CN103862233B - There is the preparation method of ripple layer sandwich structure composite plate - Google Patents
There is the preparation method of ripple layer sandwich structure composite plate Download PDFInfo
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- CN103862233B CN103862233B CN201410048716.9A CN201410048716A CN103862233B CN 103862233 B CN103862233 B CN 103862233B CN 201410048716 A CN201410048716 A CN 201410048716A CN 103862233 B CN103862233 B CN 103862233B
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- 239000002131 composite material Substances 0.000 title claims abstract description 35
- 238000002360 preparation method Methods 0.000 title claims abstract description 24
- 238000003466 welding Methods 0.000 claims abstract description 22
- 239000002360 explosive Substances 0.000 claims abstract description 17
- 239000000463 material Substances 0.000 claims abstract description 14
- 238000005476 soldering Methods 0.000 claims abstract description 8
- 229910052751 metal Inorganic materials 0.000 claims abstract description 6
- 239000002184 metal Substances 0.000 claims abstract description 6
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 42
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 16
- 238000001816 cooling Methods 0.000 claims description 14
- 229910000838 Al alloy Inorganic materials 0.000 claims description 13
- 238000007789 sealing Methods 0.000 claims description 11
- 229910000743 fusible alloy Inorganic materials 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 9
- 229910001220 stainless steel Inorganic materials 0.000 claims description 9
- 229910052786 argon Inorganic materials 0.000 claims description 8
- 239000007789 gas Substances 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 8
- 239000000839 emulsion Substances 0.000 claims description 6
- 239000010935 stainless steel Substances 0.000 claims description 5
- 239000004411 aluminium Substances 0.000 claims description 2
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 238000005516 engineering process Methods 0.000 abstract description 4
- 229910001283 5083 aluminium alloy Inorganic materials 0.000 description 17
- 238000003754 machining Methods 0.000 description 7
- 229910000975 Carbon steel Inorganic materials 0.000 description 5
- 239000010962 carbon steel Substances 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000005611 electricity Effects 0.000 description 4
- 230000003319 supportive effect Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910000622 2124 aluminium alloy Inorganic materials 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 3
- 238000009835 boiling Methods 0.000 description 2
- 235000014121 butter Nutrition 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000000284 extract Substances 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- IXSZQYVWNJNRAL-UHFFFAOYSA-N etoxazole Chemical compound CCOC1=CC(C(C)(C)C)=CC=C1C1N=C(C=2C(=CC=CC=2F)F)OC1 IXSZQYVWNJNRAL-UHFFFAOYSA-N 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/02—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of sheets
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
The invention discloses a kind of preparation method with ripple layer sandwich structure composite plate, belong to sheet metal manufacturing technology field.The present invention has the preparation method of ripple layer sandwich structure composite plate, comprises and first prepares ripple laminboard layer; Hollow parts to ripple laminboard layer adds passive plug; Ripple laminboard layer and the connection up and down between metal decking is realized by explosive welding; After taking out plug, obtain that there is ripple sandwich structure composite plate.The present invention can obtain than the higher-quality metallurgical binding intensity of soldering and interface, and achieve the connection between foreign material central layer and panel, it is prepared, and speed is fast, efficiency is high, preparation cost is low simultaneously.
Description
Technical field
The present invention relates to a kind of preparation method of laminboard layer composite plate, is specifically a kind of preparation method with ripple layer sandwich structure composite plate, belongs to sheet metal manufacturing technology field.
Background technology
At present, the composite plate with ripple layer sandwich structure obtains at Aeronautics and Astronautics engineering field to be applied widely, in the overall structure performance improving Aeronautics and Astronautics device, reduces weight and improve the aspects such as heat-proof quality having played important function.
The composite plate that existing manufacture has ripple layer sandwich structure mainly adopts superplasticforming/diffusion welding method and brazing, and it has the following disadvantages: (1), shape are single.The method only can directly prepare the composite plate with trapezoidal ripple sandwich structure, cannot be used for the preparation with radian shape, baroque ripple layer sandwich structure composite plate.(2), composite surface is of low quality, the region of especially diffusion welding (DW), and in superplasticforming process, panel and ripple laminboard layer are being connected with not to be connected the pulling force that intersection receives larger, very easily produce groove phenomenon.(3), the method is only applicable to the ripple laminboard layer situation identical with panel material, cannot be applicable to the connection for foreign material between ripple laminboard layer and panel.(4), bond strength is not high.Utilize method for welding to be connected with upper and lower panel by ripple laminboard layer, because soldering joint strength is far below mother metal, when high temperature, mechanical property does not reach the instructions for use in Aeronautics and Astronautics field.
Summary of the invention
Technical problem to be solved by this invention is to overcome above-mentioned defect, provides a kind of and can prepare various shape, the simple efficient and preparation method with ripple layer sandwich structure composite plate that can be applicable to/foreign material of high, the step of bond strength between panel and central layer.
In order to solve the problems of the technologies described above, the preparation method with ripple layer sandwich structure composite plate provided by the invention, comprises the following steps:
1) ripple laminboard layer, is prepared;
2) hollow parts, to ripple laminboard layer adds passive plug;
3), ripple laminboard layer and the connection up and down between metal decking is realized by explosive welding;
4), take out after plug, obtain that there is ripple sandwich structure composite plate.
In the present invention, the preparation process of described ripple laminboard layer is:
1) die with square wave, trapezoidal wave, triangular wave or sine waveform, is processed into stainless steel;
2), by titanium alloy plate be laid on die, then by be embossed on titanium alloy plate;
3), the mould assembled is put into heating furnace, mechanical pressurization is carried out to patrix, guarantee sealing, and by mold heated to titanium alloy superplastic forming temperature, pass into argon gas by the air inlet of patrix simultaneously, superplasticforming is carried out to titanium alloy plate material, after cooling, obtains titanium alloy ripple laminboard layer.
In the present invention, the preparation process of described ripple laminboard layer is:
1) die with square wave, trapezoidal wave, triangular wave or sine waveform, is processed into stainless steel;
2), by flat aluminium alloy plate be laid on die, then by be embossed on flat aluminium alloy plate;
3), the mould assembled is put into heating furnace, mechanical pressurization is carried out to patrix, and by mold heated to superplastic aluminum alloy forming temperature, passes into argon gas by the air inlet of patrix simultaneously, superplasticforming is carried out to aluminium horizontal sheet material, after cooling, obtains aluminium alloy ripple laminboard layer.
In the present invention, described step 2) be:
1), preparation and die have the core rod mould of identical bellows-shaped;
2), in core rod mould pour into a mould low-melting alloy, after cooling, load the hollow parts of ripple laminboard layer as plug.
In the present invention, described step 2) be: after soldering and sealing is carried out at the two ends of ripple laminboard layer hollow parts, the hollow parts to ripple laminboard layer injects low-melting alloy, after cooling as supporting plug.
In the present invention, in described step 2) be: machining inserts the hollow parts of ripple laminboard layer after going out the carbon steel plug identical with ripple laminboard layer bellows-shaped.
In the present invention, described step 3) in blast process be:
1) connecting portion, between ripple laminboard layer and upper and lower panel spreads emulsion;
2), be clipped between upper and lower panel by ripple laminboard layer, ignition charge realizes welding.
In the present invention, described upper and lower panel is titanium alloy sheet or aluminium alloy plate.
In the present invention, described ripple laminboard layer, top panel and lower panel are same material or foreign material.
Beneficial effect of the present invention: the present invention has the following advantages: (1), the present invention utilize Explosion composite to realize the connection of sandwich layer and panel, can obtain than the higher-quality metallurgical binding intensity of soldering and interface, achieve the connection between foreign material central layer and panel simultaneously; (2), the present invention utilizes super plastic forming method to be shaped separately to laminboard layer, and the ripple laminboard layer reducing reflected rate simultaneously of the complicated shape that can be shaped, ensures the precision be shaped; (3), compared with the method for attachment such as soldering and diffusion, the present invention prepares that speed is fast, efficiency is high, preparation cost is low.
Accompanying drawing explanation
Fig. 1 is preparation method's flow chart that the present invention has ripple layer sandwich structure composite plate;
Fig. 2 is ripple laminboard layer die structure dwg;
Fig. 3 is ripple laminboard layer mold sections figure;
Fig. 4 is the mould schematic diagram after assembling;
Fig. 5 is the ripple laminboard layer schematic diagram after being shaped;
Fig. 6 is mandrel form schematic diagram;
Fig. 7 is explosive welding schematic diagram;
Fig. 8 is the composite layered plate with ripple sandwich structure;
In figure, 1-die, 2-patrix, 3-air inlet, 4-metallic plate, 5-top panel, 6-lower panel, 7-plug, 8-explosive welding position.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the preparation method that the present invention has ripple layer sandwich structure composite plate is described further.
embodiment 1
The first step, is of a size of the die 1 of 260mm × 260mm × 40mm with 321 stainless steels (1Cr8Ni9Ti) machining profile, die 1 is sinusoidal wave, sinusoidal wave wavelength is 60mm, and wave amplitude is 30mm, for the manufacture of ripple laminboard layer, as shown in Figure 2,3;
Second step, is laid in the TC4 titanium alloy plate 4 being of a size of 260mm × 260mm × 1.5mm on die 1, then is pressed on TC4 titanium alloy plate 4 by patrix 2, as shown in Figure 4;
3rd step, puts into heating furnace by the mould assembled, and carries out mechanical pressurization, to ensure sealing to patrix 2; Simultaneously by mold heated to 900-920 DEG C, pass into argon gas by the air inlet 3 of patrix 2 simultaneously, superplasticforming carried out to TC4 titanium alloy plate 4, cooling after take out obtain TC4 titanium alloy ripple laminboard layer, as shown in Figure 4,5;
4th step, manufacture and die 1 have the core rod mould of identical bellows-shaped, and low-melting alloy is poured into a mould in core rod mould, low-melting alloy plug 7 is taken out after its cooling, and loaded the hollow position of TC4 titanium alloy ripple laminboard layer, plug 7 plays a supportive role when explosive welding, as shown in Figure 6;
5th step, when the explosive welding position 8(between TC4 titanium alloy ripple laminboard layer and upper TC4 titanium alloy panel 5, lower TC4 titanium alloy panel 6 and TC4 titanium alloy ripple laminboard layer are clipped in the middle of upper and lower panel and upper and lower panel contact site) spread emulsion; Then be clipped between upper and lower TC4 titanium alloy panel, electricity consumption cap sensitive explosive realizes welding between upper and lower TC4 titanium alloy panel with TC4 titanium alloy ripple laminboard layer, as shown in Figure 7;
6th step, puts into water by composite plate after blast, and after being heated to water boiling, namely low-melting alloy plug can melt and flow out from composite plate, and final acquisition has the composite plate of ripple sandwich structure, as shown in Figure 8.
embodiment 2
The first step, is of a size of the die of 260mm × 260mm × 40mm with 321 stainless steels (1Cr8Ni9Ti) machining profile, die 1 is trapezoidal wave, and the wavelength of trapezoidal wave is 60mm, and wave amplitude is 30mm, for the manufacture of ripple laminboard layer;
Second step, 5083 flat aluminium alloy plates that will be of a size of 260mm × 260mm × 2.5mm are laid on die, then by be embossed on 5083 flat aluminium alloy plates;
3rd step, puts into heating furnace by the mould assembled, and carries out mechanical pressurization to patrix, to ensure sealing; Simultaneously by mold heated to 500-535 DEG C, pass into argon gas by the air inlet of patrix simultaneously, superplasticforming carried out to 5083 flat aluminium alloy plates, cooling after take out obtain 5083 aluminium alloy ripple laminboard layers;
4th step, soldering and sealing is carried out at the two ends of 5083 aluminium alloy ripple laminboard layer hollow parts after shaping, hollow parts afterwards directly to 5083 aluminium alloy ripple laminboard layers injects low-melting alloy, after cooling the soldering and sealing at two ends is cut off, form low-melting alloy plug, plug plays a supportive role when explosive welding;
5th step, 5083 aluminium alloy ripple laminboard layers and on 5083 aluminium alloy panel, explosive welding position between lower 5083 aluminium alloy panel (when namely 5083 aluminium alloy ripple laminboard layers are clipped in upper and lower panel centre and upper and lower panel contact site) spread emulsion; Then be clipped between upper and lower 5083 aluminium alloy panel, electricity consumption cap sensitive explosive realizes welding between upper and lower 5083 aluminium alloy panel with 5083 aluminium alloy ripple laminboard layers;
6th step, puts into water by composite plate after blast, and after being heated to water boiling, namely low-melting alloy plug can melt and flow out from composite plate, and final acquisition has the composite plate of ripple sandwich structure.
embodiment 3
The first step, is of a size of the die 1 of 260mm × 260mm × 40mm with 321 stainless steels (1Cr8Ni9Ti) machining profile, die 1 is square wave, and the wavelength of square wave is 60mm, and wave amplitude is 30mm, for the manufacture of ripple laminboard layer;
Second step, is laid in the TC4 titanium alloy plate being of a size of 260mm × 260mm × 1.5mm on die, then by be embossed on TC4 titanium alloy plate;
3rd step, puts into heating furnace by the mould assembled, and carries out mechanical pressurization to patrix, to ensure sealing; Simultaneously by mold heated to 900-920 DEG C, pass into argon gas by the air inlet of patrix simultaneously, superplasticforming carried out to TC4 titanium alloy plate, cooling after take out obtain TC4 titanium alloy ripple laminboard layer;
4th step, the plug of the carbon steel material identical with TC4 titanium alloy ripple laminboard layer bellows-shaped is gone out by machining, and at mandrel surface coating butter solder resist, be inserted into the hollow parts of TC4 titanium alloy ripple laminboard layer, plug plays a supportive role when explosive welding;
5th step, TC4 titanium alloy ripple laminboard layer and on 5083 aluminium alloy panel, explosive welding position between lower 5083 aluminium alloy panel (when namely TC4 titanium alloy ripple laminboard layer is clipped in upper and lower panel centre and upper and lower panel contact site) spread emulsion; Then be clipped between upper and lower 5083 aluminium alloy panel, electricity consumption cap sensitive explosive realizes welding between upper and lower 5083 aluminium alloy panel with TC4 titanium alloy ripple laminboard layer;
6th step, extracts the carbon steel plug in composite plate out, and final acquisition has the heterogeneous material composite plate of ripple sandwich structure.
embodiment 4
The first step, is of a size of the die 1 of 260mm × 260mm × 40mm with 321 stainless steels (1Cr8Ni9Ti) machining profile, die 1 is triangular waveform, and leg-of-mutton wavelength is 60mm, and wave amplitude is 30mm, for the manufacture of ripple laminboard layer;
Second step, is laid in the TC4 titanium alloy plate being of a size of 260mm × 260mm × 1.5mm on die, then by be embossed on TC4 titanium alloy plate;
3rd step, puts into heating furnace by the mould assembled, and carries out mechanical pressurization to patrix, to ensure sealing; Simultaneously by mold heated to 900-920 DEG C, pass into argon gas by the air inlet of patrix simultaneously, superplasticforming carried out to TC4 titanium alloy plate, cooling after take out obtain TC4 titanium alloy ripple laminboard layer;
4th step, the plug of the cross section carbon steel material identical with TC4 titanium alloy ripple laminboard layer bellows-shaped is gone out by machining, and at mandrel surface coating butter solder resist, be inserted into the hollow parts of TC4 titanium alloy ripple laminboard layer, plug plays a supportive role when explosive welding;
5th step, TC4 titanium alloy ripple laminboard layer and on 2124 aluminium alloy panel, explosive welding position between lower 5083 aluminium alloy panel (when namely TC4 titanium alloy ripple laminboard layer is clipped in upper and lower panel centre and upper and lower panel contact site) spread emulsion; Then be clipped between 2124 aluminium alloy panel, lower 5083 aluminium alloy panel, electricity consumption cap sensitive explosive realizes upper 2124 aluminium alloy panel, lower welding between 5083 aluminium alloy panel with TC4 titanium alloy ripple laminboard layer;
6th step, extracts the carbon steel plug in composite plate out, and final acquisition has the heterogeneous material composite plate of ripple sandwich structure.
Stainless steel die waveform in above-described embodiment can be selected according to actual needs or make other conversion between square wave, trapezoidal wave, triangular wave or sine wave.
The above is only the preferred embodiment of the present invention, it should be pointed out that for those skilled in the art, can also make some improvement under the premise without departing from the principles of the invention, and these improvement also should be considered as protection scope of the present invention.
Claims (5)
1. there is a preparation method for ripple layer sandwich structure composite plate, it is characterized in that comprising the following steps:
1) ripple laminboard layer, is prepared;
2) hollow parts, to ripple laminboard layer adds passive plug:
First preparation and die have the core rod mould of identical bellows-shaped; Secondly in core rod mould, pour into a mould low-melting alloy, after cooling, load the hollow parts of ripple laminboard layer as plug;
Or after soldering and sealing is carried out at the two ends of ripple laminboard layer hollow parts, the hollow parts to ripple laminboard layer injects low-melting alloy, after cooling as supporting plug;
3), ripple laminboard layer and the connection up and down between metal decking is realized by explosive welding;
4), take out after plug, obtain that there is ripple sandwich structure composite plate.
2. the preparation method with ripple layer sandwich structure composite plate according to claim 1, is characterized in that the preparation process of described ripple laminboard layer is:
1) die with square wave, trapezoidal wave, triangular wave or sine waveform, is processed into stainless steel;
2), by titanium alloy plate be laid on die, then by be embossed on titanium alloy plate;
3), the mould assembled is put into heating furnace, mechanical pressurization is carried out to patrix, guarantee sealing, and by mold heated to the superplastic forming temperature of titanium alloy, pass into argon gas by the air inlet of patrix simultaneously, superplasticforming is carried out to titanium alloy plate, after cooling, obtains titanium alloy ripple laminboard layer.
3. the preparation method with ripple layer sandwich structure composite plate according to claim 1, is characterized in that the preparation process of described ripple laminboard layer is:
1) die with square wave, trapezoidal wave, triangular wave or sine waveform, is processed into stainless steel;
2), by flat aluminium alloy plate be laid on die, then by be embossed on flat aluminium alloy plate;
3), the mould assembled is put into heating furnace, mechanical pressurization is carried out to patrix, guarantee sealing, and by mold heated to the superplastic forming temperature of aluminium alloy, pass into argon gas by the air inlet of patrix simultaneously, superplasticforming is carried out to aluminium horizontal sheet material, after cooling, obtains aluminium alloy ripple laminboard layer.
4. the preparation method with ripple layer sandwich structure composite plate according to any one of claims 1 to 3, is characterized in that described step 3) in blast process be:
1) connecting portion, between ripple laminboard layer and upper and lower panel spreads emulsion;
2), be clipped between upper and lower panel by ripple laminboard layer, ignition charge realizes welding.
5. the preparation method with ripple layer sandwich structure composite plate according to claim 4, is characterized in that: described upper and lower panel is titanium alloy sheet or aluminium alloy plate.
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| CN201410048716.9A CN103862233B (en) | 2014-02-12 | 2014-02-12 | There is the preparation method of ripple layer sandwich structure composite plate |
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| CN201410048716.9A CN103862233B (en) | 2014-02-12 | 2014-02-12 | There is the preparation method of ripple layer sandwich structure composite plate |
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| CN103862233B true CN103862233B (en) | 2016-04-27 |
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| CN104723579B (en) * | 2015-04-13 | 2017-03-22 | 哈尔滨工业大学 | Assembling mold for all-composite corrugated sandwich cylindrical shells |
| CN106881561A (en) * | 2015-12-15 | 2017-06-23 | 航天特种材料及工艺技术研究所 | A kind of preparation method of titanium alloy thin wall multilayer hollow structure |
| CN108160978A (en) * | 2018-02-09 | 2018-06-15 | 中国科学技术大学 | A kind of production method of high temperature impact resistance heat exchanger |
| CN108161210B (en) * | 2018-02-09 | 2023-10-20 | 中国科学技术大学 | Self-hardening filling type hollow structure explosion composite board and manufacturing method thereof |
| CN109318541B (en) * | 2018-09-13 | 2021-06-29 | 北京理工大学 | Bidirectional corrugated lattice reinforced composite material sandwich structure |
| CN113133270A (en) * | 2020-01-14 | 2021-07-16 | 航天海鹰(哈尔滨)钛业有限公司 | Confined space forced cooling system based on special-shaped diffusion welding water-cooling plate |
| CN114776747B (en) * | 2022-03-15 | 2023-09-22 | 东北大学 | Composite hyperbolic corrugated sandwich structure for inhibiting vibration of lubricating oil tank of aero-engine and application thereof |
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| JPS52129726A (en) * | 1976-04-25 | 1977-10-31 | Showa Gouhan Kk | Production method of inorganic corrugated composite board |
| JPH01245923A (en) * | 1988-03-25 | 1989-10-02 | Mitsubishi Heavy Ind Ltd | Controlling method for thickness distribution of superplastic forming parts |
| JPH06269961A (en) * | 1993-03-19 | 1994-09-27 | Yamaki Kogyo Kk | Production of composite material |
| CN1189284C (en) * | 2002-01-04 | 2005-02-16 | 大连理工大学 | Composite metal material explosion welding technology with shape protection function |
| CN2627424Y (en) * | 2003-01-09 | 2004-07-21 | 张志良 | Explosion-welded red copper plate tube solar heat collecting device |
| CN202826578U (en) * | 2012-08-29 | 2013-03-27 | 宁波红杉高新板业有限公司 | Corrugated core type composite board |
| CN103071908B (en) * | 2013-01-18 | 2014-11-12 | 中国人民解放军理工大学野战工程学院 | Explosive welding method of arranging multiple reinforcing ribs between large-area double-layer steel plates |
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