CN206287597U - A kind of composite material structure - Google Patents
A kind of composite material structure Download PDFInfo
- Publication number
- CN206287597U CN206287597U CN201621363519.7U CN201621363519U CN206287597U CN 206287597 U CN206287597 U CN 206287597U CN 201621363519 U CN201621363519 U CN 201621363519U CN 206287597 U CN206287597 U CN 206287597U
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- Prior art keywords
- layer
- resin
- honeycomb core
- composite material
- base layer
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Abstract
The utility model discloses a kind of composite material structure, including honeycomb core, glued membrane, top panel, lower panel, base layer of resin, carbon fiber braiding layer and ceramic layer, the top of the honeycomb core is connected by glued membrane with top panel, the bottom of the honeycomb core is connected by glued membrane with lower panel, the bottom of the base layer of resin is connected with glued membrane, located at the inside of base layer of resin, the top of the base layer of resin is connected the carbon fiber braiding layer with ceramic layer.The composite material structure uses hollow honeycomb core to reach the purpose of mitigation weight on the basis of proof strength, and the ceramic layer on surface is formed by ceramic post sintering：Powder particle is continuous overall into one by mutually melting diffusion bonding, leave hole in ceramic inside, make material slimmer and more graceful, and with good anti-wear performance, carbon fiber braiding layer makes the bearing capacity of the composite material structure stronger as reinforcing material, and improves horizontal mechanical performance, compression and the cutting performance of the structure.
Description
Technical field
The utility model is related to technical field of composite materials, specially a kind of composite material structure.
Background technology
Composite, is by two or more material of different nature, by method physically or chemically, in macroscopic view
Material of the composition with new capability on (microcosmic).Various materials make up for each other's deficiencies and learn from each other in performance, produce cooperative effect, make to be combined
The combination property of material is better than former composition material and meets a variety of requirements.The matrix material of composite be divided into metal and
Nonmetallic two major class.
In the prior art, the parts in industry manufacture are generally manufactured and obtained using aluminum alloy materials, though aluminium alloy
It is so lighter than steel and alloy, but cannot still meet the light-weighted requirement of parts in industry manufacture.Nowadays there is many
Material can serve as alternative materials and come alternative metals plate, such as resin composite plates.But the rigidity of traditional resin composite plates and anti-
Tensile strength is inadequate.And it is strong in order to ensure its rigidity and stretch-proof, its weight loss effect is not again obvious.
Utility model content
The purpose of this utility model is to provide a kind of composite material structure, to solve to be proposed in above-mentioned background technology
Existing metallic composite, in intensity and lightweight urgently continue strengthen exploitation problem.
To achieve the above object, the utility model provides following technical scheme：A kind of composite material structure, including honeybee
Nest core, glued membrane, top panel, lower panel, base layer of resin, carbon fiber braiding layer and ceramic layer, the top of the honeycomb core pass through glue
Film is connected with top panel, and the bottom of the honeycomb core is connected by glued membrane with lower panel, the bottom of the base layer of resin with
Glued membrane is connected, and located at the inside of base layer of resin, the top of the base layer of resin is connected the carbon fiber braiding layer with ceramic layer
Connect.
Preferably, the top panel includes base layer of resin, carbon fiber braiding layer and ceramic layer.
Preferably, the lower panel uses alloy aluminium sheet.
Preferably, it is brought into close contact by high-temperature laminating between the base layer of resin and ceramic layer.
Preferably, the honeycomb core is made of aluminum alloy materials.
Compared with prior art, the beneficial effects of the utility model are：The composite material structure is in proof strength
On the basis of use hollow honeycomb core and mitigate to reach the purpose of weight, it is golden while using resin material as base material
Category material effectively reduce weight, the ceramic layer on surface is formed by ceramic post sintering, powder particle by mutually melting diffusion bonding into
One is continuous overall, and the advantage of this technique is that ceramics are internal leaves hole, makes material slimmer and more graceful, and with good
Anti-wear performance, carbon fiber braiding layer makes the bearing capacity of the composite material structure stronger as reinforcing material, and carries
The horizontal mechanical performance of the high structure, compression and cutting performance.
Brief description of the drawings
Fig. 1 is the utility model structural representation；
Fig. 2 is the utility model top surface plate structure schematic diagram；
Fig. 3 is the utility model carbon fiber braiding layer structural representation.
In figure：1st, honeycomb core, 2, glued membrane, 3, top panel, 4, lower panel, 5, base layer of resin, 6, carbon fiber braiding layer, 7, pottery
Enamel coating.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of the utility model protection.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme：A kind of composite material structure, including honeycomb
Core 1, glued membrane 2, top panel 3, lower panel 4, base layer of resin 5, carbon fiber braiding layer 6 and ceramic layer 7, the top of honeycomb core 1 passes through
Glued membrane 2 is connected with top panel 3, and top panel 3 includes base layer of resin 5, carbon fiber braiding layer 6 and ceramic layer 7, the bottom of honeycomb core 1
Portion is connected by glued membrane 2 with lower panel 4, and honeycomb core 1 is made of aluminum alloy materials, and cellular structure can bear high intensity
Pressure and shearing force, be unlikely to deform, lower panel 4 use alloy aluminium sheet, using aluminium alloy plate, with good intensity, and aluminium
The price of alloy material is low, more light, and the bottom of base layer of resin 5 is connected with glued membrane 2, and carbon fiber braiding layer 6 is located at resin
The inside of basic unit 5, the top of base layer of resin 5 is connected with ceramic layer 7, and space is left inside the ceramic material of ceramic layer 7, makes material
Matter is slimmer and more graceful, and ceramic material has good anti-wear performance, tight by high-temperature laminating between base layer of resin 5 and ceramic layer 7
Closely connected conjunction.
Operation principle：The composite material structure is mainly made up of honeycomb core 1, top panel 3 and lower panel 4, top panel 3
It is bonded together by glued membrane 2 and lower panel 4 and honeycomb core 1 between, honeycomb core 1 is made of aluminum alloy materials, cellular
Structure can bear the pressure and shearing force of high intensity, be unlikely to deform, and hollow structure effectively reduces the weight of material, meet
To light-weighted requirement, lower panel 4 uses alloy aluminium sheet to material, using aluminium alloy plate, with good intensity, and aluminium alloy material
The price of material is low, more light, is brought into close contact by high-temperature laminating between base layer of resin 5 and ceramic layer 7, inside base layer of resin 5
It is provided with carbon fiber braiding layer 6, the bearing capacity that carbon fiber braiding layer 6 makes the composite material structure as reinforcing material is more
By force, ceramic layer 7 is formed as surfacing by ceramic post sintering, and ceramics are internal to leave hole, makes material slimmer and more graceful, and have
Good anti-wear performance.
Although being described in detail to the utility model with reference to the foregoing embodiments, come for those skilled in the art
Say, it can still be modified to the technical scheme described in foregoing embodiments, or which part technical characteristic is entered
Row equivalent, all within spirit of the present utility model and principle, any modification, equivalent substitution and improvements made etc. all should
It is included within protection domain of the present utility model.
Claims (5)
1. a kind of composite material structure, including honeycomb core (1), glued membrane (2), top panel (3), lower panel (4), base layer of resin
(5), carbon fiber braiding layer (6) and ceramic layer (7), it is characterised in that：The top of the honeycomb core (1) by glued membrane (2) with it is upper
Panel (3) is connected, and the bottom of the honeycomb core (1) is connected by glued membrane (2) with lower panel (4), the base layer of resin (5)
Bottom be connected with glued membrane (2), the carbon fiber braiding layer (6) is located at the inside of base layer of resin (5), the base layer of resin
(5) top is connected with ceramic layer (7).
2. a kind of composite material structure according to claim 1, it is characterised in that：The top panel (3) includes tree
Aliphatic radical layer (5), carbon fiber braiding layer (6) and ceramic layer (7).
3. a kind of composite material structure according to claim 1, it is characterised in that：The lower panel (4) is using conjunction
Golden aluminium sheet.
4. a kind of composite material structure according to claim 1, it is characterised in that：The base layer of resin (5) and pottery
Enamel coating is brought into close contact between (7) by high-temperature laminating.
5. a kind of composite material structure according to claim 1, it is characterised in that：The honeycomb core (1) uses aluminium
Alloy material is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621363519.7U CN206287597U (en) | 2016-12-05 | 2016-12-05 | A kind of composite material structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621363519.7U CN206287597U (en) | 2016-12-05 | 2016-12-05 | A kind of composite material structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206287597U true CN206287597U (en) | 2017-06-30 |
Family
ID=59098304
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621363519.7U Expired - Fee Related CN206287597U (en) | 2016-12-05 | 2016-12-05 | A kind of composite material structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206287597U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109405647A (en) * | 2018-11-05 | 2019-03-01 | 中国航空制造技术研究院 | Brickwall multilayer tortoise plastron protective device and preparation method thereof |
| CN110528804A (en) * | 2019-08-23 | 2019-12-03 | 嘉兴吉象装饰建材有限公司 | High surface hardness honeycomb aluminium-plastic panel and its production technology |
-
2016
- 2016-12-05 CN CN201621363519.7U patent/CN206287597U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109405647A (en) * | 2018-11-05 | 2019-03-01 | 中国航空制造技术研究院 | Brickwall multilayer tortoise plastron protective device and preparation method thereof |
| CN110528804A (en) * | 2019-08-23 | 2019-12-03 | 嘉兴吉象装饰建材有限公司 | High surface hardness honeycomb aluminium-plastic panel and its production technology |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170630 Termination date: 20171205 |