CN108485205A - A kind of unmanned plane case material formula of lightweight - Google Patents
A kind of unmanned plane case material formula of lightweight Download PDFInfo
- Publication number
- CN108485205A CN108485205A CN201810498628.7A CN201810498628A CN108485205A CN 108485205 A CN108485205 A CN 108485205A CN 201810498628 A CN201810498628 A CN 201810498628A CN 108485205 A CN108485205 A CN 108485205A
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- China
- Prior art keywords
- parts
- unmanned plane
- lightweight
- epoxy resin
- case material
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- 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.)
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
- C08L63/04—Epoxynovolacs
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/02—Elements
- C08K3/08—Metals
- C08K2003/0881—Titanium
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K2201/00—Specific properties of additives
- C08K2201/011—Nanostructured additives
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/02—Polymer mixtures characterised by other features containing two or more polymers of the same C08L -group
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/03—Polymer mixtures characterised by other features containing three or more polymers in a blend
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/14—Polymer mixtures characterised by other features containing polymeric additives characterised by shape
- C08L2205/16—Fibres; Fibrils
Landscapes
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
The invention discloses a kind of unmanned plane case material formulas of lightweight, which is characterized in that by following parts by weight at being grouped as：40 73 parts of novolac epoxy resin, 30 65 parts of bisphenol f type epoxy resin, 6 14 parts of titanium nano-particle, 15 27 parts of carbon fiber, 8 15 parts of aramid fiber, 10 20 parts of graphene, 28 parts of dodecyl sodium sulfate, 14 parts of colorant.The present invention is suitable for low pressure molding process, and prepreg after solidification has that density is small, intensity is high, dielectric properties are excellent, is suitable for preparing lightweight, high-strength, the unmanned plane shell especially required with wave transparent.There is the features such as simple for process, production capacity is high, there is important actual application value.
Description
Technical field
The present invention relates to a kind of unmanned plane case material formulas of lightweight.
Background technology
Unmanned plane shell will have the characteristics that as body platform：The spies such as lightweight construction, at low cost, long storage life
Point.Unmanned plane is more demanding to loss of weight, and airframe-to-fuel weight ratio control can just only be vacateed weight-space below 30% gives combustion
Oil, payload, the stealthy weightening brought of compensation meet the technologies requirements such as light structure, long endurance, height are stealthy, height is motor-driven.According to
The dosage of the current advanced unmanned plane composite materials various in the world of statistics typically constitutes from the 60-80% of housing construction gross weight, some are simultaneously
It is full composite material aircraft, fails to sufficiently achieve the purpose for reducing unmanned plane shell manufacturing cost and abundant loss of weight.
Invention content
In order to overcome the defect of the above-mentioned prior art, the object of the present invention is to provide a kind of unmanned plane case materials of lightweight
Formula.
The present invention takes following technical scheme to realize：A kind of unmanned plane case material formula of lightweight, by following
Parts by weight at being grouped as：40-73 parts of novolac epoxy resin, 30-65 parts of bisphenol f type epoxy resin, 6-14 parts of titanium nano-particle,
15-27 parts of carbon fiber, 8-15 parts of aramid fiber, 10-20 parts of graphene, 2-8 parts of dodecyl sodium sulfate, 1-4 parts of colorant.
The unmanned plane case material formula of above-mentioned a kind of lightweight, by following parts by weight at being grouped as：Epoxy novolac tree
40-68 parts of fat, 30-60 parts of bisphenol f type epoxy resin, 6-11 parts of titanium nano-particle, 15-24 parts of carbon fiber, aramid fiber 8-12
Part, 10-16 parts of graphene, 2-5 parts of dodecyl sodium sulfate, 1-3 parts of colorant.
The unmanned plane case material formula of above-mentioned a kind of lightweight, by following parts by weight at being grouped as：Epoxy novolac tree
55 parts of fat, 48 parts of bisphenol f type epoxy resin, 8 parts of titanium nano-particle, 17 parts of carbon fiber, 10 parts of aramid fiber, 14 parts of graphene,
3 parts of dodecyl sodium sulfate, 2 parts of colorant.
In summary the invention has the advantages that：
The present invention is suitable for low pressure molding process, prepreg after solidification has that density is small, intensity is high, dielectric properties are excellent, fits
It is used to prepare lightweight, high-strength, the unmanned plane shell especially required with wave transparent.There is the features such as simple for process, production capacity is high,
With important actual application value.
Specific implementation mode
Specific embodiment 1：
A kind of unmanned plane case material formula of lightweight, by following parts by weight at being grouped as：40 parts of novolac epoxy resin, bis-phenol
35 parts of F types epoxy resin, 6 parts of titanium nano-particle, 15 parts of carbon fiber, 8 parts of aramid fiber, 11 parts of graphene, dodecyl sodium sulfonate
2 parts of sodium, 1 part of colorant.
Specific embodiment 2：
A kind of unmanned plane case material formula of lightweight, by following parts by weight at being grouped as：55 parts of novolac epoxy resin, bis-phenol
48 parts of F types epoxy resin, 8 parts of titanium nano-particle, 17 parts of carbon fiber, 10 parts of aramid fiber, 14 parts of graphene, dodecyl sodium sulfonate
3 parts of sodium, 2 parts of colorant.
Specific embodiment 3：
A kind of unmanned plane case material formula of lightweight, by following parts by weight at being grouped as：65 parts of novolac epoxy resin, bis-phenol
57 parts of F types epoxy resin, 11 parts of titanium nano-particle, 24 parts of carbon fiber, 12 parts of aramid fiber, 16 parts of graphene, dodecyl sulphur
5 parts of sour sodium, 3 parts of colorant.
Embodiment provided above is the better embodiment of the present invention, only is used for facilitating illustrating the present invention, not to this hair
It is bright to make any form of restriction, any those of ordinary skill in the art, if not departing from the put forward skill of the present invention
In the range of art feature, using the equivalent embodiment for locally changing or modifying made by disclosed technology contents, and
Without departing from the technical feature content of the present invention, in the range of still falling within the technology of the present invention feature.
Claims (3)
1. a kind of unmanned plane case material formula of lightweight, which is characterized in that by following parts by weight at being grouped as：Epoxy novolac
40-73 parts of resin, 30-65 parts of bisphenol f type epoxy resin, 6-14 parts of titanium nano-particle, 15-27 parts of carbon fiber, aramid fiber 8-
15 parts, 10-20 parts of graphene, 2-8 parts of dodecyl sodium sulfate, 1-4 parts of colorant.
2. a kind of unmanned plane case material formula of lightweight according to claim 1, which is characterized in that by following parts by weight
At being grouped as：40-68 parts of novolac epoxy resin, 30-60 parts of bisphenol f type epoxy resin, 6-11 parts of titanium nano-particle, carbon fiber
15-24 parts, 8-12 parts of aramid fiber, 10-16 parts of graphene, 2-5 parts of dodecyl sodium sulfate, 1-3 parts of colorant.
3. a kind of unmanned plane case material formula of lightweight according to claim 1, which is characterized in that by following parts by weight
At being grouped as：55 parts of novolac epoxy resin, 48 parts of bisphenol f type epoxy resin, 8 parts of titanium nano-particle, 17 parts of carbon fiber, aramid fiber
10 parts of fiber, 14 parts of graphene, 3 parts of dodecyl sodium sulfate, 2 parts of colorant.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810498628.7A CN108485205A (en) | 2018-05-23 | 2018-05-23 | A kind of unmanned plane case material formula of lightweight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810498628.7A CN108485205A (en) | 2018-05-23 | 2018-05-23 | A kind of unmanned plane case material formula of lightweight |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108485205A true CN108485205A (en) | 2018-09-04 |
Family
ID=63352047
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810498628.7A Withdrawn CN108485205A (en) | 2018-05-23 | 2018-05-23 | A kind of unmanned plane case material formula of lightweight |
Country Status (1)
| Country | Link |
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| CN (1) | CN108485205A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113072795A (en) * | 2021-03-15 | 2021-07-06 | 浙江宝旌炭材料有限公司 | Aramid fiber/graphene composite reinforced carbon fiber resin prepreg |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104356605A (en) * | 2014-12-11 | 2015-02-18 | 哈尔滨广龙通用航空科技有限公司 | Light prepreg for unmanned aerial vehicle shell and preparation method of prepreg |
| CN106010125A (en) * | 2016-07-13 | 2016-10-12 | 温州雏鹰科技有限公司 | Carbon fiber reinforced composite material for unmanned aerial vehicle shell and preparation method of carbon fiber reinforced composite material |
-
2018
- 2018-05-23 CN CN201810498628.7A patent/CN108485205A/en not_active Withdrawn
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104356605A (en) * | 2014-12-11 | 2015-02-18 | 哈尔滨广龙通用航空科技有限公司 | Light prepreg for unmanned aerial vehicle shell and preparation method of prepreg |
| CN106010125A (en) * | 2016-07-13 | 2016-10-12 | 温州雏鹰科技有限公司 | Carbon fiber reinforced composite material for unmanned aerial vehicle shell and preparation method of carbon fiber reinforced composite material |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113072795A (en) * | 2021-03-15 | 2021-07-06 | 浙江宝旌炭材料有限公司 | Aramid fiber/graphene composite reinforced carbon fiber resin prepreg |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180904 |
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| WW01 | Invention patent application withdrawn after publication |