CN108546381A - A kind of aviation cable jacket material and preparation method thereof - Google Patents
A kind of aviation cable jacket material and preparation method thereof Download PDFInfo
- Publication number
- CN108546381A CN108546381A CN201810517438.5A CN201810517438A CN108546381A CN 108546381 A CN108546381 A CN 108546381A CN 201810517438 A CN201810517438 A CN 201810517438A CN 108546381 A CN108546381 A CN 108546381A
- Authority
- CN
- China
- Prior art keywords
- parts
- cable jacket
- powder
- jacket material
- aviation
- 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
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L27/00—Compositions of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Compositions of derivatives of such polymers
- C08L27/02—Compositions of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Compositions of derivatives of such polymers not modified by chemical after-treatment
- C08L27/12—Compositions of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Compositions of derivatives of such polymers not modified by chemical after-treatment containing fluorine atoms
- C08L27/18—Homopolymers or copolymers or tetrafluoroethene
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J3/00—Processes of treating or compounding macromolecular substances
- C08J3/20—Compounding polymers with additives, e.g. colouring
- C08J3/203—Solid polymers with solid and/or liquid additives
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B3/00—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties
- H01B3/18—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances
- H01B3/30—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes
- H01B3/44—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes vinyl resins; acrylic resins
- H01B3/443—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes vinyl resins; acrylic resins from vinylhalogenides or other halogenoethylenic compounds
- H01B3/445—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes vinyl resins; acrylic resins from vinylhalogenides or other halogenoethylenic compounds from vinylfluorides or other fluoroethylenic compounds
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2327/00—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Derivatives of such polymers
- C08J2327/02—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Derivatives of such polymers not modified by chemical after-treatment
- C08J2327/12—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Derivatives of such polymers not modified by chemical after-treatment containing fluorine atoms
- C08J2327/18—Homopolymers or copolymers of tetrafluoroethylene
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2427/00—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Derivatives of such polymers
- C08J2427/02—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Derivatives of such polymers not modified by chemical after-treatment
- C08J2427/12—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a halogen; Derivatives of such polymers not modified by chemical after-treatment containing fluorine atoms
- C08J2427/16—Homopolymers or copolymers of vinylidene fluoride
-
- 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
- C08K3/18—Oxygen-containing compounds, e.g. metal carbonyls
- C08K3/20—Oxides; Hydroxides
- C08K3/22—Oxides; Hydroxides of metals
- C08K2003/2296—Oxides; Hydroxides of metals of zinc
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2201/00—Properties
- C08L2201/02—Flame or fire retardant/resistant
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2201/00—Properties
- C08L2201/08—Stabilised against heat, light or radiation or oxydation
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2203/00—Applications
- C08L2203/20—Applications use in electrical or conductive gadgets
- C08L2203/202—Applications use in electrical or conductive gadgets use in electrical wires or wirecoating
Landscapes
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
The present invention provides a kind of aviation cable jacket material and preparation method thereof, and the aviation cable jacket material includes following raw material：Polytetrafluoroethylene (PTFE), Kynoar, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine, liquid silica gel, diisononyl phthalate, terephthalate, stearic acid；Preparation method includes the following steps：S1, prepare raw material；S2, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine disperse in liquid silica gel；S3, mixing；S4, it extrusion, is molded, is drying to obtain.Cable jacket material proposed by the present invention, formula is reasonable, and preparation process raw material easily disperses, cable jacket material obtained has excellent mechanical property, flame retardant property and anti-aging property, fire retardant additive amount is few, and service life grows favorable reproducibility between close batch, is suitable for industrialized production.
Description
Technical field
The present invention relates to cable jacket field of material technology more particularly to a kind of aviation cable jacket material and its preparations
Method.
Background technology
Cable is the general designation of optical cable, cable and other items, and there are many uses of the cable, is mainly used for control installation, connection is set
It is standby, the multiple actions such as transmit electric power, be a common and indispensable thing in daily life.In order to improve the use of cable
Service life and security performance, it will usually which external in cable is arranged protective case, cable jacket material used in different field and field
Requirement be also not quite similar, and cable for aerospace sheath material is due to the use of the special of field, therefore to cable jacket material
The requirement of material is also higher than traditional cable jacket material, for example is wanted in the requirement of high temperature resistant, rub resistance and weight etc.
Far above traditional cable jacket material.The elasticity of mesh but current aviation cable jacket is relatively low, and tension and anti-extrusion ability are simultaneously
It is undesirable, and a large amount of fire retardant would generally be added in order to improve flame retardant effect, therefore seriously affected aviation and protected with cable
The tensile property of cover material.Based on the deficiencies in the prior art, the present invention propose a kind of aviation cable jacket material and
Preparation method.
Invention content
The purpose of the present invention is to solve the elastic low of existing cable jacket material, tension and anti-extrusion energy force difference, resistance
The big deficiency of combustion agent dosage, and a kind of aviation cable jacket material and preparation method thereof proposed.
In order to achieve the above object, the present invention is achieved by the following technical programs：
A kind of aviation cable jacket material, includes the raw material of following parts by weight：80~100 parts of polytetrafluoroethylene (PTFE) gathers partially
20~40 parts of vinyl fluoride, 1~5 part of sericite in powder, 2~6 parts of clay powder, 1~3 part of zinc oxide, 0.5~1.5 part of antimony oxide,
1~3 part of melamine, 3~8 parts of liquid silica gel, 0.2~0.6 part of diisononyl phthalate, terephthalate 0.1~
0.3 part, 0.5~1.5 part of stearic acid.
Preferably, the mass ratio of the clay powder and zinc oxide is 2：1.
Preferably, the mass ratio of the antimony oxide and melamine is 1：2.
Preferably, the aviation cable jacket material includes the raw material of following parts by weight：85~95 parts of polytetrafluoroethylene (PTFE),
25~35 parts of Kynoar, 2~4 parts of sericite in powder, 3~5 parts of clay powder, 1~3 part of zinc oxide, antimony oxide 0.8~
1.2 parts, 1.6~2.4 parts of melamine, 4~8 parts of liquid silica gel, 0.2~0.6 part of diisononyl phthalate, terephthaldehyde
0.1~0.3 part of acid esters, 0.8~1.2 part of stearic acid.
Preferably, the aviation cable jacket material includes the raw material of following parts by weight：90 parts of polytetrafluoroethylene (PTFE) gathers partially
30 parts of vinyl fluoride, 3 parts of sericite in powder, 4 parts of clay powder, 2 parts of zinc oxide, 1 part of antimony oxide, 2 parts of melamine, liquid silica gel
6,0.4 part of diisononyl phthalate, 0.2 part of terephthalate, 1 part of stearic acid.
The invention also provides a kind of aviation preparation methods of cable jacket material, include the following steps：
S1, according to 80~100 parts of polytetrafluoroethylene (PTFE), 20~40 parts of Kynoar, 1~5 part of sericite in powder, clay powder 2
~6 parts, 1~3 part of zinc oxide, 0.5~1.5 part of antimony oxide, 1~3 part of melamine, 3~8 parts of liquid silica gel, adjacent benzene two
0.2~0.6 part of formic acid dinonyl, 0.1~0.3 part of terephthalate, 0.5~1.5 part of stearic acid weigh each raw material, standby
With；
S2, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine are added in liquid silica gel and grind 5
~10min, re-ultrasonic dispersion is uniform to obtain mixture A；
S3, it polytetrafluoroethylene (PTFE) and Kynoar is added in kneader is kneaded, then step S2 prepared mixed
Conjunction object A and step S1 weighs diisononyl phthalate, terephthalate and stearic acid agent and is added sequentially to kneader
In, continue to be kneaded to uniformly to get mixture B；
S4, mixture B made from step S3 is added in screw extruder, it is extruded, be molded, be drying to obtain aviation
With cable jacket material.
Cable jacket material provided by the invention, compared with prior art advantage be：Cable jacket proposed by the present invention
Material, formula is reasonable, and preparation process raw material easily disperses, and cable jacket material obtained has excellent mechanical property, anti-flammability
Energy and anti-aging property, fire retardant additive amount is few, and service life grows favorable reproducibility between close batch, is suitable for industrialized production；
Using polytetrafluoroethylene (PTFE) and Kynoar as major ingredient, assign cable jacket material excellent corrosion resistance, by adding sericite
Powder and a certain proportion of clay powder and zinc oxide to ensure that cable jacket material has excellent wearability performance, and are matched
Close antimony oxide, melamine and the liquid silica gel of rational proportion, diisononyl phthalate, terephthalate and
Stearic acid significantly improves the tensile strength and elongation at break of cable jacket material, and tests prove that line prepared by the present invention
The anti-aging property and flame retardant property of cable sheath material are apparently higher than commercial goods, and the invention also provides a kind of operation letters
The method of the preparation aviation cable jacket material single, stock dispersion effect is good, will first be not easy sericite in powder, the clay of mixing
Powder, zinc oxide, antimony oxide, melamine are heated to be ground in liquid silica gel, with improve its in polytetrafluoroethylene (PTFE) and
Mixing in Kynoar is prepared for later stage production performance uniformity, stability height.
Specific implementation mode
The present invention is made further to explain with reference to specific embodiment.
Embodiment 1
A kind of aviation cable jacket material proposed by the present invention, includes the raw material of following parts by weight：Polytetrafluoroethylene (PTFE) 80
Part, 20 parts of Kynoar, 1 part of sericite in powder, 2 parts of clay powder, 1 part of zinc oxide, 0.5 part of antimony oxide, melamine 1
Part, 3 parts of liquid silica gel, 0.2 part of diisononyl phthalate, 0.1 part of terephthalate, 0.5 part of stearic acid；
Preparation method includes the following steps：
S1, according to 80 parts of polytetrafluoroethylene (PTFE), 20 parts of Kynoar, 1 part of sericite in powder, 2 parts of clay powder, 1 part of zinc oxide,
0.5 part of antimony oxide, 1 part of melamine, 3 parts of liquid silica gel, 0.2 part of diisononyl phthalate, terephthalate
0.1 part, 0.5 part of stearic acid weigh each raw material, it is spare；
S2, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine are added in liquid silica gel and are ground
5min, re-ultrasonic dispersion is uniform to obtain mixture A；
S3, it polytetrafluoroethylene (PTFE) and Kynoar is added in kneader is kneaded, then step S2 prepared mixed
Conjunction object A and step S1 weighs diisononyl phthalate, terephthalate and stearic acid agent and is added sequentially to kneader
In, continue to be kneaded to uniformly to get mixture B；
S4, mixture B made from step S3 is added in screw extruder, it is extruded, be molded, be drying to obtain aviation
With cable jacket material.
Embodiment 2
A kind of aviation cable jacket material proposed by the present invention, includes the raw material of following parts by weight：Polytetrafluoroethylene (PTFE) 90
Part, 30 parts of Kynoar, 3 parts of sericite in powder, 4 parts of clay powder, 2 parts of zinc oxide, 1 part of antimony oxide, 2 parts of melamine,
Liquid silica gel 6,0.4 part of diisononyl phthalate, 0.2 part of terephthalate, 1 part of stearic acid；
Preparation method includes the following steps：
S1, according to 90 parts of polytetrafluoroethylene (PTFE), 30 parts of Kynoar, 3 parts of sericite in powder, 4 parts of clay powder, 2 parts of zinc oxide,
1 part of antimony oxide, 2 parts of melamine, liquid silica gel 6,0.4 part of diisononyl phthalate, terephthalate 0.2
Part, 1 part of stearic acid weigh each raw material, spare；
S2, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine are added in liquid silica gel and are ground
8min, re-ultrasonic dispersion is uniform to obtain mixture A；
S3, it polytetrafluoroethylene (PTFE) and Kynoar is added in kneader is kneaded, then step S2 prepared mixed
Conjunction object A and step S1 weighs diisononyl phthalate, terephthalate and stearic acid agent and is added sequentially to kneader
In, continue to be kneaded to uniformly to get mixture B；
S4, mixture B made from step S3 is added in screw extruder, it is extruded, be molded, be drying to obtain aviation
With cable jacket material.
Embodiment 3
Embodiment 1
A kind of aviation cable jacket material proposed by the present invention, includes the raw material of following parts by weight：Polytetrafluoroethylene (PTFE) 100
Part, 40 parts of Kynoar, 5 parts of sericite in powder, 6 parts of clay powder, 3 parts of zinc oxide, 1.5 parts of antimony oxide, melamine 3
Part, 8 parts of liquid silica gel, 0.6 part of diisononyl phthalate, 0.3 part of terephthalate, 1.5 parts of stearic acid；
Preparation method includes the following steps：
S1, according to 100 parts of polytetrafluoroethylene (PTFE), 40 parts of Kynoar, 5 parts of sericite in powder, 6 parts of clay powder, zinc oxide 3
Part, 1.5 parts of antimony oxide, 3 parts of melamine, 8 parts of liquid silica gel, 0.6 part of diisononyl phthalate, terephthalic acid (TPA)
0.3 part of ester, 1.5 parts of stearic acid weigh each raw material, spare；
S2, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine are added in liquid silica gel and are ground
10min, re-ultrasonic dispersion is uniform to obtain mixture A；
S3, it polytetrafluoroethylene (PTFE) and Kynoar is added in kneader is kneaded, then step S2 prepared mixed
Conjunction object A and step S1 weighs diisononyl phthalate, terephthalate and stearic acid agent and is added sequentially to kneader
In, continue to be kneaded to uniformly to get mixture B；
S4, mixture B made from step S3 is added in screw extruder, it is extruded, be molded, be drying to obtain aviation
With cable jacket material.
The cable jacket material and commercially available cable jacket material prepared to Examples 1 to 3 is tested for the property respectively, is tied
Fruit is as follows：
1, performance test before aging, it is as a result as follows：
| Test event | Embodiment 1 | Embodiment 2 | Embodiment 3 | It is commercially available |
| Tensile strength MPa | 35 | 44 | 38 | 26 |
| Elongation at break % | 451 | 482 | 474 | 247 |
| Flame retardant rating | V-0 | V-0 | V-0 | V-2 |
2, thermal aging test, 313 ± 3 DEG C of test temperature, ageing time 120h, test result is as follows：
| Test event | Embodiment 1 | Embodiment 2 | Embodiment 3 | It is commercially available |
| Variation in tensile strength % | 3.6 | 4.1 | 3.2 | 10.4 |
| Elongation at break change rate % | 3.2 | 4.2 | 2.0 | 11.6 |
Above-mentioned test result shows that the flame retardant rating of cable jacket material prepared by Examples 1 to 3 is UL-94V0 grades, in fact
A Zhang Qiangdu Gao Jun are applied in 30MPa or more, elongation at break greatly 450 or more, and change rate exists after thermal aging test
5% hereinafter, and under same test condition, the tensile strength of commercially available cable jacket material is 26MPa, elongation at break only has
457%, show that the flame retardant property, tensile strength, elongation at break of cable jacket material proposed by the present invention are significantly increased,
And cable jacket material property prepared by Examples 1 to 3 is close, shows the preparation weight of cable jacket material proposed by the present invention
Existing property is good, is suitable for industrialized production.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (6)
1. a kind of aviation cable jacket material, which is characterized in that include the raw material of following parts by weight：Polytetrafluoroethylene (PTFE) 80~
100 parts, 20~40 parts of Kynoar, 1~5 part of sericite in powder, 2~6 parts of clay powder, 1~3 part of zinc oxide, antimony oxide
0.5~1.5 part, 1~3 part of melamine, 3~8 parts of liquid silica gel, 0.2~0.6 part of diisononyl phthalate, to benzene two
0.1~0.3 part of formic acid esters, 0.5~1.5 part of stearic acid.
2. a kind of aviation cable jacket material according to claim 1, which is characterized in that the clay powder and zinc oxide
Mass ratio be 2：1.
3. a kind of aviation cable jacket material according to claim 1, which is characterized in that the antimony oxide and three
The mass ratio of poly cyanamid is 1：2.
4. a kind of aviation cable jacket material according to claim 1, which is characterized in that the aviation cable jacket
Material includes the raw material of following parts by weight：85~95 parts of polytetrafluoroethylene (PTFE), 25~35 parts of Kynoar, sericite in powder 2~4
Part, 3~5 parts of clay powder, 1~3 part of zinc oxide, 0.8~1.2 part of antimony oxide, 1.6~2.4 parts of melamine, liquid silica gel
4~8 parts, 0.2~0.6 part of diisononyl phthalate, 0.1~0.3 part of terephthalate, 0.8~1.2 part of stearic acid.
5. a kind of aviation cable jacket material according to claim 1 or 2 or 3, which is characterized in that the aviation line
Cable sheath material includes the raw material of following parts by weight：90 parts of polytetrafluoroethylene (PTFE), 30 parts of Kynoar, 3 parts of sericite in powder, clay
4 parts of powder, 2 parts of zinc oxide, 1 part of antimony oxide, 2 parts of melamine, liquid silica gel 6,0.4 part of diisononyl phthalate,
0.2 part of terephthalate, 1 part of stearic acid.
6. a kind of aviation preparation method of cable jacket material, which is characterized in that include the following steps：
S1, according to 80~100 parts of polytetrafluoroethylene (PTFE), 20~40 parts of Kynoar, 1~5 part of sericite in powder, clay powder 2~6
Part, 1~3 part of zinc oxide, 0.5~1.5 part of antimony oxide, 1~3 part of melamine, 3~8 parts of liquid silica gel, phthalic acid
0.2~0.6 part of dinonyl, 0.1~0.3 part of terephthalate, 0.5~1.5 part of stearic acid weigh each raw material, spare；
S2, sericite in powder, clay powder, zinc oxide, antimony oxide, melamine are added in liquid silica gel grinding 5~
10min, re-ultrasonic dispersion is uniform to obtain mixture A；
S3, polytetrafluoroethylene (PTFE) and Kynoar are added in kneader to the mixture A being kneaded, then step S2 is prepared
And step S1 weighs diisononyl phthalate, terephthalate and stearic acid agent and is added sequentially in kneader, after
It is continuous to be kneaded to uniformly to get mixture B；
S4, mixture B made from step S3 is added in screw extruder, it is extruded, be molded, be drying to obtain aviation line
Cable sheath material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810517438.5A CN108546381A (en) | 2018-05-25 | 2018-05-25 | A kind of aviation cable jacket material and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810517438.5A CN108546381A (en) | 2018-05-25 | 2018-05-25 | A kind of aviation cable jacket material and preparation method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108546381A true CN108546381A (en) | 2018-09-18 |
Family
ID=63511203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810517438.5A Pending CN108546381A (en) | 2018-05-25 | 2018-05-25 | A kind of aviation cable jacket material and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108546381A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007314639A (en) * | 2006-05-24 | 2007-12-06 | Daikin Ind Ltd | Flame-retardant material, and electric wire jacket and lan cable made thereof |
| CN105175959A (en) * | 2015-07-14 | 2015-12-23 | 安徽春辉仪表线缆集团有限公司 | Heatproof corrosion-resistant cable material for urban rail transport and preparation method thereof |
| CN106221090A (en) * | 2016-08-30 | 2016-12-14 | 李兆源 | A kind of pump valve modified plastic material |
-
2018
- 2018-05-25 CN CN201810517438.5A patent/CN108546381A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007314639A (en) * | 2006-05-24 | 2007-12-06 | Daikin Ind Ltd | Flame-retardant material, and electric wire jacket and lan cable made thereof |
| CN105175959A (en) * | 2015-07-14 | 2015-12-23 | 安徽春辉仪表线缆集团有限公司 | Heatproof corrosion-resistant cable material for urban rail transport and preparation method thereof |
| CN106221090A (en) * | 2016-08-30 | 2016-12-14 | 李兆源 | A kind of pump valve modified plastic material |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102746593A (en) | Nitrile rubber insulation flat cable material and preparation method | |
| CN107383696A (en) | A kind of extra-weather-proof high temperature resistant polyvinyl chloride cable material of outdoor uvioresistant and its compound method | |
| WO2018192163A1 (en) | Dynamic vulcanisation flame retardant tpv composite material and preparation method therefor | |
| CN107011600A (en) | A kind of ageing-resistant environmental-friendflame-retardant flame-retardant cable crane span structure of high intensity antistatic and preparation method thereof | |
| CN112321955A (en) | A kind of environment-friendly flame retardant insulating rubber composite material and preparation method thereof | |
| CN108546381A (en) | A kind of aviation cable jacket material and preparation method thereof | |
| CN106566041A (en) | Flexible and distortion-resistant special cable material for wind power generation equipment | |
| CN105885248A (en) | Silane crosslinked rubber cable sheath material | |
| CN105504401A (en) | Cable material with high aging resistance and oil resistance and preparing method thereof | |
| CN105802247B (en) | A kind of weatherability cable insulation material and preparation method thereof | |
| CN113773568A (en) | Insulating material, preparation method and application thereof | |
| CN103554802A (en) | Formula of strippable semiconductive outer shielding material for cable | |
| CN106366629A (en) | Coupling-modified-fullerene-added aluminum hydroxide composite cable material | |
| CN111849044A (en) | High-strength anti-aging cable material | |
| CN105348620A (en) | Weather-proof chemically-crosslinked polyethylene insulated material resistant to temperature of 150 DEG C | |
| CN103304898A (en) | Antistatic flame retardant PP (polypropylene) material | |
| CN111925653A (en) | Thin-wall low-smoke halogen-free flame-retardant insulating material and preparation method thereof | |
| CN105602080A (en) | High-flame-resistance and high-temperature-resistant low-smoke cable material and preparation method thereof | |
| CN103554635B (en) | A kind of preparation technology of strippable semi-conductive external shield material | |
| CN112724468B (en) | Composite environment-friendly flame retardant for PP and PP flame-retardant plastic | |
| CN108546350A (en) | A kind of Insulation anticorrosive cable material and preparation method thereof | |
| CN108623895A (en) | A kind of low temperature resistant cable jacket material and preparation method thereof | |
| CN104311938A (en) | Cable material with strong photostability and preparation method thereof | |
| CN104861396A (en) | Polyvinyl chloride cable material for heat-resistant connecting wire of notebook computer and preparation method of polyvinyl chloride cable material | |
| CN114031866A (en) | Aging-resistant and discoloration-resistant PVC cable material and preparation method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180918 |
|
| WD01 | Invention patent application deemed withdrawn after publication |