CN109795131A - A kind of carbon fiber/cyanate composite material pipe fitting and preparation method thereof - Google Patents

A kind of carbon fiber/cyanate composite material pipe fitting and preparation method thereof Download PDF

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Publication number
CN109795131A
CN109795131A CN201711139248.6A CN201711139248A CN109795131A CN 109795131 A CN109795131 A CN 109795131A CN 201711139248 A CN201711139248 A CN 201711139248A CN 109795131 A CN109795131 A CN 109795131A
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China
Prior art keywords
carbon fiber
pipe fitting
cyanate
composite material
prepreg
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CN201711139248.6A
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Chinese (zh)
Inventor
林再文
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Changchun Chang Guang Aerospace Composites Co Ltd
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Changchun Chang Guang Aerospace Composites Co Ltd
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Priority to CN201711139248.6A priority Critical patent/CN109795131A/en
Publication of CN109795131A publication Critical patent/CN109795131A/en
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Abstract

The present invention relates to space camera technical fields, specifically disclose a kind of carbon fiber/cyanate composite material pipe fitting and preparation method thereof.Pipe fitting of the invention is integrally formed by prepreg placement process by low coefficient of thermal expansion carbon fiber/cyanate composite material and is made, there is no interface problems, it can be used in space optics truss structure, truss structure environmental stability can be improved, precision, stability influence for improvement variation of ambient temperature to space optics structure, be of great significance, solve the swollen property of existing metallic pipe coupling low-heat and two aspect performance of high specific strength can not both with technological deficiency.

Description

A kind of carbon fiber/cyanate composite material pipe fitting and preparation method thereof
Technical field
The present invention relates to space camera technical field, in particular to a kind of truss structure carbon fiber/cyanate composite wood Expects pipe connector and preparation method thereof.
Background technique
Mainstream structure of the truss structure as space camera, it is often desirable that it is with low coefficient of thermal expansion: become in environment temperature Stable structure when change does not influence imaging precision, stability.
Truss rod structure generallys use composite material, can be by selection fiber, resin and laying angle, in rod piece axis To the low or zero thermal expansion of acquisition.
Truss pipe fitting, since structure, load condition are complicated, common used material is aluminium alloy, titanium alloy, low-heat is swollen system Number alloy.Aluminium alloy, titanium alloy loading ability are high, can be processed into the pipe fitting of complicated shape, but material itself heat expansion system Number is big (2.3 × 10-5/ DEG C of aluminium alloy coefficient of thermal expansion, 9.4 × 10-5/ DEG C of titanium alloy coefficient of thermal expansion).Low coefficient of thermal expansion alloy, heat Swollen coefficient is low (such as invar, coefficient of thermal expansion 0), however density is larger, and specific strength is low, specific stiffness is low.
Summary of the invention
The present invention is directed to overcome, the swollen property of metallic pipe coupling low-heat can not be simultaneous with two aspect performance of high specific strength in the prior art The technological deficiency of tool provides a kind of novel truss structure carbon fibre reinforced pipe connector and preparation method thereof.
To achieve the above object, the invention adopts the following technical scheme:
On the one hand, the present invention provides a kind of carbon fiber/cyanate composite material pipe fitting, and the pipe fitting is by the swollen system of low-heat Number carbon fiber/cyanate composite material is integrally formed by prepreg placement process and is made.The composite pipe joint can be used for In the truss structure of space camera.
In some embodiments, the pipe fitting on pipe fitting axial direction thermal expansion factor absolute value less than 1 × 10-6/K。
In some embodiments, the low coefficient of thermal expansion carbon fiber/cyanate composite material, in 0 ° of direction coefficient of thermal expansion of single layer For α1, -1 × 10-6/ K < α1< 1 × 10-6/K;It is α in 90 ° of direction coefficient of thermal expansions of single layer2, 15 × 10-6/ K < α2< 35 × 10-6/K。
In some embodiments, the carbon fiber/cyanate composite material is by high-strength carbon fiber/cyanate ester material and Gao Mo Type carbon fiber/cyanate ester material is mixed to get.
In some embodiments, in the high-strength carbon fiber/cyanate ester material intensity of carbon fiber be 2000MPa~ 4000MPa, modulus are 200GPa~300GPa;The modulus of carbon fiber exists in the high model carbon fiber/cyanate ester material 300GPa or more.
In some embodiments, the laying angle of the carbon fiber/cyanate composite material is (02/±θ)n, 60 °≤θ≤ 80°。
In some embodiments, with carbon fiber/cyanate composite material volume for 100%, the carbon fiber/cyanate is multiple In condensation material, the volume content of carbon fiber is 57%~63%.
Yet another aspect, the present invention provide a kind of preparation method of above-mentioned pipe fitting, the preparation method include: S1, According to laying angle and sequence, laying cyanate/carbon fiber prepreg on mold;S2, pass through metal to mould or vacuum bag method It is compacted laying;S3, entirety enter furnace curing molding and obtain the pipe fitting.
In some embodiments, the mold is metal positive.
In some embodiments, the cyanate/carbon fiber prepreg is by high-strength carbon fiber/cyanate prepreg and Gao Mo Type carbon fiber/two kinds of cyanate prepreg prepreg is mixed to prepare.
The beneficial effects of the present invention are: low coefficient of thermal expansion carbon fiber/cyanate composite material pipe fitting of the invention leads to It crosses integrated molding solidification to obtain, interface problem is not present, can be used in space optics truss structure, truss structure environment can be improved Stability, precision, stability influence for improvement variation of ambient temperature to space optics structure, is of great significance.
In carbon fiber provided by the invention/cyanate composite material pipe fitting, carbon fiber/cyanate prepreg is using high-strength Type carbon fiber/cyanate prepreg and high model carbon fiber/cyanate prepreg mix use, axial to use high model carbon fiber Low coefficient of thermal expansion is contributed, circumferential direction is high-intensitive using the contribution of high-strength carbon fiber.Taking into account low thermal expansion properties and high specific strength performance While, preferably solve in forming process that there are the pipe fitting problem of Cracking that internal stress may cause in pipe fitting.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, below in conjunction with specific embodiment, to this Invention is further elaborated.It should be appreciated that described herein, specific examples are only used to explain the present invention, without structure At limitation of the present invention.
The present invention provides a kind of truss structure carbon fiber/cyanate composite material pipe fitting, and the pipe fitting is swollen by low-heat Coefficient carbon fiber/cyanate composite material is integrally formed by prepreg placement process and is made.Be integrally formed obtain product without Splicing face and fiber continuity is good, product mechanical property is more excellent, reliability is higher.
In specific embodiment, pipe fitting of the invention on pipe fitting axial direction thermal expansion factor absolute value less than 1 × 10-6/ K.Especially by using the carbon fiber with typically negative thermal expansion coefficient, after forming single layer with resin matrix, 0 ° of direction heat Swollen coefficient is α1, -1 × 10-6/ K < α1< 1 × 10-6/ K is α in 90 ° of direction coefficient of thermal expansions of single layer2, 15 × 10-6/ K < α2< 35×10-6/ K can make laminate X to coefficient of thermal expansion absolute value less than 1 × 10 by designing laying-6/ K, so that pipe fitting exists Thermal expansion factor absolute value is less than 1 × 10 on pipe fitting axial direction-6/K。
Wherein, carbon fiber/cyanate composite material is by high-strength carbon fiber, high model carbon fiber and cyanate ester resin matrix Two kinds of individual prepregs are obtained by sweat connecting method, high model carbon fiber/cyanate prepreg is as 0 ° of layer, high-strength carbon Fiber/cyanate prepreg molds (or vacuum bag method) as θ ° of layer according to designed laying angle and sequence laying forming Solidification.Specifically, high-strength carbon fiber is selected from Japanese Koryo company's T 300B, T400HB, T700SC, T800HB or HF40A type carbon At least one of fiber, high model carbon fiber are selected from Japanese Koryo company M35JB, M40JB, M46JB, M55JB or M60JB type At least one of carbon fiber selects such composite material collocation to use, and pipe fitting obtained can have low heat expansion, There can be high specific strength again.
In specific embodiment, carbon fiber/cyanate composite material laying angle is (02/±θ)n, 60 °≤θ≤80 °, lead to Cross using such laying angle can reduce process implementing during laying angular error to product axial thermal expansion coefficient It influences.Meanwhile interiors of products after forming and hardening can be reduced with the use of two kinds of carbon fibers/cyanate prepreg selected above The radial internal stress of fiber and resin boundary surface.For the present invention by using carbon fiber/cyanate composite material, designability is strong, By adjusting laying angle, low expansion character can be obtained in particular directions.
Carbon fiber/laying angle of cyanate composite material selection and the carbon fiber of selection are that the present inventor is logical It crosses and makes the creative labor acquisition, laying angular error is to product axial thermal expansion coefficient during can reduce process implementing Influence, reduce the radial internal stress of interiors of products fiber and resin boundary surface after forming and hardening.
In carbon fiber/cyanate composite material used in pipe fitting of the invention, with carbon fiber/cyanate composite material Volume be 100%, the volume content of carbon fiber is 57%~63%, enables to every power of the composite material finally obtained It learns performance indicator to be optimal, is equalized tension and compression, Interlaminar shear strengths.
Yet another aspect, the present invention provide a kind of preparation method of above-mentioned pipe fitting, preparation method include: S1, according to Laying angle and sequence, laying cyanate/carbon fiber prepreg on mold, specific prepreg pass through sweat connecting legal system It is standby;S2, laying is compacted to mould or vacuum bag method by metal;S3, entirety enter furnace curing molding and obtain pipe fitting.Specifically, step Mould therefor is metal positive in rapid S1, and cyanate/carbon fiber prepreg of laying is by high-strength carbon fiber/cyanate prepreg It is mixed to prepare with high modulus carbon fiber/two kinds of cyanate prepreg prepreg, so that pipe fitting obtained can have low-heat swollen Swollen property, and can have high specific strength.
Carbon fiber/cyanate composite material of the invention is compared during the preparation process by using prepreg placement process For winding process, fiber volume fraction can be preferably controlled, to improve product mechanical property.
Low coefficient of thermal expansion carbon fiber/cyanate composite material pipe fitting of the invention is obtained, no by being integrally formed solidification There are interface problems, can be used in space optics truss structure, and truss structure environmental stability can be improved, for improving environment temperature Precision of the degree variation to space optics structure, stability influence, are of great significance.
In carbon fiber provided by the invention/cyanate composite material pipe fitting, carbon fiber/cyanate prepreg is using high-strength Degree carbon fiber/cyanate prepreg and high modulus carbon fiber/cyanate prepreg mix use, axial to use high modulus carbon fiber Low coefficient of thermal expansion is contributed, circumferential direction is high-intensitive using high-strength carbon fiber contribution, is taking into account low thermal expansion properties and high specific strength performance While, preferably solve in forming process that there are the pipe fitting problem of Cracking that internal stress may cause in pipe fitting.
It is described in detail below in conjunction with specific embodiment.
Embodiment 1
S1, according to [02/±66]4Laying angle and sequence, laying cyanate/carbon fiber is pre- on metal positive mold Leaching material, 0 ° of laying are high model carbon fiber/cyanate prepreg, and thickness 0.15mm, 66 ° of layings are high-strength carbon fiber/cyanic acid Ester prepreg, thickness are 0.125mm;Wherein, high model carbon fiber uses toray company M55JB, high-strength carbon fiber For Japanese Koryo company's T 800HB;S2, pass through metal to the real laying of molding;S3, it will integrally enter furnace curing molding and obtain pipe fitting.
After tested, the pipe fitting axial direction coefficient of thermal expansion of pipe fitting obtained is -0.337 × 10-6/ K, hoop rigidity are 55.02GPa, pipe fitting does not occur cracking phenomena in forming process.
Embodiment 2
S1, according to [02/±68]4Laying angle and sequence, laying cyanate/carbon fiber is pre- on metal positive mold Leaching material, 0 ° of laying are high model carbon fiber/cyanate prepreg, and thickness 0.15mm, 68 ° of layings are high-strength carbon fiber/cyanic acid Two kinds of prepregs of ester prepreg are according to thickness is 0.125mm;Wherein, high modulus carbon fiber is using Japanese Koryo company M55JB, high-strength carbon fiber are Japan Koryo company's T 700SC;S2, pass through metal to the real laying of molding;S3, furnace will integrally be entered Curing molding obtains pipe fitting.
After tested, the pipe fitting axial direction coefficient of thermal expansion of pipe fitting obtained is -0.296 × 10-6/ K, hoop rigidity are 58.03GPa, pipe fitting does not occur cracking phenomena in forming process.
Embodiment 3
S1, according to [02/±61]3Laying angle and sequence, laying cyanate/carbon fiber is pre- on metal positive mold Leaching material, 0 ° of laying are high-strength carbon fiber/cyanate prepreg, and thickness 0.2mm, 61 ° of layings are high model carbon fiber/cyanate Prepreg, thickness are 0.1mm;Wherein, high modulus carbon fiber uses Japan Koryo company M40JB, and high-strength carbon fiber is day This Koryo company's T 700SC;S2, pass through metal to the real laying of molding;S3, it will integrally enter furnace curing molding and obtain pipe fitting.
After tested, the pipe fitting axial direction coefficient of thermal expansion of pipe fitting obtained is -0.0687 × 10-6/ K, hoop rigidity are 28.57GPa, pipe fitting does not occur cracking phenomena in forming process.
Embodiment 4
S1, according to [02/±80]4Laying angle and sequence, laying cyanate/carbon fiber is pre- on metal positive mold Leaching material, 0 ° of laying are high-strength carbon fiber/cyanate prepreg, and thickness 0.15mm, 80 ° of layings are high model carbon fiber/cyanic acid Ester prepreg, thickness are 0.1mm;Wherein, high modulus carbon fiber uses Japan Koryo company M55JB, and high-strength carbon fiber is Japanese Koryo company's T 700SC;S2, pass through metal to the real laying of molding;S3, it will integrally enter furnace curing molding and obtain pipe fitting.
After tested, the pipe fitting axial direction coefficient of thermal expansion of pipe fitting obtained is -0.158 × 10-6/ K, hoop rigidity are 47.75GPa, pipe fitting does not occur cracking phenomena in forming process.
Embodiment 5
S1, according to [02/±60]3Laying angle and sequence, laying cyanate/carbon fiber is pre- on metal positive mold Leaching material, 0 ° of laying are high-strength carbon fiber/cyanate prepreg, and thickness 0.15mm, 60 ° of layings are high model carbon fiber/cyanic acid Ester prepreg, thickness are 0.15mm;Wherein, high modulus carbon fiber uses Japan Koryo company M40JB, and high-strength carbon fiber is Japanese Koryo company's T 700SC;S2, pass through metal to the real laying of molding;S3, it will integrally enter furnace curing molding and obtain pipe fitting.
After tested, the coefficient of thermal expansion of pipe fitting obtained is -0.222 × 10-6/ K, hoop rigidity 36.57GPa, molding Pipe fitting does not occur cracking phenomena in the process.
To sum up, in carbon fiber provided by the invention/cyanate composite material pipe fitting, carbon fiber/cyanate preimpregnation Material mixes use using high-strength carbon fiber/cyanate prepreg and high modulus carbon fiber/cyanate prepreg, axial using high Modulus carbon fiber contributes low coefficient of thermal expansion, circumferential high-intensitive using high-strength carbon fiber contribution, is taking into account low thermal expansion properties and height While specific strength performance, preferably solve in forming process that there are the pipe fittings that internal stress may cause to open in pipe fitting Split problem.
The above described specific embodiments of the present invention are not intended to limit the scope of the present invention..Any basis Any other various changes and modifications made by technical concept of the invention should be included in the guarantor of the claims in the present invention It protects in range.

Claims (10)

1. a kind of carbon fiber/cyanate composite material pipe fitting, which is characterized in that the pipe fitting is by low coefficient of thermal expansion carbon fiber Dimension/cyanate composite material is integrally formed by prepreg placement process and is made.
2. pipe fitting as described in claim 1, which is characterized in that pipe fitting coefficient of thermal expansion on pipe fitting axial direction is exhausted To value less than 1 × 10-6/K。
3. pipe fitting as described in claim 1, which is characterized in that the low coefficient of thermal expansion carbon fiber/cyanate composite material, It is α in 0 ° of direction coefficient of thermal expansion of single layer1, -1 × 10-6/ K < α1< 1 × 10-6/K;It is α in 90 ° of direction coefficient of thermal expansions of single layer2, 15 ×10-6/ K < α2< 35 × 10-6/K。
4. pipe fitting as described in claim 1, which is characterized in that the carbon fiber/cyanate composite material is by high-strength carbon Fiber/cyanate ester material is mixed to get with high model carbon fiber/cyanate ester material.
5. pipe fitting as claimed in claim 4, which is characterized in that carbon fiber in the high-strength carbon fiber/cyanate ester material Intensity be 2000MPa~4000MPa, modulus be 200GPa~300GPa;Carbon in the high model carbon fiber/cyanate ester material The modulus of fiber is in 300GPa or more.
6. pipe fitting as described in claim 1, which is characterized in that the laying angle of the carbon fiber/cyanate composite material It is (02/±θ)n, 60 °≤θ≤80 °.
7. pipe fitting as described in claim 1, which is characterized in that be with carbon fiber/cyanate composite material volume 100%, in the carbon fiber/cyanate composite material, the volume content of carbon fiber is 57%~63%.
8. a kind of preparation method of pipe fitting as described in claim 1, which is characterized in that the preparation method includes:
S1, according to laying angle and sequence, laying cyanate/carbon fiber prepreg on mold;
S2, laying is compacted to mould or vacuum bag method by metal;
S3, entirety enter furnace curing molding and obtain the pipe fitting.
9. preparation method as described in claim 1, which is characterized in that the mold is metal positive.
10. preparation method as described in claim 1, which is characterized in that the cyanate/carbon fiber prepreg is by high-strength carbon Fiber/cyanate prepreg is mixed to prepare with high model carbon fiber/two kinds of cyanate prepreg prepreg.
CN201711139248.6A 2017-11-16 2017-11-16 A kind of carbon fiber/cyanate composite material pipe fitting and preparation method thereof Pending CN109795131A (en)

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CN110439892A (en) * 2019-07-26 2019-11-12 中国科学院长春光学精密机械与物理研究所 A kind of rod piece connector and solidification tooling
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CN110529475A (en) * 2019-08-22 2019-12-03 中山大学 Split-type composite material multiple-pass joint for antenna back frame
CN110529475B (en) * 2019-08-22 2021-05-25 中山大学 Split type composite material multi-way joint for antenna back frame
CN112060617A (en) * 2020-08-31 2020-12-11 长春长光宇航复合材料有限公司 Composite hollow curved tube, forming die and preparation method

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