CN101508176A - Composite material pulling and extruding molding method by heating baking-path to solidify - Google Patents

Composite material pulling and extruding molding method by heating baking-path to solidify Download PDF

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Publication number
CN101508176A
CN101508176A CNA2009100246496A CN200910024649A CN101508176A CN 101508176 A CN101508176 A CN 101508176A CN A2009100246496 A CNA2009100246496 A CN A2009100246496A CN 200910024649 A CN200910024649 A CN 200910024649A CN 101508176 A CN101508176 A CN 101508176A
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China
Prior art keywords
composite material
drying tunnel
mold
cured
pultrusion
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Pending
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CNA2009100246496A
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Chinese (zh)
Inventor
李勇
肖军
谭永刚
程培忠
孙涛
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Nanjing University of Aeronautics and Astronautics
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Nanjing University of Aeronautics and Astronautics
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Application filed by Nanjing University of Aeronautics and Astronautics filed Critical Nanjing University of Aeronautics and Astronautics
Priority to CNA2009100246496A priority Critical patent/CN101508176A/en
Publication of CN101508176A publication Critical patent/CN101508176A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a pultrusion molding method for a drying tunnel-assisted post-cured composite material, which belongs to the technical field of composite material molding. The method is characterized by comprising the following steps that: (1) reinforced fibers are released through a yarn releasing device and enter a steeping vat through a guide device; (2) fibers impregnated with resin are cured in a hot mold into a gel state; (3) the gel-like composite material product out of the mold is cured in a heating drying tunnel; and (4) the cured composite material is coiled by a coiling device under the traction of a traction unit. The method solves the problem of the prior method that the friction in the curing area of a pultrusion mold is overlarge to cause dead mold, and is particularly applicable to pultruded products with a large specific surface area.

Description

The composite material pultrusion method that adopts the auxiliary back of drying tunnel to solidify
Technical field
The present invention relates to a kind of composite material pultrusion method that adopts the auxiliary back of drying tunnel to solidify, belong to technical field of composite material molding.
Background technology
Pultrude process is the moulding process that automaticity is the highest in the composite material forming method, production efficiency is the highest, is applicable to the production of the continuous composite material goods with constant cross-section shape.As " the fiberglass optical cable strengthens the development of core fast pultrusion technology " (Shen Huiping, Pei Hong, Gao Xudong etc. glass fibre, 2004, (1): 18-19.) ... introduced a kind of typical composite material drawing and extruding technical process: fiber is put yarn and entered the steeping vat impregnating resin, enter heated mold and solidify after preformed, the composite product of curing is through the draw-gear traction continuous rolling of depanning or cut.There is certain defective in this technology: the higher temperature of needs when resin solidifies in mould, resin solidification is emitted a large amount of heat simultaneously, thereby this composite product thermal expansion that causes having cured produces very big frictional resistance in the resin solidification district, expensive mould, the damage goods mechanical property of wearing and tearing causes dead mould to reduce pultrusion production efficiency easily.Especially have bigger specific area when product, the frictional resistance that produces in the mold cured district even can surpass the limit breaking load of product cause product can't adopt pultrude process production.Particularly have continuous pultrusion than the bigger serface goods for finishing composite product, a kind of method that can effectively reduce curing area frictional resistance is demanded invention urgently.
Summary of the invention
Purpose of the present invention, provide a kind of composite material pultrusion method that adopts the auxiliary back of drying tunnel to solidify, to solve the excessive difficult problem that causes dead mould easily of pultrusion die curing area frictional resistance, particularly solution has the difficulty that is difficult to realize pultrusion production than the bigger serface product.
A kind of composite material pultrusion method that adopts the auxiliary back of drying tunnel to solidify is characterized in that process is as follows:
1), fortifying fibre is put yarn and is entered steeping vat through guider by putting yarn feeding device;
2), pitch based fiber is cured to gel state through preformed by heated mold;
3), the composite product that reaches gel state of depanning is finished curing by the heating drying tunnel;
4), under the traction of draw-gear through the wrap-up rolling.
The steeping vat temperature is controlled in the proper range in the said method, and resin viscosity can kept more than 3 hours between 0.5Pa.s~2Pa.s.Mould adopts the low heating-up temperature of more typical pultrusion method, regulates pultrusion speed according to mold temperature simultaneously, and resin reaches gel state when making depanning, can possess stable shape.Drying tunnel adopts higher temperature, and the composite product of gel is solidified rapidly.Drying tunnel two ends open-ended adopts the low higher thermograde form of medium temperature of two ends temperature simultaneously.For the drying tunnel inlet, this thermograde can make the curing degree of composite product improve gradually, and the unexpected temperature of avoiding being in gel state of goods raises, and causes alteration of form; For the drying tunnel outlet, this thermograde can make composite product cool off gradually, avoids too fast cooling to cause very big internal stress influence product properties.That the present invention has is low to extruding equipment repacking cost, the pultrude process parameter is regulated simple advantage.
For the bigger pultrusion product of specific area, i.e. the long-pending ratio A of the area that contacts with die cavity of goods and article cross sections 1/ A 2Bigger, in the thermal expansion strain stress HeatUnder the identical condition, can produce bigger cavity pressure P, thereby produce bigger frictional resistance f.Strength of materials σ at goods bUnder certain condition, goods specific area A 1/ A 2Big more, f/F MaxBig more, work as f/F Max〉=1 o'clock, the frictional resistance of these goods in die cavity was enough to make the goods fracture, can't be by pultrude process production.The present invention can effectively reduce the thermal expansion strain stress of goods in the mold cured district Heat, be specially adapted to have pultrusion than the bigger serface goods.
f=μ×P (1)
P=σ heat×A 1 (2)
σ heat=E×ε heat (3)
F max=σ b×A 2 (4)
f F max = μE σ b × A 1 A 2 × ϵ heat - - - ( 5 )
In the following formula: f---pultrusion frictional resistance; Coefficient of friction between μ---die cavity and goods; P---cavity pressure; σ Heat---the goods thermal expansion stress; A 1---goods and die cavity contact area; E---goods elastic modelling quantity; ε Heat---the thermal expansion strain; F Max---goods can bear ultimate load; σ b---product tensile strength; A 2---article cross sections is long-pending.
Description of drawings
Fig. 1 is the present device structural representation.
Fig. 2 is a drying tunnel temperature distribution schematic diagram of the present invention.
Label title among Fig. 1: 1. put yarn feeding device; 2. guider; 3. steeping vat; 4. pre-shaping device 5. moulds; 6. drying tunnel; 7. draw-gear; 8. wrap-up.
The specific embodiment
Adopt the composite pole of FW-77 hot setting system epoxy resin and T300 carbon fiber pultrusion diameter 0.3mm.
1, the steeping vat temperature determines
Determine that according to sticking temperature test steeping vat can make resin keep viscosity 0.5Pa.s~2Pa.s3 hour, sets 35 ℃ of steeping vat temperature in 35 ℃ ± 2 ℃ scopes.
2, mold temperature determines
Through overtesting, choosing mold temperature is 140 ℃, neither makes mould produce bigger pultrusion resistance and can make PhastGel in the resin short time again, improves pultrusion speed.
3, determining of pultrusion speed
Under 140 ℃ of mold temperatures, select the pultrusion speed of 0.75m/min, can control and reach gel state after resin goes out mould.
4, drying tunnel temperature determines
Under above-mentioned pultrusion speed, adopt 175 ℃ drying tunnel temperature that resin is solidified in drying tunnel fully.

Claims (2)

1, a kind of composite material pultrusion method that adopts the auxiliary back of drying tunnel to solidify is characterized in that process is as follows:
(1), fortifying fibre is put yarn and is entered steeping vat through guider by putting yarn feeding device;
(2), pitch based fiber is cured to gel state through preformed by heated mold;
(3), the composite product that reaches gel state of depanning is finished curing by the heating drying tunnel;
(4), under the traction of draw-gear through the wrap-up rolling.
2, the composite material pultrusion method of employing drying tunnel according to claim 1 auxiliary back curing, it is characterized in that: (3) goes on foot described drying tunnel, high thermograde form in the middle of its temperature employing two ends are low.
CNA2009100246496A 2009-02-25 2009-02-25 Composite material pulling and extruding molding method by heating baking-path to solidify Pending CN101508176A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNA2009100246496A CN101508176A (en) 2009-02-25 2009-02-25 Composite material pulling and extruding molding method by heating baking-path to solidify

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNA2009100246496A CN101508176A (en) 2009-02-25 2009-02-25 Composite material pulling and extruding molding method by heating baking-path to solidify

Publications (1)

Publication Number Publication Date
CN101508176A true CN101508176A (en) 2009-08-19

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Country Status (1)

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CN (1) CN101508176A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102463678A (en) * 2010-11-10 2012-05-23 江苏源盛复合材料技术股份有限公司 Production technology of cable support
CN102553866A (en) * 2011-11-23 2012-07-11 四川航天五源复合材料有限公司 Automatic residue cleaning device and method thereof
CN102729493A (en) * 2012-06-20 2012-10-17 天津工业大学 Molding method and molding apparatus of composite material toughened thin rod
CN102873883A (en) * 2012-10-23 2013-01-16 西安永兴科技发展有限公司 Sealing dipping pultrusion system device for producing optical fiber reinforced core and preparation method
CN103009634A (en) * 2011-09-26 2013-04-03 蓝星(北京)化工机械有限公司 Thermoplastic resin composite material and preparation method thereof
CN104723583A (en) * 2015-03-30 2015-06-24 南京航空航天大学 Equipment and method for preparing composite material, Z-pin, by using electronic beam curing technology
CN105269833A (en) * 2014-11-04 2016-01-27 北京盛华瑞科技有限公司 Two-time compression molding technology for thermoplastic composite material
CN105729744A (en) * 2016-04-01 2016-07-06 安徽冠廷科技有限公司 Production process of carbon fiber compound T-shaped steel
CN105729832A (en) * 2016-04-01 2016-07-06 安徽冠廷科技有限公司 Production process of carbon fiber compound joist steel
CN105835379A (en) * 2016-04-01 2016-08-10 安徽冠廷科技有限公司 Production process for glass fiber composite profiles
CN113320191A (en) * 2021-06-01 2021-08-31 华东理工大学 Pultrusion method of high-performance thermoplastic composite material I-beam

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102463678A (en) * 2010-11-10 2012-05-23 江苏源盛复合材料技术股份有限公司 Production technology of cable support
CN102463678B (en) * 2010-11-10 2014-07-09 江苏源盛复合材料技术股份有限公司 Production technology of cable support
CN103009634B (en) * 2011-09-26 2015-02-18 蓝星(北京)化工机械有限公司 Thermoplastic resin composite material and preparation method thereof
CN103009634A (en) * 2011-09-26 2013-04-03 蓝星(北京)化工机械有限公司 Thermoplastic resin composite material and preparation method thereof
CN102553866A (en) * 2011-11-23 2012-07-11 四川航天五源复合材料有限公司 Automatic residue cleaning device and method thereof
CN102729493A (en) * 2012-06-20 2012-10-17 天津工业大学 Molding method and molding apparatus of composite material toughened thin rod
CN102873883A (en) * 2012-10-23 2013-01-16 西安永兴科技发展有限公司 Sealing dipping pultrusion system device for producing optical fiber reinforced core and preparation method
CN105269833A (en) * 2014-11-04 2016-01-27 北京盛华瑞科技有限公司 Two-time compression molding technology for thermoplastic composite material
CN105269833B (en) * 2014-11-04 2018-04-03 北京盛华瑞科技有限公司 A kind of thermoplastic composite secondary mould pressing forming method
CN104723583A (en) * 2015-03-30 2015-06-24 南京航空航天大学 Equipment and method for preparing composite material, Z-pin, by using electronic beam curing technology
CN105729744A (en) * 2016-04-01 2016-07-06 安徽冠廷科技有限公司 Production process of carbon fiber compound T-shaped steel
CN105729832A (en) * 2016-04-01 2016-07-06 安徽冠廷科技有限公司 Production process of carbon fiber compound joist steel
CN105835379A (en) * 2016-04-01 2016-08-10 安徽冠廷科技有限公司 Production process for glass fiber composite profiles
CN113320191A (en) * 2021-06-01 2021-08-31 华东理工大学 Pultrusion method of high-performance thermoplastic composite material I-beam

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Open date: 20090819