CN206749179U - A kind of aircraft glass based on graphene - Google Patents
A kind of aircraft glass based on graphene Download PDFInfo
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- CN206749179U CN206749179U CN201720434256.2U CN201720434256U CN206749179U CN 206749179 U CN206749179 U CN 206749179U CN 201720434256 U CN201720434256 U CN 201720434256U CN 206749179 U CN206749179 U CN 206749179U
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Abstract
A kind of aircraft glass based on graphene is the utility model is related to, is tightly connected successively including inner layer glass, bearing glass and glass outer, the edge of the bearing glass and glass outer, vacuum interlayer is formed between bearing glass and glass outer；There is graphene fiber heating film and graphene heat conducting film in the vacuum interlayer；The graphene heat conducting film is laid on the inside of glass outer, and graphene fiber heating film is laid on the inside of graphene heat conducting film.The utility model is set by sandwich construction so that and aircraft glass has heating, heat conductivility in itself, effectively antifog, while on the premise of sight is not influenceed, can quickly antifog deicing.
Description
Technical field
The anti-icing field of glass product is the utility model is related to, more particularly, to a kind of aircraft glass based on graphene.
Background technology
Aircraft can be influenceed in flight course by weather environment and state of flight, on some surfaces, such as windscreen glass
There is icing frost, serious threat flight safety in the surfaces such as glass, the leading edge of a wing, air inlet road junction.Particularly windshield
Icing frost, the visual field and the visual comfort of pilot can be largely influenceed, for a long time under icing frosting state
Flight, the problems such as visual fatigue error in judgement can be caused.To improve this phenomenon, being coated with electric heating film on the inside of windshield can
Icing and frost are effectively removed, meanwhile, windshield visible light transmissivity is not influenceed, improves flight safety performance.
The anti-icing frost prevention technology of traditional windshield of aircraft using gas heat and anti-freeze fluid etc., with motor exhaust entered by gas thermal recovery
Row heating, complicated efficiency is low, and anti-freeze fluid is only limitted to the anti-icing use in ground, and the Electric heating used is simple indium oxide
Tin monofilm or resistance screen, certain limitation in electrically heated uniformity and square resistance be present, while to windshield
The miscellaneous functions such as energy-efficient performance, which have no, to be significantly improved.
The content of the invention
The purpose of this utility model be exactly in order to provided the defects of overcoming above-mentioned prior art to exist a kind of quick heating,
Quick conductive, the aircraft glass based on graphene of environmental protection and energy saving, there is the anti-icing function of quick frost prevention.
The purpose of this utility model can be achieved through the following technical solutions：A kind of aircraft glass based on graphene,
Including：Include inner layer glass, bearing glass and glass outer successively, the edge sealing of the bearing glass and glass outer connects
Connect, vacuum interlayer is formed between bearing glass and glass outer；There is graphene fiber heating film and stone in the vacuum interlayer
Black alkene heat conducting film；The graphene heat conducting film is laid on the inside of glass outer, and graphene fiber heating film is laid on graphene and led
On the inside of hotting mask.
Further, the graphene heat conducting film is transparent that its thickness is 1~1000 micron.
Further, graphene fiber heating film is made up of more graphene fibers, more graphene fiber parallel connections, with setting
The electrode slice put in internal layer Glass base is connected.
The beneficial effects of the utility model are：The utility model is set by sandwich construction so that aircraft glass is in itself
It is effectively antifog with heat conductivility, while on the premise of sight is not influenceed, there is heating function, can quick deicing.
Brief description of the drawings
Fig. 1 is the structural representation of aircraft compound glass；
In figure：Inner layer glass 1, bearing glass 2, glass outer 3, vacuum interlayer 4, graphene fiber heating film 5, graphene
Heat conducting film 6.
Embodiment
The utility model is described in detail with specific embodiment below in conjunction with the accompanying drawings.The present embodiment is with the utility model
Implemented premised on technical scheme, give detailed embodiment and specific operating process, but guarantor of the present utility model
Shield scope is not limited to following embodiments.
As shown in figure 1, the present embodiment provides a kind of aircraft compound glass based on graphene technology, there is the anti-icing work(of frost prevention
Can, there is the anti-icing function of frost prevention, successively including inner layer glass 1, bearing glass 2 and glass outer 3, the bearing glass 2 and outside
The edge of layer glass 3 is tightly connected, and vacuum interlayer 4 is formed between bearing glass 2 and glass outer 3；In the vacuum interlayer 4
With graphene fiber heating film 5 and graphene heat conducting film 6；The graphene heat conducting film 6 is laid on the inner side of glass outer 3, stone
Black alkene fiber heating film 5 is laid on the inner side of graphene heat conducting film 6.Graphene fiber heating film 5 is made up of more graphene fibers,
More graphene fiber Parallel Designs, as common technical means in the art, electrode slice can be set in internal layer Glass base,
In the case of severe cold, graphene fiber in parallel is connected by electrode slice with aircraft power supply, you can realize that graphene fiber generates heat
The heating of film 5, then heat is quickly conducted by graphene heat conducting film 6 and to whole glass, reaches the antifog effect of heating deicing.
As the common knowledge of this area, the graphene heat conducting film 6 and graphene fiber heating film 5 of use are transparent
, its thickness is 1~1000 micron.
The graphene product that the utility model is related to is the existing product of this area, such as the limited public affairs of the high alkene science and technology in Hangzhou
Department, the product of Zhejiang Tan Gushangxi materials Science and Technology Ltd..
The advantages of general principle and principal character of the present utility model and the utility model has been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification
Simply illustrate principle of the present utility model, on the premise of the spirit and scope of the utility model is not departed from, the utility model is also
Various changes and modifications are had, these changes and improvements are both fallen within claimed the scope of the utility model.The utility model
Claimed scope is by appended claims and its equivalent thereof.
Claims (3)
1. a kind of aircraft glass based on graphene, it is characterised in that successively including inner layer glass (1), bearing glass (2) and outer
The edge of layer glass (3), the bearing glass (2) and glass outer (3) is tightly connected, bearing glass (2) and glass outer
(3) vacuum interlayer (4) is formed between；There is graphene fiber heating film (5) and graphene heat conducting film in the vacuum interlayer (4)
(6)；The graphene heat conducting film (6) is laid on the inside of glass outer (3), and graphene fiber heating film (5) is laid on graphene
On the inside of heat conducting film (6).
2. aircraft glass according to claim 1, it is characterised in that the graphene heat conducting film is transparent, its thickness
For 1~1000 micron.
3. aircraft glass according to claim 1, it is characterised in that graphene fiber heating film (5) is by more graphenes
Fiber forms, and more graphene fiber parallel connections, is connected with the electrode slice for being arranged on inner layer glass bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720434256.2U CN206749179U (en) | 2017-04-24 | 2017-04-24 | A kind of aircraft glass based on graphene |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720434256.2U CN206749179U (en) | 2017-04-24 | 2017-04-24 | A kind of aircraft glass based on graphene |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206749179U true CN206749179U (en) | 2017-12-15 |
Family
ID=60614813
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720434256.2U Active CN206749179U (en) | 2017-04-24 | 2017-04-24 | A kind of aircraft glass based on graphene |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206749179U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108638807A (en) * | 2018-04-11 | 2018-10-12 | 杭州牛墨科技有限公司 | A kind of vehicle glass of the chemical deicing quick-drying based on few layer graphene |
| CN109195236A (en) * | 2018-11-05 | 2019-01-11 | 厦门信果石墨烯科技有限公司 | A kind of graphene fever power generating glass and its manufacturing method |
-
2017
- 2017-04-24 CN CN201720434256.2U patent/CN206749179U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108638807A (en) * | 2018-04-11 | 2018-10-12 | 杭州牛墨科技有限公司 | A kind of vehicle glass of the chemical deicing quick-drying based on few layer graphene |
| CN109195236A (en) * | 2018-11-05 | 2019-01-11 | 厦门信果石墨烯科技有限公司 | A kind of graphene fever power generating glass and its manufacturing method |
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