CN106476302A - The manufacture method of complex fiber material shell - Google Patents
The manufacture method of complex fiber material shell Download PDFInfo
- Publication number
- CN106476302A CN106476302A CN201510553200.4A CN201510553200A CN106476302A CN 106476302 A CN106476302 A CN 106476302A CN 201510553200 A CN201510553200 A CN 201510553200A CN 106476302 A CN106476302 A CN 106476302A
- Authority
- CN
- China
- Prior art keywords
- mother metal
- cut
- laminated
- cotton cloth
- weaved cotton
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
Abstract
A kind of manufacture method of complex fiber material shell, comprising a previous step, a forming step, and a cutting step.In the previous step, multiple prepreg composite materials are weaved cotton cloth and is laminated for a mother metal.Multiple prepreg composite materials of the area less than the vertical mother metal of the mother metal and fiber directionality are weaved cotton cloth and are laminated for a Rankine.The Rankine is overlapping on the mother metal, forms the thicker workpiece to be laminated in a part.In the forming step, the workpiece to be laminated is carried out hot pressing to be shaped to a cut piece to be cut.In the cutting step, multiple key position holes are cut out in the cut piece to be cut and seat is set so that a keyboard is obtained.By stiffener vertical with mother metal for fiber directionality is overlapping on mother metal, make the keyboard made arrange seat key-position area structural strength higher, lift consumer's purchase intention.
Description
Technical field
The present invention relates to a kind of manufacture method of shell, particularly relates to outside a kind of complex fiber material
The manufacture method of shell.
Background technology
The casing of general notebook computer is can to open ground pivot joint bottom by a base and one
The upper lid composition of seat.And the base contains a underlying drain pan, and one can be with this
Drain pan pairing and be available for keycap protrude from its surface keyboard arrange seat.Current main flow still with
The mode that plastic cement is projected molds the keyboard and arranges seat, although the technology that plastic cement is projected is more ripe
And plastic go out the more complicated external form of configuration, but the texture of plastic cement is still cheap and not beautiful to consumer
The impression of sight.
And although the keyboard gone out with carbon fiber forming is arranged seat and has preferably matter with respect to plastic cement
Sense, but opened up multiple compact arranged key position holes thereon, reduce and open up out the grade key position hole
Region structural strength, and the typewriting power of user need to be often born in this region, if knot
Structure intensity deficiency certainly will affect the purchase intention of consumer.
Content of the invention
It is an object of the invention to provide outside a kind of higher complex fiber material of key-position area intensity
The manufacture method of shell.
The manufacture method of complex fiber material shell of the present invention, it is characterised in that:The manufacture method
Comprising a previous step, a forming step, and a cutting step;In the previous step
In, multiple prepreg composite materials are weaved cotton cloth and are laminated for a mother metal, by area less than the mother metal and
Multiple prepreg composite materials of the vertical mother metal of fiber directionality are weaved cotton cloth and are laminated for a Rankine,
The Rankine is overlapping on the mother metal, forms the thicker workpiece to be laminated in a part;At this
In forming step, the workpiece to be laminated is placed in the middle of a mould, the mould includes public affairs
Mould, and a master mold that can be matched with the male model, are then carried out hot pressing, this are waited to press
Conjunction Workpiece shaping is a cut piece to be cut, and the cut piece to be cut has the thicker thickening of a thickness
Area;In the cutting step, multiple key position holes are cut out on the thickened area of the cut piece to be cut,
Seat is set so that a keyboard is obtained, the keyboard arranges seat comprising the thicker key-position area of a thickness,
And multiple key position holes being formed on the key-position area.
It is preferred that in the manufacture method of aforementioned complex fiber material shell, the wherein previous step
Prepreg composite materials to weave cotton cloth knitted selected from carbon-fiber cloth, fiberglass woven cloth, aramid fiber
Cloth, basalt fibre are weaved cotton cloth, and boron fibre is weaved cotton cloth.
The beneficial effects of the present invention is:By by stiffener vertical with mother metal for fiber directionality
Be overlapping on mother metal, make the keyboard made arrange seat key-position area structural strength higher, lifting disappears
The purchase intention of the person of expense.
Description of the drawings
Fig. 1 is a schematic diagram, and the manufacture method of complex fiber material shell of the present invention is described
One previous step;
Fig. 2 is a schematic diagram, and the manufacture method of complex fiber material shell of the present invention is described
One forming step;And
Fig. 3 is a schematic diagram, and the manufacture method of complex fiber material shell of the present invention is described
One cutting step.
Specific embodiment
Below in conjunction with the accompanying drawings and embodiment the present invention is described in detail.
One embodiment of the manufacture method of complex fiber material shell of the present invention is comprising before one
Put step, a forming step, and a cutting step.
Refering to Fig. 1, in the previous step, first prepare two groups of different preimpregnation composite woods of area
Material is weaved cotton cloth, and these prepreg composite materials weave cotton cloth be selected from carbon-fiber cloth, fiberglass woven cloth,
Aramid fiber is weaved cotton cloth, basalt fibre is weaved cotton cloth, and boron fibre is weaved cotton cloth.Then area is larger
One group of multiple prepreg composite materials is weaved cotton cloth and is laminated for a mother metal 11, and area is less more than another group
Individual prepreg composite materials are weaved cotton cloth and are laminated for a Rankine 12.The Rankine 12 is overlapping in this
The thicker workpiece to be laminated 2 in a part, and the Rankine 12 and the mother is formed on mother metal 11
The fiber directionality of material 11 is to be mutually perpendicular to.
Refering to Fig. 2, in the forming step, prepare a mould 3, the mould 3 includes one
Individual male model 31, and a master mold 32 that can coordinate with the male model 31.By the workpiece to be laminated 2
Be placed in the mould 3 and carry out hot pressing, by hot-forming for the workpiece to be laminated 2 be one
Cut piece to be cut 4, the cut piece to be cut 4 have the thicker thickened area 41 of a thickness.Need especially
Illustrate, weaved cotton cloth according to prepreg composite materials be selected from carbon-fiber cloth, fiberglass woven cloth,
Aramid fiber is weaved cotton cloth, basalt fibre is weaved cotton cloth, or boron fibre is weaved cotton cloth, the pressure of its hot pressing,
Temperature, and to have an institute different the time, but here is not added to repeat.
Refering to Fig. 3, in the cutting step, cut on the thickened area 41 of the cut piece to be cut 4
Go out multiple key position holes 52, seat 5 is set so that a keyboard is obtained.The keyboard arranges seat 5 and includes one
The thicker key-position area 51 of individual thickness, and multiple key position holes 52 being formed on the key-position area 51.
In sum, by the mother metal 11 superimposition fiber directionality vertical with the mother metal 11
Rankine 12, it is strong that the key-position area 51 that the keyboard that forms out can be made to arrange seat 5 increases structure
Degree, 51 thickness of key-position area is thicker in addition, and then can improve structural strength further, with
While fibrous composite is integrally formed and increases texture, the strong of key-position area 51 can be also taken into account
Spend so that the typewriting power of user is born, therefore the purpose of the present invention can be reached really.
Claims (2)
1. a kind of manufacture method of complex fiber material shell, it is characterised in that:The manufacture
Method includes previous step, a forming step, and a cutting step;Before this
Put in step, multiple prepreg composite materials are weaved cotton cloth a mother metal is laminated for, area is less than
Multiple prepreg composite materials of the mother metal and the vertical mother metal of fiber directionality are weaved cotton cloth and are laminated for one
Individual Rankine, the Rankine is overlapping on the mother metal, and what one part of formation was thicker waits to press
Close workpiece;In the forming step, the workpiece to be laminated is placed in the middle of a mould, should
Mould includes a male model, and a master mold that can be matched with the male model, then carries out heat
Pressing, so that by the Workpiece shaping to be laminated as a cut piece to be cut, the cut piece to be cut has one
The thicker thickened area of individual thickness;In the cutting step, on the thickened area of the cut piece to be cut
Multiple key position holes are cut out, seat is set so that a keyboard is obtained, the keyboard arranges seat and includes one
The thicker key-position area of individual thickness, and multiple key position holes being formed on the key-position area.
2. the manufacture method of complex fiber material shell according to claim 1, its feature
It is:Prepreg composite materials in the previous step weave cotton cloth be selected from carbon-fiber cloth, glass
Fiber weaving cloth, aramid fiber are weaved cotton cloth, basalt fibre is weaved cotton cloth, and boron fibre is weaved cotton cloth.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510553200.4A CN106476302A (en) | 2015-09-02 | 2015-09-02 | The manufacture method of complex fiber material shell |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510553200.4A CN106476302A (en) | 2015-09-02 | 2015-09-02 | The manufacture method of complex fiber material shell |
Publications (1)
Publication Number | Publication Date |
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CN106476302A true CN106476302A (en) | 2017-03-08 |
Family
ID=58237855
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510553200.4A Pending CN106476302A (en) | 2015-09-02 | 2015-09-02 | The manufacture method of complex fiber material shell |
Country Status (1)
Country | Link |
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CN (1) | CN106476302A (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1955583B2 (en) * | 1969-11-05 | 1974-12-05 | Olympia Werke Ag, 2940 Wilhelmshaven | Method of making an elastically deformable cover |
CN103177895A (en) * | 2011-12-22 | 2013-06-26 | 明安国际企业股份有限公司 | Composite reinforced casing |
CN103802323A (en) * | 2012-11-07 | 2014-05-21 | 联想(北京)有限公司 | Method used for preparing keyboard, and keyboard |
CN104057623A (en) * | 2013-03-18 | 2014-09-24 | 汉达精密电子(昆山)有限公司 | Computer housing manufacturing method and product thereof |
-
2015
- 2015-09-02 CN CN201510553200.4A patent/CN106476302A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1955583B2 (en) * | 1969-11-05 | 1974-12-05 | Olympia Werke Ag, 2940 Wilhelmshaven | Method of making an elastically deformable cover |
CN103177895A (en) * | 2011-12-22 | 2013-06-26 | 明安国际企业股份有限公司 | Composite reinforced casing |
CN103802323A (en) * | 2012-11-07 | 2014-05-21 | 联想(北京)有限公司 | Method used for preparing keyboard, and keyboard |
CN104057623A (en) * | 2013-03-18 | 2014-09-24 | 汉达精密电子(昆山)有限公司 | Computer housing manufacturing method and product thereof |
Non-Patent Citations (2)
Title |
---|
何红媛等: "《材料成型技术基础》", 31 January 2015, 东南大学出版社 * |
薛红前: "《飞机装配工艺学》", 31 March 2015, 西北工业大学出版社 * |
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Application publication date: 20170308 |