |