CN205149063U - Carbon fiber flat structure spare - Google Patents

Carbon fiber flat structure spare Download PDF

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Publication number
CN205149063U
CN205149063U CN201520865721.9U CN201520865721U CN205149063U CN 205149063 U CN205149063 U CN 205149063U CN 201520865721 U CN201520865721 U CN 201520865721U CN 205149063 U CN205149063 U CN 205149063U
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China
Prior art keywords
carbon fiber
slab construction
construction part
layer
sides
Prior art date
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Active
Application number
CN201520865721.9U
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Chinese (zh)
Inventor
路强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Anhui jialiqi Advanced Composite Technology Co.,Ltd.
Original Assignee
Anhui Jialiqi Aerospace Carbon Fiber Co Ltd
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Application filed by Anhui Jialiqi Aerospace Carbon Fiber Co Ltd filed Critical Anhui Jialiqi Aerospace Carbon Fiber Co Ltd
Priority to CN201520865721.9U priority Critical patent/CN205149063U/en
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Publication of CN205149063U publication Critical patent/CN205149063U/en
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Abstract

The utility model provides a carbon fiber flat structure spare, carbon fiber flat structure spare includes a plurality of layers of carbon fiber composite bed according to different angle layings, the outmost first layer that is respectively of the both sides of flat structure spare, the carbon fiber composite bed that is located flat structure spare center is the intermediate level, a plurality of layers of carbon fiber composite bed are by well mind -set both sides, the first layer of both sides and the 8th layer laying angle are 45 and 90 respectively. Compared with the prior art, it can guarantee from middle laying mode to the bilateral symmetry that performances such as plate top and bottom intensity, temper are unanimous, and the range of application is wider.

Description

A kind of carbon fiber slab construction part
Technical field
The utility model relates to carbon fibre material technical field, specifically a kind of carbon fiber planar plate members.
Background technology
Carbon fiber is a kind of fibrous carbon material.It is the micro crystal graphite material obtained through carbonization and graphitization processing by organic fiber, carbon fibre composite has the advantages such as high strength, high temperature resistant, corrosion-resistant, proportion is little, instead of a lot of traditional material, be widely used in various field, as rocket, aircraft, vehicle, apparatus, weaving, medical domain etc.
Apart from the previously described advantages, carbon fibre composite has stronger adsorption capacity, at present at house ornamentation and other furnishing fields, applies comparatively extensive.During house ornamentation, easily produce a large amount of formaldehyde, formaldehyde is larger to person injury.So most people, when selecting finishing material, pays much attention to the content of formaldehyde of finishing material.After having fitted up, also can place the article a bit with formaldehyde adsorption function at home, as active carbon etc.
Along with the generation of carbon fibre composite, also having stronger adsorption capacity while itself comparing environmental protection, is the good material of house ornamentation first-selection.But the thickness of the panel of house ornamentation is not easily blocked up, but intensity and toughness need again to reach certain requirement, so require just higher to the sheet material that carbon fibre composite is made into.
Carbon fiber sheet, in manufacturing process, can adopt the laying mode of different angles to make, reach maximum intensity and toughness to realize the thinnest thickness.At present, most manufacturer adopts asymmetrical laying mode, the plate that this laying mode is produced, and above and below intensity is different with toughness, has limitation during use.
Utility model content
The purpose of this utility model is to solve the defect that in prior art, carbon fiber plate above and below intensity is different with toughness, provides a kind of carbon fiber slab construction part to solve the problems referred to above.
The utility model is achieved through the following technical solutions above-mentioned technical purpose:
A kind of carbon fiber slab construction part, described carbon fiber slab construction part comprises some layers of carbon fiber composite bed; Every layer of carbon fiber composite bed is according to different angles laying; Described slab construction part is from thickness direction, and carbon fiber composite bed is from two side direction Central Symmetry layings; Wherein, from both sides to center, the laying angle of the ground floor of both sides and the 8th layer is respectively 45 ° and 90 °.
Preferably, the thickness of described carbon fiber slab construction part is 2mm.
Preferably, described carbon fiber slab construction part comprises 16 layers of carbon fiber composite bed.
Preferably, the thickness of described every layer of carbon fiber composite bed is 0.125mm.
Preferably, described carbon fibre composite is prepreg.
Preferably, described prepreg is unidirectional pre-immersion material.
Preferably, on the thickness direction of described carbon fiber slab construction part, from both sides to center, the laying angle of the layer 5 of both sides is 45 °.
Preferably, on the thickness direction of described carbon fiber slab construction part, from both sides to center, the second layer of both sides and the laying angle of layer 6 are 0 °.
Preferably, on the thickness direction of described carbon fiber slab construction part, from both sides to center, the third layer of both sides and the laying angle of layer 7 are-45 °.
Preferably, on the thickness direction of described carbon fiber slab construction part, from both sides to center, the laying angle of the 4th layer of both sides is 90 °.
The utility model compared with prior art, has the following advantages:
The carbon fiber slab construction part that the utility model provides comprises 16 layers of carbon fiber composite bed, and the thickness of every layer of carbon fiber composite bed is 0.125mm.The gross thickness of plate is 2mm.The design of thickness like this and the number of plies not only meets plate intensity, meanwhile, in turn ensure that the toughness of plate.
And it is certainly middle to monosymmetric laying mode, can ensure that the performances such as plate top and bottom intensity, toughness are consistent.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of a kind of carbon fiber slab construction of the utility model part;
Fig. 2 is the hierarchy schematic diagram of a kind of carbon fiber slab construction of the utility model part.
Detailed description of the invention
For making to have a better understanding and awareness architectural feature of the present utility model and effect of reaching, coordinating detailed description in order to preferred embodiment and accompanying drawing, being described as follows:
As shown in Figure 1, a kind of carbon fiber slab construction part, carbon fiber slab construction part comprises some layers of carbon fiber composite bed; Every layer of carbon fiber composite bed is according to different angles laying; Slab construction part is from thickness direction, and carbon fiber composite bed is from two side direction Central Symmetry layings.Both sides outermost layer is ground floor, and the carbon fiber composite bed be in the middle of slab construction part is intermediate layer.
The carbon fiber slab construction part that the utility model provides comprises 16 layers of carbon fiber composite bed, and the thickness of every layer of carbon fiber composite bed is 0.125mm.The gross thickness of plate is 2mm.The design of thickness like this and the number of plies not only meets plate intensity, meanwhile, in turn ensure that the toughness of plate.
The carbon fibre composite that the utility model provides is unidirectional pre-immersion material.
The carbon fiber plate employing that the utility model provides, is specially to the technique of bilateral symmetry laying from center:
As shown in Figure 2, in the thickness direction thereof, from both sides to center, the ground floor 1 of both sides and the laying angle of layer 55 are 45 ° to carbon fiber slab construction part; From both sides to center, the second layer 2 of both sides and the laying angle of layer 66 are 0 °; From both sides to center, the third layer 3 of both sides and the laying angle of layer 77 are-45 °; From both sides to center, the laying angle of the 4th layer 4 of both sides and the 8th layer 8 is 90 °.
The carbon fiber plate of 2mm thickness, from middle to monosymmetric laying mode, can ensure that the performances such as plate top and bottom intensity, toughness are consistent.
More than show and describe general principle of the present utility model, principal character and advantage of the present utility model.The technical staff of the industry should understand; the utility model is not restricted to the described embodiments; the just principle of the present utility model described in above-described embodiment and description; under the prerequisite not departing from the utility model spirit and scope, the utility model also has various changes and modifications, and these changes and improvements all fall in claimed scope of the present utility model.The protection domain that the utility model requires is defined by appending claims and equivalent thereof.

Claims (10)

1. a carbon fiber slab construction part, is characterized in that: described carbon fiber slab construction part comprises the some layers of carbon fiber composite bed according to different angles laying; The outermost layer of the both sides of described slab construction part is respectively ground floor, and the carbon fiber composite bed being positioned at slab construction part center is intermediate layer; Described some layers of carbon fiber composite bed by center to both sides; The laying angle of the ground floor of both sides and the 8th layer is respectively 45 ° and 90 °.
2. a kind of carbon fiber slab construction part according to claim 1, is characterized in that: the thickness of described carbon fiber slab construction part is 2mm.
3. a kind of carbon fiber slab construction part according to claim 1, is characterized in that: described carbon fiber slab construction part comprises 16 layers of carbon fiber composite bed.
4. a kind of carbon fiber slab construction part according to claim 3, is characterized in that: the thickness of described every layer of carbon fiber composite bed is 0.125mm.
5. a kind of carbon fiber slab construction part according to claim 1, is characterized in that: the material of described carbon fiber composite bed is prepreg.
6. a kind of carbon fiber slab construction part according to claim 5, is characterized in that: described prepreg is unidirectional pre-immersion material.
7. a kind of carbon fiber slab construction part according to claim 3, is characterized in that: the laying angle of the layer 5 of described carbon fiber slab construction part both sides is 45 °.
8. a kind of carbon fiber slab construction part according to claim 3, is characterized in that: the described second layer of carbon fiber slab construction part both sides and the laying angle of layer 6 are 0 °.
9. a kind of carbon fiber slab construction part according to claim 3, is characterized in that: the described third layer of carbon fiber slab construction part both sides and the laying angle of layer 7 are-45 °.
10. a kind of carbon fiber slab construction part according to claim 3, is characterized in that: the laying angle of the 4th layer, described carbon fiber slab construction part both sides is 90 °.
CN201520865721.9U 2015-10-30 2015-10-30 Carbon fiber flat structure spare Active CN205149063U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520865721.9U CN205149063U (en) 2015-10-30 2015-10-30 Carbon fiber flat structure spare

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520865721.9U CN205149063U (en) 2015-10-30 2015-10-30 Carbon fiber flat structure spare

Publications (1)

Publication Number Publication Date
CN205149063U true CN205149063U (en) 2016-04-13

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CN201520865721.9U Active CN205149063U (en) 2015-10-30 2015-10-30 Carbon fiber flat structure spare

Country Status (1)

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CN (1) CN205149063U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105252842A (en) * 2015-10-30 2016-01-20 安徽佳力奇航天碳纤维有限公司 Carbon fiber flat structural member

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105252842A (en) * 2015-10-30 2016-01-20 安徽佳力奇航天碳纤维有限公司 Carbon fiber flat structural member

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Legal Events

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C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 234000 Chaoyang Road 169, Suzhou High-tech Industrial Park, Anhui Province

Patentee after: Anhui jialiqi Carbon Fiber Technology Co Ltd

Address before: 234000 Chaoyang Road 169, Suzhou High-tech Industrial Park, Anhui Province

Patentee before: ANHUI JIALIQI AEROSPACE CARBON FIBER CO., LTD.

CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 234000 Chaoyang Road 169, Suzhou High-tech Industrial Park, Anhui Province

Patentee after: Anhui jialiqi Advanced Composite Technology Co.,Ltd.

Address before: 234000 Chaoyang Road 169, Suzhou High-tech Industrial Park, Anhui Province

Patentee before: ANHUI JIALIQI AEROSPACE CARBON FIBER Co.,Ltd.