CN105751651A - Production method of anti-layering foam sandwich composite plate - Google Patents

Production method of anti-layering foam sandwich composite plate Download PDF

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Publication number
CN105751651A
CN105751651A CN201610244381.7A CN201610244381A CN105751651A CN 105751651 A CN105751651 A CN 105751651A CN 201610244381 A CN201610244381 A CN 201610244381A CN 105751651 A CN105751651 A CN 105751651A
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CN
China
Prior art keywords
hole
composite plate
sandwich composite
fabric
mould
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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
CN201610244381.7A
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Chinese (zh)
Inventor
杨朝坤
朱增余
罗国伟
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.)
Guangdong Yatai New Material Technology Co Ltd
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Guangdong Yatai New Material Technology 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 Guangdong Yatai New Material Technology Co Ltd filed Critical Guangdong Yatai New Material Technology Co Ltd
Priority to CN201610244381.7A priority Critical patent/CN105751651A/en
Publication of CN105751651A publication Critical patent/CN105751651A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/02Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/28Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
    • B32B27/281Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42 comprising polyimides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/36Layered products comprising a layer of synthetic resin comprising polyesters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/38Layered products comprising a layer of synthetic resin comprising epoxy resins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/42Layered products comprising a layer of synthetic resin comprising condensation resins of aldehydes, e.g. with phenols, ureas or melamines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/18Layered 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 features of a layer of foamed material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/10Properties of the layers or laminate having particular acoustical properties
    • B32B2307/102Insulating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/304Insulating

Abstract

The invention discloses a production method of an anti-layering foam sandwich composite plate.The production method is characterized in that foaming materials are injected through a glue injecting cavity formed by convex-concave die assembly, the structural glue is used to coats the edge of the dies, a glue injecting opening and a glue outlet are sealed, and die assembly heating and the like are performed to form the foam-loop-embedded anti-layering foam sandwich composite plate.By the mutual embedding of hardened loops and the foaming materials, the anti-layering performance can be increased evidently, the comprehensive mechanical performances such as tensile resistance, pressing resistance, bending resistance and shearing resistance can be evidently increased at the same time.By the profile control of the dies and the die-attaching production process, the special-shaped curved-surface-structured sandwich composite plate can be produced.The anti-layering foam sandwich composite plate can be directly applied to structure support parts, thermal insulation and sound insulation plates, and the like.

Description

A kind of preparation method of anti-layering foam sandwich composite plate
Technical field:
The present invention relates to technical field of composite materials, the preparation method being specifically related to a kind of anti-layering foam sandwich composite plate.
Background technology:
The problem that the skin material of foam sandwich composite plate material and foamed core material are easily layered, is the important indicator affecting the comprehensive serviceability of material.Compared with metal material (such as aluminium alloy), composite is when manufacturing or having an accident impact (instrument in flying bird, slungshot, hail, assembling process falls) in use, its internal delamination damage that easily appearance not easily observes, the safety of serious threat materials'use.Therefore, how improving the shock resistance lesion capability of composite is one of key technology of applying at the main force support structure such as wing, fuselage of composite.
There are some technical measures both at home and abroad, as fabric implants Xcore technology, knitting skill, suturing skill, needling technique etc. with foam suturing skill, pin.These technology or cost height, damage fiber, otherwise artificial participation is too much, and standardization level is relatively low, and product quality concordance is poor.
Summary of the invention:
It is an object of the invention to be in that to provide that a kind of moulding process is simple, be prone to standardized production, product quality concordance better, can significantly improve composite plate delamination resistance can and the preparation method of anti-layering foam sandwich composite plate of comprehensive mechanical property.
The present invention is achieved by the following technical solutions:
The preparation method of a kind of anti-layering foam sandwich composite plate, specifically comprises the following steps that
Step 1: bore the first through hole and the second through hole on the upper mold, mold is convex mold or negative mold, first through hole and the second through hole are positioned at die edge place, wherein the first through hole is as foaming into Jiao Kou, second through hole is as foaming gum exudation mouth, and the first through hole and the second through-hole diameter are identical, and diameter is 5mm~20mm, the inside and outside Skin Exit of the first through hole and the second through hole needs place to make chamfering or fillet processes, in order to inserts injected rubber hose and goes out sebific duct;
Step 2: coat releasing agent on negative mold surface or complete release cloth, repaste gel coat, by Circular Single Terry Machine fabric paving on mould, fabric smooth surface is affixed on die surface, and looped pile, facing to the open side of mould, dips in the resin compound containing firming agent with brush, uniformly brushing is on fabric, making the abundant barrier fabric of resin, treat that it solidifies substantially, the looped pile of solidification is vertical state;Releasing agent or the good release cloth of lay is coated on convex mold surface, repaste gel coat, by Circular Single Terry Machine fabric paving on mould, fabric smooth surface is affixed on die surface, and looped pile, facing to the open side of mould, dips in the resin compound containing firming agent with brush, uniformly brushing is on fabric, making the abundant barrier fabric of resin, treat that it solidifies substantially, the looped pile of solidification is vertical state;
Step 3: the drill bit of suitable diameter stretches into the first described through hole and the second through hole, gets through composite layer, removes chip;
Step 4: the edge's smearing structure glue before matched moulds, makes edge bonding by structure glue, and is encapsulated in by expanded material in the middle of knop cloth reinforced composite, by convex mold and negative mold matched moulds and fix, constitutes injecting glue cavity between upper and lower mould;
Step 5: enter Jiao Kou by the foaming of mold, injecting frothing material in injecting glue cavity, now foaming gum exudation mouth is in open mode;
Step 6: just filled expanded material in injecting glue cavity and when slightly glue overflows, the foaming of mold has been entered Jiao Kou and foaming gum exudation mouth closure is dead;
Step 7: edge is coated structure glue, fill expanded material, block the mould matched moulds extremely entering Jiao Kou and gum exudation mouth, now matched moulds is carried out hyperthermic treatment, obtain anti-layering foam sandwich composite plate, take out made anti-layering foam sandwich composite plate, with the drill bit of suitable diameter, gum-injecting port and gum exudation mouth are drilled through, clean out mould and through hole, reuse to facilitate.
Preferably, the expanded material described in step 5 is epoxy resin, phenolic resin, polyimides or polyurethane.
Preferably, described knop cloth is warp knitted terry fabric or weft knitting knop cloth or towel knop cloth.
Raised line material make eyelid covering and expanded material to make the composite plate of core be a kind of can give full play to the lightweight of bi-material characteristic, the structure of anti-layering or function sheet material.Except can being largely used to structural panel, also there is huge applications space in fields such as insulation, sound-absorbing sound insulation, suction ripple/wave transparents.
nullThe invention has the beneficial effects as follows: the preparation method of a kind of anti-layering foam sandwich composite plate of the present invention,Overcome the deficiency that expanded material sandwich composite board skin layer is easily layered with sandwich layer,There is provided a kind of special fibre fabric to add sticker mould lay and form skin material,By the injecting glue cavity injecting frothing material formed to convex concave mould matched moulds,Structure glue and seal pouring mouth and gum exudation mouth it is coated with by die edge,The operations such as matched moulds intensification,Form the anti-layering sandwich composite board that foam embeds mutually with looped pile,Embedded with the mutual of expanded material by the looped pile hardened,Delamination resistance energy can be significantly improved,Can also significantly improve simultaneously and draw、Pressure、Curved、The comprehensive mechanical property such as cut,Controlled by the profile of mould,Patch mould preparation technology,Abnormal curved surface structure sandwich composite board can be prepared into,Anti-layering foam sandwich composite plate can be directly used for structural support、Insulation、Sound-absorbing, resistant panels material etc..
Accompanying drawing illustrates:
Fig. 1 is the knop cloth of present invention lay structural representation in convex mold;
Fig. 2 is the knop cloth of present invention lay structural representation in negative mold;
Fig. 3 is the anti-layering foam sandwich composite plate structural representation after the matched moulds of the present invention.
Wherein, 1, negative mold;2, convex mold;3, the first through hole;4, the second through hole;5, structure glue adds fiber;6, lower knop cloth;7, upper knop cloth;8, expanded material;9, looped pile.
Detailed description of the invention:
Below in conjunction with embodiments of the invention, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is only a part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
Embodiment:
Step 1: as shown in Figure 1, convex mold 2 is bored two through holes, respectively the first through hole 3 and the second through hole 4, two through holes are positioned at die edge place, and wherein the first through hole 3 is as foaming into Jiao Kou, and the second through hole 4 is as foaming gum exudation mouth, two through-hole diameters are identical, diameter is 5mm~20mm, and the inside and outside Skin Exit of the first through hole 3 and the second through hole 4 needs place to make chamfering or fillet processes, in order to inserts injected rubber hose and goes out sebific duct;Two through holes can also be bored in negative mold 1.
Step 2: as depicted in figs. 1 and 2, coat releasing agent on negative mold 1 surface or complete release cloth, repasting gel coat, by carbon fiber Circular Single Terry Machine fabric paving on mould, fabric smooth surface is affixed on die surface, looped pile is facing to the open side of mould, dipping in the resin compound containing firming agent with brush, uniformly brushing is on fabric, makes the abundant barrier fabric of resin, treating that it solidifies substantially, the looped pile of solidification is vertical state;Releasing agent or the good release cloth of lay is coated on convex mold 2 surface, repaste gel coat, by carbon fiber Circular Single Terry Machine fabric paving on mould, fabric smooth surface is affixed on die surface, and looped pile, facing to the open side of mould, dips in the resin compound containing firming agent with brush, uniformly brushing is on fabric, making the abundant barrier fabric of resin, treat that it solidifies substantially, the looped pile of solidification is vertical state;The gel coat being coated with is epoxy resin or phenolic resin or polyimides or polyurethane (PU) etc. or thermoplastic polymer etc.;
Step 3: the drill bit of suitable diameter is stretched into above-mentioned two through hole, gets through composite layer, removes chip;
Step 4: edge's smearing structure glue before negative mold 1 with the 2-in-1 mould of convex mold and fiber 5, make edge bonding by structure glue, and expanded material is encapsulated in the middle of knop cloth reinforced composite, by convex mold 2 and negative mold 1 matched moulds and fix, between convex mold 2 and negative mold 1, constitute injecting glue cavity;
Step 5: entering Jiao Kou (the first through hole), injecting frothing material in injecting glue cavity by the foaming of convex mold 2, now foaming gum exudation mouth is in open mode;
Step 6: just filled expanded material in injecting glue cavity and when slightly glue overflows, enters Jiao Kou (the first through hole) and foaming gum exudation mouth (the second through hole) closure extremely by the foaming of convex mold;
Step 7: as shown in Figure 3, edge is coated structure glue, fill expanded material, block the mould matched moulds extremely entering Jiao Kou and gum exudation mouth, now matched moulds is carried out hyperthermic treatment, control blowing temperature and time well, obtain the anti-layering foam sandwich composite plate of required expansion density, described expanded material adopts polyester resin to add foaming agent, such as the resin compound being made up of isocyanates, polyhydric alcohol, it is also possible to for hard foam or thermoplastic polymer's expanded materials such as epoxy resin, phenolic resin, polyimides or polyurethane (PU);The anti-layering foam sandwich composite plate of preparation, including upper knop cloth 7 and lower knop cloth 6, the centre of upper knop cloth 7 and lower knop cloth 6 is compounded with expanded material 8, and the looped pile 9 of described upper knop cloth 7 and lower knop cloth 6 embeds in expanded material 8;
Step 8: take out made anti-layering foam sandwich composite plate, with the drill bit of suitable diameter, gum-injecting port and gum exudation mouth are drilled through, clean out mould and through hole, reuse to facilitate.
These are only presently preferred embodiments of the present invention, not in order to limit the present invention, all within the spirit and principles in the present invention, any amendment of making, equivalent replacement, improvement etc., should be included within protection scope of the present invention.

Claims (3)

1. the preparation method of an anti-layering foam sandwich composite plate, it is characterised in that specifically comprise the following steps that
Step 1: bore the first through hole and the second through hole in convex mold or negative mold, the first described through hole and the second through hole are positioned at die edge place, and wherein the first through hole is as foaming into Jiao Kou, and the second through hole is as foaming gum exudation mouth, first through hole and the second through-hole diameter are identical, and diameter is 5mm~20mm;
Step 2: coat releasing agent on negative mold surface or complete release cloth, repaste gel coat, by Circular Single Terry Machine fabric paving on mould, fabric smooth surface is affixed on die surface, and looped pile, facing to the open side of mould, dips in the resin compound containing firming agent with brush, uniformly brushing is on fabric, making the abundant barrier fabric of resin, treat that it solidifies substantially, the looped pile of solidification is vertical state;Releasing agent or the good release cloth of lay is coated on convex mold surface, repaste gel coat, by Circular Single Terry Machine fabric paving on mould, fabric smooth surface is affixed on die surface, and looped pile, facing to the open side of mould, dips in the resin compound containing firming agent with brush, uniformly brushing is on fabric, making the abundant barrier fabric of resin, treat that it solidifies substantially, the looped pile of solidification is vertical state;
Step 3: the drill bit of suitable diameter stretches into the first described through hole and the second through hole, gets through composite layer, removes chip;
Step 4: the edge's smearing structure glue before matched moulds, makes edge bonding by structure glue, and is encapsulated in by expanded material in the middle of knop cloth reinforced composite, by convex mold and negative mold matched moulds and fix, constitutes injecting glue cavity between upper and lower mould;
Step 5: enter Jiao Kou by the foaming of mold, injecting frothing material in injecting glue cavity, now foaming gum exudation mouth is in open mode;
Step 6: just filled expanded material in injecting glue cavity and when slightly glue overflows, the foaming of mold has been entered Jiao Kou and foaming gum exudation mouth closure is dead;
Step 7: edge is coated structure glue, closure extremely enters the mould matched moulds of Jiao Kou and gum exudation mouth, now matched moulds is carried out hyperthermic treatment, obtain anti-layering foam sandwich composite plate, take out made anti-layering foam sandwich composite plate, with the drill bit of suitable diameter, gum-injecting port and gum exudation mouth are drilled through, clean out mould and through hole, reuse to facilitate.
2. the preparation method of anti-layering foam sandwich composite plate according to claim 1, it is characterised in that: the expanded material described in step 5 is epoxy resin, phenolic resin, polyimides or polyurethane.
3. the preparation method of anti-layering foam sandwich composite plate according to claim 1, it is characterised in that: described knop cloth is warp knitted terry fabric or weft knitting knop cloth or towel knop cloth.
CN201610244381.7A 2016-04-18 2016-04-18 Production method of anti-layering foam sandwich composite plate Pending CN105751651A (en)

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Application Number Priority Date Filing Date Title
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107053698A (en) * 2016-12-19 2017-08-18 广东亚太新材料科技有限公司 A kind of preparation method of the anti-layering foam core filled composite material plate material of pile
CN108544809A (en) * 2018-03-29 2018-09-18 江苏赛菲新材料有限公司 A kind of sandwich structure composite material and preparation method thereof
CN110524757A (en) * 2019-08-07 2019-12-03 中国商用飞机有限责任公司北京民用飞机技术研究中心 The flat-plate molded mold of PMI foam core and its application method
CN110978672A (en) * 2019-12-17 2020-04-10 南京工程学院 Integrally formed sandwich structure and process

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101630774A (en) * 2009-08-07 2010-01-20 北京玻钢院复合材料有限公司 Glass steel radar cover single element and forming method thereof
CN101973101A (en) * 2010-11-02 2011-02-16 中天高科特种车辆有限公司 Manufacturing process of recreation vehicle head
CN202088613U (en) * 2011-04-19 2011-12-28 苏州美克思科技发展有限公司 Looped fiber fabric phenolic aldehyde foam composite plate
CN102367019A (en) * 2011-11-03 2012-03-07 中材科技股份有限公司 Fiber-reinforcement three-dimensional sandwich composite material
CN103373014A (en) * 2012-04-25 2013-10-30 浙江昱辉阳光能源有限公司 Thermal insulation material and preparation method thereof
CN105365143A (en) * 2015-11-20 2016-03-02 奇瑞汽车股份有限公司 On-line foam forming method for composite material sandwich structure
CN105442811A (en) * 2015-12-02 2016-03-30 中材科技股份有限公司 Heat insulation decoration plate and preparation method thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101630774A (en) * 2009-08-07 2010-01-20 北京玻钢院复合材料有限公司 Glass steel radar cover single element and forming method thereof
CN101973101A (en) * 2010-11-02 2011-02-16 中天高科特种车辆有限公司 Manufacturing process of recreation vehicle head
CN202088613U (en) * 2011-04-19 2011-12-28 苏州美克思科技发展有限公司 Looped fiber fabric phenolic aldehyde foam composite plate
CN102367019A (en) * 2011-11-03 2012-03-07 中材科技股份有限公司 Fiber-reinforcement three-dimensional sandwich composite material
CN103373014A (en) * 2012-04-25 2013-10-30 浙江昱辉阳光能源有限公司 Thermal insulation material and preparation method thereof
CN105365143A (en) * 2015-11-20 2016-03-02 奇瑞汽车股份有限公司 On-line foam forming method for composite material sandwich structure
CN105442811A (en) * 2015-12-02 2016-03-30 中材科技股份有限公司 Heat insulation decoration plate and preparation method thereof

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107053698A (en) * 2016-12-19 2017-08-18 广东亚太新材料科技有限公司 A kind of preparation method of the anti-layering foam core filled composite material plate material of pile
CN108544809A (en) * 2018-03-29 2018-09-18 江苏赛菲新材料有限公司 A kind of sandwich structure composite material and preparation method thereof
CN110524757A (en) * 2019-08-07 2019-12-03 中国商用飞机有限责任公司北京民用飞机技术研究中心 The flat-plate molded mold of PMI foam core and its application method
CN110978672A (en) * 2019-12-17 2020-04-10 南京工程学院 Integrally formed sandwich structure and process

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