CN112574530A - Design and processing technology of basalt fiber propeller - Google Patents
Design and processing technology of basalt fiber propeller Download PDFInfo
- Publication number
- CN112574530A CN112574530A CN202011430224.8A CN202011430224A CN112574530A CN 112574530 A CN112574530 A CN 112574530A CN 202011430224 A CN202011430224 A CN 202011430224A CN 112574530 A CN112574530 A CN 112574530A
- Authority
- CN
- China
- Prior art keywords
- basalt fiber
- propeller
- parts
- glue solution
- processing technology
- 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
- 229920002748 Basalt fiber Polymers 0.000 title claims abstract description 61
- 238000005516 engineering process Methods 0.000 title claims abstract description 23
- 238000012545 processing Methods 0.000 title claims abstract description 17
- 238000013461 design Methods 0.000 title abstract description 6
- 239000003292 glue Substances 0.000 claims abstract description 26
- 239000004744 fabric Substances 0.000 claims abstract description 21
- 239000007822 coupling agent Substances 0.000 claims abstract description 19
- 239000003822 epoxy resin Substances 0.000 claims abstract description 19
- 239000003607 modifier Substances 0.000 claims abstract description 19
- 229920000647 polyepoxide Polymers 0.000 claims abstract description 19
- 239000003963 antioxidant agent Substances 0.000 claims abstract description 13
- 230000003078 antioxidant effect Effects 0.000 claims abstract description 13
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 13
- 239000012745 toughening agent Substances 0.000 claims abstract description 13
- 238000004519 manufacturing process Methods 0.000 claims abstract description 9
- 238000005520 cutting process Methods 0.000 claims abstract description 7
- 238000002791 soaking Methods 0.000 claims abstract description 7
- 238000000465 moulding Methods 0.000 claims abstract description 5
- 238000007731 hot pressing Methods 0.000 claims abstract 2
- 239000000243 solution Substances 0.000 claims description 25
- 238000000034 method Methods 0.000 claims description 18
- 230000008569 process Effects 0.000 claims description 15
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 claims description 12
- 238000002156 mixing Methods 0.000 claims description 12
- 238000005303 weighing Methods 0.000 claims description 12
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical class [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 8
- 239000006087 Silane Coupling Agent Substances 0.000 claims description 6
- 239000011248 coating agent Substances 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 238000010790 dilution Methods 0.000 claims description 6
- 239000012895 dilution Substances 0.000 claims description 6
- 238000003756 stirring Methods 0.000 claims description 6
- 238000000748 compression moulding Methods 0.000 claims description 5
- 238000003825 pressing Methods 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims 1
- 239000002131 composite material Substances 0.000 abstract description 5
- 230000032683 aging Effects 0.000 abstract description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 7
- 239000004917 carbon fiber Substances 0.000 description 7
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 7
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 239000003365 glass fiber Substances 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- 125000005375 organosiloxane group Chemical group 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000004593 Epoxy Substances 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000011208 reinforced composite material Substances 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 241001391944 Commicarpus scandens Species 0.000 description 1
- 229910000629 Rh alloy Inorganic materials 0.000 description 1
- 230000006750 UV protection Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000002074 melt spinning Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- PXXKQOPKNFECSZ-UHFFFAOYSA-N platinum rhodium Chemical compound [Rh].[Pt] PXXKQOPKNFECSZ-UHFFFAOYSA-N 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000004224 protection Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 238000005491 wire drawing Methods 0.000 description 1
Classifications
-
- 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
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
-
- 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
- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
-
- 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
- C08K13/00—Use of mixtures of ingredients not covered by one single of the preceding main groups, each of these compounds being essential
- C08K13/04—Ingredients characterised by their shape and organic or inorganic ingredients
-
- 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
- C08K5/00—Use of organic ingredients
- C08K5/54—Silicon-containing compounds
- C08K5/541—Silicon-containing compounds containing oxygen
- C08K5/5435—Silicon-containing compounds containing oxygen containing oxygen in a ring
-
- 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
- C08K7/00—Use of ingredients characterised by shape
- C08K7/02—Fibres or whiskers
- C08K7/04—Fibres or whiskers inorganic
- C08K7/10—Silicon-containing compounds
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
The invention provides a design and processing technology of a basalt fiber propeller, and relates to the field of composite materials. The basalt fiber propeller comprises the following components in parts by weight: 100 parts of basalt fiber, 30-50 parts of epoxy resin, 10-30 parts of a modifier, 2-3 parts of a coupling agent, 10-20 parts of a curing agent, 0.05-0.1 part of an antioxidant, 0.1-0.2 part of a toughening agent, and a processing technology of the basalt fiber propeller, wherein the processing technology comprises the following manufacturing technologies: cutting and soaking basalt fiber cloth S1, preparing viscous glue solution S2, preparing mixed viscous glue solution S3, forming prepreg S4, and molding and curing the prepreg S5 or a hot pressing tank. The propeller is light in weight, high in strength, strong in toughness, low in price, ultraviolet irradiation resistant and ageing resistant through the components and the processing technology.
Description
Technical Field
The invention relates to the field of composite materials, in particular to a design and processing technology of a basalt fiber propeller.
Background
The screw propeller is one of the important power devices of small and medium-sized unmanned aerial vehicles. The performance of screw directly determines unmanned aerial vehicle's performance, and the efficiency of screw is closely relevant with the journey with unmanned aerial vehicle's time of flight. Traditional unmanned aerial vehicle screw is wooden or plastics material commonly used. The wood propeller has the advantages of light weight, easy processing, low cost, convenient use and the like, but is easy to scratch, and has poor rain and snow resistance, poor weather resistance and lower efficiency. The plastic propeller is easy to process, low in cost, high in processing precision, light in weight, low in strength and easy to break. Along with the development of science and technology, the demand of unmanned aerial vehicle screw flight, glass fiber and carbon fiber preparation screw get into market. Glass fibers have the advantages of light weight, high tensile strength, and abrasion resistance, but are brittle and have poor abrasion resistance. The carbon fiber epoxy resin reinforced composite material is one of the most advanced high-performance composite materials at present, and has the characteristics of light weight, high strength, high temperature resistance, corrosion resistance, excellent thermodynamic performance and the like. The carbon fiber epoxy resin composite material is applied to the unmanned aerial vehicle, so that the obvious weight reduction effect is achieved, and the performances of fatigue resistance, corrosion resistance and the like are greatly improved. However, the carbon fiber epoxy resin composite material is high in price, the manufacturing cost of the unmanned aerial vehicle propeller is greatly improved, the ultraviolet resistance and the aging resistance of the propeller are low, and the carbon fiber unmanned aerial vehicle propeller is limited to be used in a large amount.
The continuous basalt fiber is a continuous fiber prepared by taking natural basalt ore single-component mineral as a raw material, crushing the raw material, adding the crushed raw material into a melting furnace, melting at 1450-1500 ℃, and then adopting a melt spinning method through a platinum-rhodium alloy wire drawing bushing. The basalt fiber is superior to glass fiber in many technical indexes such as high temperature resistance, chemical stability, corrosion resistance, heat conductivity, electric insulation wire, friction resistance and the like, can replace expensive carbon fiber in part of technologies, and does not generate environmental problems related to asbestos. Therefore, the basalt fiber is an ecological environment-friendly material with low raw material cost, low energy consumption and clean production process, and will play an increasingly important role in various fields of future national economy.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides a design and processing technology of a basalt fiber propeller, and solves the problem that various defects generated by wood, plastic, glass fiber and carbon fiber epoxy resin reinforced composite materials used by existing small and medium-sized unmanned aerial vehicle propellers influence the use of the propellers.
(II) technical scheme
In order to achieve the purpose, the invention is realized by the following technical scheme: the basalt fiber propeller comprises the following components in parts by weight: 100 parts of basalt fiber, 30-50 parts of epoxy resin, 10-30 parts of a modifier, 2-3 parts of a coupling agent, 10-20 parts of a curing agent, 0.05-0.1 part of an antioxidant and 0.1-0.2 part of a toughening agent.
Preferably, the modifier is an epoxy-terminated organosiloxane.
Preferably, the coupling agent is a silane coupling agent.
Preferably, the forming process of the basalt fiber propeller is a compression molding process.
Preferably, the forming process of the basalt fiber propeller is a process.
A processing technology of a basalt fiber propeller comprises the following manufacturing technologies:
s1: cutting basalt fiber cloth according to the size of the propeller, weighing, adding acetone for dilution after weighing the required coupling agent, soaking the basalt fiber cloth for 4-6 hours, taking out and airing;
s2: mixing an organic siloxane modifier and epoxy resin, and uniformly stirring at 20-60 ℃ to obtain a viscous glue solution;
s3: adding a curing agent, an antioxidant and a toughening agent into the viscous glue solution in sequence, mixing uniformly, standing and defoaming to obtain a mixed viscous glue solution;
s4: coating the mixed viscous glue solution on basalt fiber cloth to form a prepreg;
s5: the number of layers for laying the prepreg is determined according to the thickness of the propeller, and the product is obtained by adopting a mould pressing or autoclave forming process, wherein the curing temperature of the material is 80-150 ℃, the applied pressure is 0.2-0.8 MPa, and the curing time is 2-5 h.
(III) advantageous effects
The invention provides a design and processing technology of a basalt fiber propeller. The method has the following beneficial effects:
1. according to the invention, the organic siloxane modified epoxy resin is adopted, the ultraviolet radiation resistance and the ageing resistance of the resin are obviously enhanced, the toughness and the corrosion resistance are very strong, and the strength of the epoxy resin is further enhanced by taking the basalt fiber unidirectional cloth as a reinforcing material.
2. The invention adopts the integral structure of compression molding or autoclave molding, and has the advantages of high strength, light specific gravity, low price, long service life and the like.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The first embodiment is as follows:
the embodiment of the invention provides a basalt fiber propeller which comprises the following components in parts by weight: 100 parts of basalt fiber, 30 parts of epoxy resin, 10 parts of modifier, 2 parts of coupling agent, 10 parts of curing agent, 0.05 part of antioxidant and 0.1 part of toughening agent, wherein the modifier is epoxy-terminated organosiloxane, and the coupling agent is silane coupling agent.
A processing technology of a basalt fiber propeller comprises the following manufacturing technologies:
s1: cutting basalt fiber cloth according to the size of the propeller, weighing, adding acetone for dilution after weighing the required coupling agent, soaking the basalt fiber cloth for 4 hours, taking out and drying;
s2: mixing organic siloxane modifier and epoxy resin, and stirring uniformly at 20 ℃ to obtain viscous glue solution;
s3: adding a curing agent, an antioxidant and a toughening agent into the viscous glue solution in sequence, mixing uniformly, standing and defoaming to obtain a mixed viscous glue solution;
s4: coating the mixed viscous glue solution on basalt fiber cloth to form a prepreg;
s5: the number of layers for laying the prepreg is determined according to the thickness of the propeller, and the product is obtained by adopting a compression molding process, wherein the curing temperature of the material is 80 ℃, the applied pressure is 0.2MPa, and the curing time is 2 h.
Example two:
the embodiment of the invention provides a basalt fiber propeller which comprises the following components in parts by weight: 100 parts of basalt fiber, 30 parts of epoxy resin, 10 parts of modifier, 2 parts of coupling agent, 10 parts of curing agent, 0.05 part of antioxidant and 0.1 part of toughening agent, wherein the modifier is epoxy-terminated organosiloxane, and the coupling agent is silane coupling agent.
A processing technology of a basalt fiber propeller comprises the following manufacturing technologies:
s1: cutting basalt fiber cloth according to the size of the propeller, weighing, adding acetone for dilution after weighing the required coupling agent, soaking the basalt fiber cloth for 5 hours, taking out and drying;
s2: mixing organic siloxane modifier and epoxy resin, and stirring uniformly at 45 ℃ to obtain viscous glue solution;
s3: adding a curing agent, an antioxidant and a toughening agent into the viscous glue solution in sequence, mixing uniformly, standing and defoaming to obtain a mixed viscous glue solution;
s4: coating the mixed viscous glue solution on basalt fiber cloth to form a prepreg;
s5: determining the number of layers for laying the prepreg according to the thickness of the propeller, and obtaining the product by adopting an autoclave molding process, wherein the curing temperature of the material is 120 ℃, the applied pressure is 0.8MPa, and the curing time is 3 h.
Example three:
the embodiment of the invention provides a basalt fiber propeller which comprises the following components in parts by weight: 100 parts of basalt fiber, 50 parts of epoxy resin, 30 parts of modifier, 3 parts of coupling agent, 20 parts of curing agent, 0.1 part of antioxidant and 0.2 part of toughening agent, wherein the modifier is epoxy terminated organic siloxane, and the coupling agent is silane coupling agent.
A processing technology of a basalt fiber propeller comprises the following manufacturing technologies:
s1: cutting basalt fiber cloth according to the size of the propeller, weighing, adding acetone for dilution after weighing the required coupling agent, soaking the basalt fiber cloth for 6 hours, taking out and drying;
s2: mixing organic siloxane modifier and epoxy resin, and stirring uniformly at 35 ℃ to obtain viscous glue solution;
s3: adding a curing agent, an antioxidant and a toughening agent into the viscous glue solution in sequence, mixing uniformly, standing and defoaming to obtain a mixed viscous glue solution;
s4: coating the mixed viscous glue solution on basalt fiber cloth to form a prepreg;
s5: the number of layers for laying the prepreg is determined according to the thickness of the propeller, and the product is obtained by adopting a compression molding process, wherein the curing temperature of the material is 100 ℃, the applied pressure is 0.5MPa, and the curing time is 4 h.
Example four:
the embodiment of the invention provides a basalt fiber propeller which comprises the following components in parts by weight: 100 parts of basalt fiber, 50 parts of epoxy resin, 30 parts of modifier, 3 parts of coupling agent, 20 parts of curing agent, 0.1 part of antioxidant and 0.2 part of toughening agent, wherein the modifier is epoxy terminated organic siloxane, and the coupling agent is silane coupling agent.
A processing technology of a basalt fiber propeller comprises the following manufacturing technologies:
s1: cutting basalt fiber cloth according to the size of the propeller, weighing, adding acetone for dilution after weighing the required coupling agent, soaking the basalt fiber cloth for 6 hours, taking out and drying;
s2: mixing organic siloxane modifier and epoxy resin, and stirring uniformly at 60 ℃ to obtain viscous glue solution;
s3: adding a curing agent, an antioxidant and a toughening agent into the viscous glue solution in sequence, mixing uniformly, standing and defoaming to obtain a mixed viscous glue solution;
s4: coating the mixed viscous glue solution on basalt fiber cloth to form a prepreg;
s5: determining the number of layers for laying the prepreg according to the thickness of the propeller, and obtaining the product by adopting an autoclave molding process, wherein the curing temperature of the material is 150 ℃, the applied pressure is 0.8MPa, and the curing time is 5 h.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. A basalt fiber propeller is characterized in that: the composition comprises the following components in parts by weight: 100 parts of basalt fiber, 30-50 parts of epoxy resin, 10-30 parts of a modifier, 2-3 parts of a coupling agent, 10-20 parts of a curing agent, 0.05-0.1 part of an antioxidant and 0.1-0.2 part of a toughening agent.
2. A basalt fiber propeller as claimed in claim 1, wherein: the basalt fibers are preferably unidirectional basalt fiber cloth.
3. A basalt fiber propeller as claimed in claim 1, wherein: the modifier is epoxy-terminated organic siloxane.
4. A basalt fiber propeller as claimed in claim 1, wherein: the coupling agent is a silane coupling agent.
5. A basalt fiber propeller as claimed in claim 1, wherein: the molding process of the basalt fiber propeller is a compression molding process.
6. A basalt fiber propeller as claimed in claim 1, wherein: the forming process of the basalt fiber propeller is a hot-pressing tank forming process.
7. A processing technology of a basalt fiber propeller is characterized in that: the method comprises the following manufacturing processes:
s1: cutting basalt fiber cloth according to the size of the propeller, weighing, adding acetone for dilution after weighing the required coupling agent, soaking the basalt fiber cloth for 4-6 hours, taking out and airing;
s2: mixing an organic siloxane modifier and epoxy resin, and uniformly stirring at 20-60 ℃ to obtain a viscous glue solution;
s3: adding a curing agent, an antioxidant and a toughening agent into the viscous glue solution in sequence, mixing uniformly, standing and defoaming to obtain a mixed viscous glue solution;
s4: coating the mixed viscous glue solution on basalt fiber cloth to form a prepreg;
s5: the number of layers for laying the prepreg is determined according to the thickness of the propeller, and the product is obtained by adopting a mould pressing or autoclave forming process, wherein the curing temperature of the material is 80-150 ℃, the applied pressure is 0.2-0.8 MPa, and the curing time is 2-5 h.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011430224.8A CN112574530A (en) | 2020-12-07 | 2020-12-07 | Design and processing technology of basalt fiber propeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011430224.8A CN112574530A (en) | 2020-12-07 | 2020-12-07 | Design and processing technology of basalt fiber propeller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112574530A true CN112574530A (en) | 2021-03-30 |
Family
ID=75130405
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011430224.8A Pending CN112574530A (en) | 2020-12-07 | 2020-12-07 | Design and processing technology of basalt fiber propeller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112574530A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113320239A (en) * | 2021-06-15 | 2021-08-31 | 武汉中科先进技术研究院有限公司 | Basalt fiber reinforced wear-resistant composite material and preparation method thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103612407A (en) * | 2013-11-03 | 2014-03-05 | 哈尔滨理工大学 | Manufacturing method of basalt fiber strengthened epoxy resin insulation pipe |
| CN104129081A (en) * | 2014-06-25 | 2014-11-05 | 四川航天五源复合材料有限公司 | Preparation process for continuous basalt fiber composite material |
| CN106084872A (en) * | 2016-06-17 | 2016-11-09 | 句容市百事特复合材料有限公司 | A kind of basalt fibre strengthens thermosetting resin prepreg cloth |
| CN108546353A (en) * | 2018-02-09 | 2018-09-18 | 成都天府轨谷科技有限公司 | A kind of car body manufacture basalt fiber composite material and preparation method thereof |
| US20180371187A1 (en) * | 2017-06-21 | 2018-12-27 | Hyundai Motor Company | Basalt-fiber-reinforced thermoplastic composite material and method of manufacturing the same |
| CN110845829A (en) * | 2019-10-18 | 2020-02-28 | 成都鲁晨新材料科技有限公司 | Low-temperature curing epoxy resin composition and preparation method of prepreg and composite material thereof |
-
2020
- 2020-12-07 CN CN202011430224.8A patent/CN112574530A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103612407A (en) * | 2013-11-03 | 2014-03-05 | 哈尔滨理工大学 | Manufacturing method of basalt fiber strengthened epoxy resin insulation pipe |
| CN104129081A (en) * | 2014-06-25 | 2014-11-05 | 四川航天五源复合材料有限公司 | Preparation process for continuous basalt fiber composite material |
| CN106084872A (en) * | 2016-06-17 | 2016-11-09 | 句容市百事特复合材料有限公司 | A kind of basalt fibre strengthens thermosetting resin prepreg cloth |
| US20180371187A1 (en) * | 2017-06-21 | 2018-12-27 | Hyundai Motor Company | Basalt-fiber-reinforced thermoplastic composite material and method of manufacturing the same |
| CN108546353A (en) * | 2018-02-09 | 2018-09-18 | 成都天府轨谷科技有限公司 | A kind of car body manufacture basalt fiber composite material and preparation method thereof |
| CN110845829A (en) * | 2019-10-18 | 2020-02-28 | 成都鲁晨新材料科技有限公司 | Low-temperature curing epoxy resin composition and preparation method of prepreg and composite material thereof |
Non-Patent Citations (1)
| Title |
|---|
| 刘艳 等: "环氧封端硅氧烷改性环氧树脂的制备及性能研究" * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113320239A (en) * | 2021-06-15 | 2021-08-31 | 武汉中科先进技术研究院有限公司 | Basalt fiber reinforced wear-resistant composite material and preparation method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100564448C (en) | A kind of method for preparing molded epoxy resin sheet and products thereof | |
| CN117487324B (en) | Basalt fiber reinforced corrosion-resistant composite rib and preparation method thereof | |
| CN107541018B (en) | Impregnating resin for reinforcing aramid fiber honeycomb composite material and application thereof | |
| CN101781444A (en) | Method for preparing rare-earth-modified glass-fiber epoxy-resin composite materials | |
| CN110483952A (en) | A kind of plant fiber reinforced epoxy composite material | |
| CN111057369A (en) | Carbon fiber reinforced polyamide composite material pre-soaked basalt fiber cloth and preparation method thereof | |
| CN116694030A (en) | Ultra-light high-strength composite material and preparation method and application thereof | |
| CN112574530A (en) | Design and processing technology of basalt fiber propeller | |
| CN107009649A (en) | A kind of production technology of fiberglass drawing and extruding section bar | |
| CN109878431B (en) | High-performance environment-friendly basalt fiber/fibrilia reinforced resin composite automotive ceiling interior panel and preparation method thereof | |
| CN110305450A (en) | A kind of overhead transmission line fiber-reinforced resin base composite core and preparation method thereof | |
| CN101260224B (en) | Method for modifying bisphenol A epoxy resin by using liquid crystal epoxy resin | |
| CN104845304A (en) | Resource reutilization method by utilization of copper-clad plate residue | |
| CN104985830B (en) | The antiseptic fire-retardation handling process of glass-fiber reinforced plastic grille | |
| CN102952371A (en) | Modified thermosetting ultrahigh-molecular epoxy resin marine board | |
| CN110577727A (en) | anti-aging glass fiber reinforced plastic photovoltaic support and production process thereof | |
| CN101805442A (en) | Epoxy resin composition for large wind blades and preparation method thereof | |
| CN109666264A (en) | A kind of RTM molding bamboo fiber felt enhancing thermosetting resin based composites and preparation method | |
| CN102382368A (en) | Carbon fiber/cenosphere/polypropylene ternary composited material and preparation method thereof | |
| CN109334040A (en) | A kind of pipe-making method of fibre pipe | |
| CN113999484A (en) | Light-weight high-strength high-impact-resistance high-modulus nano modified epoxy resin composition for wind power blade main beam and preparation method thereof | |
| CN113637290A (en) | Epoxy resin-based composite material with high glass transition temperature and capable of being rapidly molded for wind power pultrusion girder and preparation method of epoxy resin-based composite material | |
| CN101838442A (en) | Preparation method of rare earth modified glass fiber epoxy resin composite material | |
| CN102617928A (en) | Modified polypropylene composite material for centrifugal fan of air conditioner cabinet | |
| CN104890258A (en) | Manufacturing technology of corrosion-resisting antiflaming single-hole plate sectional material |
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: 20210330 |
|
| WD01 | Invention patent application deemed withdrawn after publication |