CN106320696A - High-strength lightweight composite building formwork and manufacturing process thereof - Google Patents
High-strength lightweight composite building formwork and manufacturing process thereof Download PDFInfo
- Publication number
- CN106320696A CN106320696A CN201610925974.XA CN201610925974A CN106320696A CN 106320696 A CN106320696 A CN 106320696A CN 201610925974 A CN201610925974 A CN 201610925974A CN 106320696 A CN106320696 A CN 106320696A
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- side frame
- composite material
- formwork
- mould board
- strength light
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Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
- E04G9/00—Forming or shuttering elements for general use
- E04G9/10—Forming or shuttering elements for general use with additional peculiarities such as surface shaping, insulating or heating, permeability to water or air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B19/00—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica
- B32B19/02—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica the layer of fibres or particles being impregnated or embedded in a plastic substance
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B19/00—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica
- B32B19/06—Layered products comprising a layer of natural mineral fibres or particles, e.g. asbestos, mica next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/026—Knitted fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/20—All layers being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2607/00—Walls, panels
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Mechanical Engineering (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Textile Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
The invention discloses a high-strength lightweight composite building formwork and a manufacturing process thereof, relates to the technical field of building formwork structures and manufacturing processes and overcomes the technical defect that an existing building formwork is not environment-friendly and is high in cost, heavy and short in service life. The composite building formwork comprises a formwork body integrally made from a carbon fiber composite, a side frame and reinforcing ribs, wherein the formwork body adopts a rectangular structure; the side frame is located on the bottom surface of the formwork body and is flush with four sides of the formwork body, the inner side surface of the side frame and the bottom surface of the formwork body are chamfered for transition, the inner walls of two vertically adjacent side edges of the side frame are chamfered for transition, and connecting holes are formed in side walls in four directions of the side frame; the reinforcing ribs are arranged on the bottom surface of the formwork body and the side wall of the side frame. The formwork is light and durable, has the advantages of high strength, high toughness, corrosion resistance, high-temperature resistance and the like, has the weight being half of that of an aluminum alloy building formwork and one fourth of that of a steel building formwork, and is light to use and good in comfort.
Description
Technical field
The present invention relates to architectural template structure and Manufacturing Techniques field.
Background technology
The building template of life-time service is all wooden, steel form, aluminum alloy pattern plate in the market.The cheap user of wooden form
Just but the use time long is easy for scrapping, put off until some time later for conservation of nature environment, transition disafforestation can cause natural environment
Unbalance, and storage and transport are not convenient.Steel form, aluminum alloy pattern plate do not possess anti-corrosive properties, easily react with cement, so
Before cement casting, steel, aluminum alloy mould plate surface all must be brushed paint and be prevented corrosion, the most not environmentally but also increase cost.Steel, aluminum
Alloy templates once brushes oily uneven omission, may result in template together with theing cement solidifies, so that template is in dismounting time-varying
Shape or scrap.
Summary of the invention
In sum, it is an object of the invention to solving existing building template not environmentally, cost height, heavy and service life
Short technical deficiency, and a kind of high-strength light composite material building mould board and processing technology thereof are proposed.
For solving technical problem proposed by the invention, the technical scheme of employing is:
A kind of high-strength light composite material building mould board, it is characterised in that described building template includes employing carbon fiber and is combined
Material integrated plate body, side frame and reinforcement；Described plate body is rectangular configuration；Described side frame is positioned at plate body
Bottom surface, and flush with plate body four edges, side frame medial surface and plate body bottom surface chamfered transition, side frame is vertically adjacent to both sides
Limit inwall chamfered transition, the sidewall of side frame four direction is equipped with connecting hole；Described reinforcement be located at plate body bottom surface and
Side frame inwall.
Described reinforcement includes vertically disposed cross reinforcing and waling.
Described reinforcement is positioned at plate body bottom surface and uses chamfered transition structure with side frame medial surface intersection.
Described side frame lateral surface four corner uses right-angle structure.
The T700 grade carbon fiber preimpregnation that described plate body, side frame and reinforcement uses mass percent to be 40 ± 5%
Material, the basalt fibre of 20 ± 5%, 10 ± 5% glass fibre and 30% epoxy resin in the environment of 155 ° ± 5 ° 20 ± 5 minutes
Hot-forming composite.
The processing technology of described high-strength light composite material building mould board, it is characterised in that step is as follows:
First, respectively by after T700 grade carbon fiber precursor, basalt fibre precursor and the pre-epoxy resin dipping of glass fiber precursor, incite somebody to action
Each precursor containing epoxy resin is knitted to form woven cloth；
Then, above-described for two-layer base fabric stacking is added on the pre-manufactured model supporting with building template, pre-formed；
Afterwards, pre-formed building template is put in die cavity, in the environment of 155 ± 5 c 20 ± 5 minutes hot-forming, cold
But building template blank is formed after solidifying and setting；
Finally, building template blank repaired, hole and polishing.
The pre-formed required T700 grade carbon fiber prepreg that woven cloth each material mass percentage ratio is 40 ± 5%, 20 ±
Basalt fibre, 10 ± 5% glass fibre and 30 ± 5% epoxy resin of 5%.
Pre-formed required woven cloth includes twill weave cloth and straight burr woven cloth；Twill weave cloth time pre-formed
It is added on pre-manufactured model with straight burr woven cloth alternating layers.
Mix after described T700 grade carbon fiber precursor, basalt fibre precursor and the pre-epoxy resin dipping of glass fiber precursor
It is woven into woven cloth, or is separately woven into woven cloth.
The invention have the benefit that the template Portable durable of the present invention, there is high intensity, high tenacity, corrosion-resistant and resistance to
The advantages such as high temperature, weight is 1/2nd of aluminum alloy building template, is 1/4th of steel building template, uses light, relaxes
Adaptive is good.
Especially in skyscraper, when floor reaches more than 25 layers, template, when integral wall face is lifted up, is other
Template is incomparable.Not only safety is light, more saves a large amount of labour force.Due to carbon fibre composite acid and alkali-resistance, with cement
Mortar does not reacts, smooth after metope solidification, it is not necessary to the most manually to fill a vacancy and strike off.
Accompanying drawing explanation
Fig. 1 is the high-strength light composite material building mould board perspective view one of the present invention.
Fig. 2 is the high-strength light composite material building mould board perspective view two of the present invention.
Fig. 3 is that the high-strength light composite material building mould board of the present invention looks up structural representation two.
Fig. 4 is A A cross section structure schematic diagram in Fig. 3；
Fig. 5 is the structural representation that split of the present invention assembles when using.
Tool present embodiment
Below in conjunction with accompanying drawing and currently preferred specific embodiment, the structure of the present invention is further described.
Shown in Fig. 5, the high-strength light composite material building mould board of the present invention, include employing carbon fine
The dimension plate body 1 of composite material integral formed, side frame 2 and reinforcement 3.Plate body 1, side frame 2 and reinforcement 3 use quality
Percentage ratio is T700 grade carbon fiber prepreg, the basalt fibre of 20 ± 5%, 10 ± 5% glass fibre and 30% epoxy of 40 ± 5%
Resin is 20 ± 5 minutes hot-forming composites in the environment of 155 ° ± 5 °.
Described plate body 1 is rectangular configuration；Described side frame 2 is positioned at plate body 1 bottom surface, and neat with plate body 1 four edges
Flat；In order to ensure support strength, side frame 2 medial surface is 95 degree with the angle of plate body 1 bottom surface, and the two is chamfered transition；Side
Frame 2, vertically adjacent to dual-side inwall chamfered transition, the sidewall of side frame 2 four direction is equipped with connecting hole 21；Described add
Strong muscle 3 is located at plate body 1 bottom surface and side frame 2 inwall, is similarly guarantee support strength, reinforcement 3 be positioned at plate body 1 bottom surface with
Side frame 2 medial surface intersection uses chamfered transition structure.Reinforcement 3 includes vertically disposed cross reinforcing and longitudinally adds
Strong muscle.Aliging for the ease of assembly of the present invention, side frame 2 lateral surface four corner uses right-angle structure.Specifically can use four
The a size of reinforcement of (4-8) * (15-25) mm, and the rounding having radius to be 15-30mm, strengthen gradient 20-40 degree.
The processing technology of the high-strength light composite material building mould board of the present invention, step is as follows:
First, respectively by after T700 grade carbon fiber precursor, basalt fibre precursor and the pre-epoxy resin dipping of glass fiber precursor, incite somebody to action
Each precursor containing epoxy resin is knitted to form woven cloth.Described T700 grade carbon fiber precursor, basalt fibre precursor and glass
After the pre-epoxy resin dipping of glass fiber precursor, mixed weaving becomes woven cloth, or is separately woven into woven cloth.Pre-formed required volume
Weave cotton cloth and include twill weave cloth and straight burr woven cloth；Twill weave cloth and straight burr woven cloth alternating layers superposition time pre-formed
On pre-manufactured model.Pre-formed required woven cloth includes twill weave cloth and straight burr woven cloth.Finally give is prefabricated
The T700 grade carbon fiber prepreg that woven cloth each material mass percentage ratio is 40 ± 5%, the basalt of 20 ± 5% needed for molding are fine
Dimension, 10 ± 5% glass fibre and 30 ± 5% epoxy resin.
Then, above-described for two-layer base fabric stacking is added on the pre-manufactured model supporting with building template, prefabricated
Molding；When woven cloth includes twill weave cloth and straight burr woven cloth；Twill weave cloth and straight burr woven cloth time pre-formed
Alternating layers is added on pre-manufactured model, it is ensured that support strength.Pre-manufactured model is put together by multiple cell blocks, adjacent two lists
It is provided with, between unit's block, the gap that the woven cloth for constituting reinforcement is filled.
Afterwards, put in die cavity by after pre-formed building form removal, in the environment of 155 ± 5 c 20 ± 5 minutes
Hot-forming, form building template blank after cooling and solidifying sizing.
Finally, building template blank repaired, hole and polishing.
The support strength that carbon fiber prepreg of the present invention and epoxy resin content are required during selecting to meet normal use
While, effectively control production cost.
T700 grade carbon fiber containing epoxy resin, basalt fibre and glass fibre prepreg are woven by present invention process
Become woven cloth, carry out pre-formed and hot-forming, there is make efficiency high, high intensity, high tenacity, corrosion-resistant and high temperature resistant one-tenth
This low advantage.
Claims (9)
1. a high-strength light composite material building mould board, it is characterised in that it is multiple that described building template includes employing carbon fiber
Condensation material integrated plate body, side frame and reinforcement；Described plate body is rectangular configuration；Described side frame is positioned at plate originally
Body bottom surface, and flush with plate body four edges, side frame medial surface and plate body bottom surface chamfered transition, side frame is vertically adjacent to two
Side inside wall chamfered transition, the sidewall of side frame four direction is equipped with connecting hole；Described reinforcement is located at plate body bottom surface
With side frame inwall.
A kind of high-strength light composite material building mould board the most according to claim 1, it is characterised in that: described reinforcement
Muscle includes vertically disposed cross reinforcing and waling.
A kind of high-strength light composite material building mould board the most according to claim 1, it is characterised in that: described reinforcement
Muscle is positioned at plate body bottom surface and uses chamfered transition structure with side frame medial surface intersection.
A kind of high-strength light composite material building mould board the most according to claim 1, it is characterised in that: described side
Frame lateral surface four corner uses right-angle structure.
A kind of high-strength light composite material building mould board the most according to claim 1, it is characterised in that: described plate is originally
T700 grade carbon fiber prepreg, the basalt of 20 ± 5% that body, side frame and reinforcement use mass percent to be 40 ± 5% are fine
Dimension, 10 ± 5% glass fibre and 30% epoxy resin, 20 ± 5 minutes hot-forming composites in the environment of 155 ° ± 5 °.
6. the processing technology of the high-strength light composite material building mould board as described in any one of claim 1 to 5, its feature exists
As follows in step:
First, respectively by after T700 grade carbon fiber precursor, basalt fibre precursor and the pre-epoxy resin dipping of glass fiber precursor, incite somebody to action
Each precursor containing epoxy resin is knitted to form woven cloth；
Then, above-described for two-layer base fabric stacking is added on the pre-manufactured model supporting with building template, pre-formed；
Afterwards, pre-formed building template is put in die cavity, in the environment of 155 ± 5 c 20 ± 5 minutes hot-forming, cold
But building template blank is formed after solidifying and setting；
Finally, building template blank repaired, hole and polishing.
The processing technology of high-strength light composite material building mould board the most according to claim 6, it is characterised in that: prefabricated
The T700 grade carbon fiber prepreg that woven cloth each material mass percentage ratio is 40 ± 5%, the basalt of 20 ± 5% needed for molding are fine
Dimension, 10 ± 5% glass fibre and 30 ± 5% epoxy resin.
The processing technology of high-strength light composite material building mould board the most according to claim 6, it is characterised in that: prefabricated
Woven cloth needed for molding includes twill weave cloth and straight burr woven cloth；Twill weave cloth and straight burr woven cloth time pre-formed
Alternating layers is added on pre-manufactured model.
The processing technology of high-strength light composite material building mould board the most according to claim 6, it is characterised in that: described
T700 grade carbon fiber precursor, mixed weaving becomes braiding after basalt fibre precursor epoxy resin dipping pre-with glass fiber precursor
Cloth, or it is separately woven into woven cloth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610925974.XA CN106320696A (en) | 2016-10-31 | 2016-10-31 | High-strength lightweight composite building formwork and manufacturing process thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610925974.XA CN106320696A (en) | 2016-10-31 | 2016-10-31 | High-strength lightweight composite building formwork and manufacturing process thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106320696A true CN106320696A (en) | 2017-01-11 |
Family
ID=57819273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610925974.XA Pending CN106320696A (en) | 2016-10-31 | 2016-10-31 | High-strength lightweight composite building formwork and manufacturing process thereof |
Country Status (1)
| Country | Link |
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| CN (1) | CN106320696A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107060318A (en) * | 2017-05-11 | 2017-08-18 | 扬州赛创新材料科技有限公司 | A kind of composite building template and its manufacture method |
| CN112727065A (en) * | 2020-12-26 | 2021-04-30 | 晟通科技集团有限公司 | Form panel |
| TWI779525B (en) * | 2021-03-18 | 2022-10-01 | 永虹先進材料股份有限公司 | Carbon fiber plate, manufacturing method and system thereof |
| CN115478684A (en) * | 2022-10-31 | 2022-12-16 | 山东科华赛邦新材料股份有限公司 | Composite building template and manufacturing method thereof |
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| US6357196B1 (en) * | 1997-05-02 | 2002-03-19 | Mccombs M. Scott | Pultruded utility pole |
| CN201007083Y (en) * | 2007-01-11 | 2008-01-16 | 上海克朗宁技术设备有限公司 | Injection molding building mould |
| CN201155084Y (en) * | 2008-02-05 | 2008-11-26 | 万水 | Pultrusion resin based fiber-reinforced plastic section bar |
| CN101591972A (en) * | 2009-06-29 | 2009-12-02 | 南京工业大学 | A kind of building template molded through pultrusion of composite material |
| CN105604312A (en) * | 2016-02-25 | 2016-05-25 | 广州金发碳纤维新材料发展有限公司 | Fiber-reinforced building formwork and preparation method thereof |
| CN206144130U (en) * | 2016-10-31 | 2017-05-03 | 深圳市天龙金属制品有限公司 | High strength light weight composite building templates |
-
2016
- 2016-10-31 CN CN201610925974.XA patent/CN106320696A/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6357196B1 (en) * | 1997-05-02 | 2002-03-19 | Mccombs M. Scott | Pultruded utility pole |
| CN201007083Y (en) * | 2007-01-11 | 2008-01-16 | 上海克朗宁技术设备有限公司 | Injection molding building mould |
| CN201155084Y (en) * | 2008-02-05 | 2008-11-26 | 万水 | Pultrusion resin based fiber-reinforced plastic section bar |
| CN101591972A (en) * | 2009-06-29 | 2009-12-02 | 南京工业大学 | A kind of building template molded through pultrusion of composite material |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107060318A (en) * | 2017-05-11 | 2017-08-18 | 扬州赛创新材料科技有限公司 | A kind of composite building template and its manufacture method |
| CN112727065A (en) * | 2020-12-26 | 2021-04-30 | 晟通科技集团有限公司 | Form panel |
| TWI779525B (en) * | 2021-03-18 | 2022-10-01 | 永虹先進材料股份有限公司 | Carbon fiber plate, manufacturing method and system thereof |
| CN115478684A (en) * | 2022-10-31 | 2022-12-16 | 山东科华赛邦新材料股份有限公司 | Composite building template and manufacturing method thereof |
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Application publication date: 20170111 |
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