CN108262976A - The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework - Google Patents

The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework Download PDF

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Publication number
CN108262976A
CN108262976A CN201611267266.8A CN201611267266A CN108262976A CN 108262976 A CN108262976 A CN 108262976A CN 201611267266 A CN201611267266 A CN 201611267266A CN 108262976 A CN108262976 A CN 108262976A
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CN
China
Prior art keywords
composite material
space framework
carbon fiber
liner
structural member
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
Application number
CN201611267266.8A
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Chinese (zh)
Inventor
马钰尧
胡匡
胡一匡
张平
张一平
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhengzhou Yoshida Patent Operation Co Ltd
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Zhengzhou Yoshida Patent Operation Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhengzhou Yoshida Patent Operation Co Ltd filed Critical Zhengzhou Yoshida Patent Operation Co Ltd
Priority to CN201611267266.8A priority Critical patent/CN108262976A/en
Publication of CN108262976A publication Critical patent/CN108262976A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/522Joining tubular articles
    • B29C66/5227Joining tubular articles for forming multi-tubular articles by longitudinally joining elementary tubular articles wall-to-wall (e.g. joining the wall of a first tubular article to the wall of a second tubular article) or for forming multilayer tubular articles

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

The invention discloses the methods that a kind of slide fastener occlusion carbon fiber winding composite material structural member prepares space framework.Carbon fiber can bear very big pulling force, and will not deform, but be made as it is solid if, not only can waste of materials, increase weight, and performance improve it is also little, therefore the present invention is designed according to the thickness and stress of pipe, and very big this performance of pulling force is born so as to be optimal performance carbon fiber;Using the space framework light weight of this method preparation, rigidity is high, safety is good, can be as the skeleton of automobile, car and seat.

Description

The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework
Technical field
The present invention relates to the methods that a kind of slide fastener occlusion carbon fiber winding composite material structural member prepares space framework.
Background technology
With the fast development of modern technologies, higher requirement is proposed to material, carbon fiber has high intensity, resistance to height Warm, corrosion-resistant, endurance, light weight can bear the characteristic that very big pulling force etc. is significantly higher than steel, aluminium etc., belong to typical height Performance fibers have overwhelming advantage relative to traditional metal material.Carbon fiber is removed alone as adiabatic heat-insulation material Material is outer, is added in the materials such as resin, metal, ceramics, concrete usually as reinforcing material, forms carbon fibre composite. The composite material force structure and preparation method of reasonable design are needed when carbon fibre composite is used as structural member, can just be filled Carbon fiber is waved in distribution can bear very big this advantage of pulling force.
Invention content
Carbon fiber maximum feature is can to bear very big pulling force in carbon fibre composite, and resin bears pressure, existing Material is made inner tubular portion and does not support, and if plate is made, since plate thickness is too small, generation torque is small, does not make full use of carbon Fiber can bear the advantages of very big pulling force, so needing to study how to give full play to the side that carbon fiber bears this advantage of pulling force Method.It needs the carbon fibre composite light product of density is made thus, if foam is made, since continuous fiber can not Foaming, that is, allow to foam, and the performance of resin can be had an impact after foaming, original performance is lost, can not bear very big drawing Power, therefore how to realize carbon fibre composite as structural member and become to bear very big pulling force for very big problem.
The present invention is exactly to solve the above-mentioned problems, to provide a kind of slide fastener occlusion carbon fiber winding composite material structural member system The method of standby space framework.
The present invention uses following technical scheme:A kind of slide fastener occlusion carbon fiber winding composite material structural member prepares three-dimensional frame The method of frame, the cellular composite material tube that the carbon fiber winding composite material structural member is prepared for continuous carbon fibre, honeycomb The honeycomb hole of shape composite material tube is continuous carbon fibre wound composite pipe, and at least two compositions are whole a branch of, and adjacent twines Position is contacted with each other equipped with the zipper teeth being mutually twisted around pipe, is interlocked by zipper teeth, so as to make adjacent winding pipe It links together, forms whole cellular composite material tube, the method for preparing space framework includes the following steps:
(1)Draw the space framework three-dimensional drawing;
(2)Rubber liner is made according to each ring-shaped frame shape of space framework respectively, rubber liner is disconnected for a side Ring-shaped frame, both ends wherein one end of disconnection are closed, and the other end is set into outlet passageway, and the position that liner disconnects is longer than ring-shaped frame 2.5cm;
(3)Group frame external mold is made according to space framework shape;
(4)Selection matches diameter and the preimpregnation carbon fiber winding composite material tube of length with rubber liner;
(5)Composite material tube is respectively fitted on liner;
(6)Proper amount of gas is filled with to liner;
(7)The prepreg composite materials pipe for being inserted in liner is combined according to the shape of space framework;
(8)It will be in the sub-assembly merging group frame external mold of step 7;
(9)It is charged and discharged gas repeatedly to liner, makes to generate slightly play between winding fiber, be suitble to preimpregnation wound composite pipe Wind the shape of lines;
(10)Mold is heating and curing;
(11)Die sinking, mould unloading, the ring-shaped frame grafting that one side is disconnected are closed.
The step(7)In, prepreg composite materials pipe forms the corresponding ring-shaped frame in each position of space framework, adjacent to become A branch of ring-shaped frame contacts with each other position equipped with the zipper teeth being mutually twisted, and is interlocked, is formed whole by zipper teeth Space framework shape.
Carbon fiber can bear very big pulling force, and will not deform, but be made as it is solid if, not only can waste of materials, increase Add weight, and performance raising is also little, therefore the present invention is designed according to the thickness and stress of pipe, so as to be optimal hair It waves carbon fiber and bears very big this performance of pulling force;Using the space framework light weight of this method preparation, rigidity is high, safety is good, It can be as the skeleton of automobile, car and seat.
Description of the drawings
Fig. 1 is the structure diagram of carbon fiber winding composite material structural member.
Fig. 2 is carbon fiber winding composite material tube structure diagram.
Fig. 3 is adjacent winding pipe attachment structure schematic diagram.
Fig. 4 is the structure diagram of space framework.
Specific embodiment
The present invention is described in further detail with specific embodiment below in conjunction with the accompanying drawings.
As shown in Figure 1 to 4, a kind of slide fastener occlusion carbon fiber winding composite material structural member prepares the side of space framework Method, the carbon fiber winding composite material structural member is cellular composite material tube prepared by continuous carbon fibre, cellular compound The honeycomb hole of tubes of material is continuous carbon fibre wound composite pipe 1, at least two form it is whole a branch of, fiber winding method with The winding method of steel wire is the same in high pressure steel wire sebific duct, and adjacent winding pipe contacts with each other position equipped with the zipper teeth being mutually twisted 2, it is interlocked by zipper teeth 2, so as to which adjacent winding pipe be made to link together, forms whole cellular composite material Pipe, the method for preparing space framework include the following steps:
(1)Draw the space framework three-dimensional drawing;
(2)Rubber liner is made according to each ring-shaped frame shape of space framework respectively, rubber liner is disconnected for a side Ring-shaped frame, both ends wherein one end of disconnection are closed, and the other end is set into outlet passageway, and the position that liner disconnects is longer than ring-shaped frame 2.5cm;
(3)Group frame external mold is made according to space framework shape;
(4)Selection matches diameter and the preimpregnation carbon fiber winding composite material tube of length with rubber liner;
(5)Composite material tube is respectively fitted on liner;
(6)Proper amount of gas is filled with to liner;
(7)The prepreg composite materials pipe for being inserted in liner is combined according to the shape of space framework;
(8)It will be in the sub-assembly merging group frame external mold of step 7;
(9)It is charged and discharged gas repeatedly to liner, makes to generate slightly play between winding fiber, be suitble to preimpregnation wound composite pipe The shape of lines is wound, eliminates fibre stress;
(10)Mold is heating and curing;
(11)Die sinking, mould unloading, the ring-shaped frame grafting that one side is disconnected are closed.
The step(7)In, prepreg composite materials pipe forms the corresponding ring-shaped frame in each position of space framework, adjacent to become A branch of ring-shaped frame contacts with each other position equipped with the zipper teeth being mutually twisted, and is interlocked, is formed whole by zipper teeth Space framework shape.

Claims (2)

1. a kind of method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework, it is characterised in that:It is described Carbon fiber winding composite material structural member is cellular composite material tube prepared by continuous carbon fibre, cellular composite material tube Honeycomb hole is continuous carbon fibre wound composite pipe, and at least two form whole a branch of, and adjacent winding pipe contacts with each other portion Position is equipped with the zipper teeth being mutually twisted, and is interlocked by zipper teeth, so as to which adjacent winding pipe be made to link together, forms Whole cellular composite material tube, the method for preparing space framework include the following steps:
(1)Draw the space framework three-dimensional drawing;
(2)Rubber liner is made according to each ring-shaped frame shape of space framework respectively, rubber liner is disconnected for a side Ring-shaped frame, both ends wherein one end of disconnection are closed, and the other end is set into outlet passageway, and the position that liner disconnects is longer than ring-shaped frame 2.5cm;
(3)Group frame external mold is made according to space framework shape;
(4)Selection matches diameter and the preimpregnation carbon fiber winding composite material tube of length with rubber liner;
(5)Composite material tube is respectively fitted on liner;
(6)Proper amount of gas is filled with to liner;
(7)The prepreg composite materials pipe for being inserted in liner is combined according to the shape of space framework;
(8)It will be in the sub-assembly merging group frame external mold of step 7;
(9)It is charged and discharged gas repeatedly to liner, makes to generate slightly play between winding fiber, be suitble to preimpregnation wound composite pipe Wind the shape of lines;
(10)Mold is heating and curing;
(11)Die sinking, mould unloading, the ring-shaped frame grafting that one side is disconnected are closed.
2. the method that slide fastener occlusion carbon fiber winding composite material structural member according to claim 1 prepares space framework, It is characterized in that:The step(7)In, prepreg composite materials pipe forms the corresponding ring-shaped frame in each position of space framework, adjacent Position is contacted with each other equipped with the zipper teeth being mutually twisted as a branch of ring-shaped frame, is interlocked, is formed by zipper teeth Whole solid frame shape.
CN201611267266.8A 2016-12-31 2016-12-31 The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework Pending CN108262976A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611267266.8A CN108262976A (en) 2016-12-31 2016-12-31 The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611267266.8A CN108262976A (en) 2016-12-31 2016-12-31 The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework

Publications (1)

Publication Number Publication Date
CN108262976A true CN108262976A (en) 2018-07-10

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ID=62771015

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611267266.8A Pending CN108262976A (en) 2016-12-31 2016-12-31 The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework

Country Status (1)

Country Link
CN (1) CN108262976A (en)

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Application publication date: 20180710

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