CN100546732C - The super plastic forming method of plate type heat converter special titanium plate - Google Patents
The super plastic forming method of plate type heat converter special titanium plate Download PDFInfo
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- CN100546732C CN100546732C CNB2007100461440A CN200710046144A CN100546732C CN 100546732 C CN100546732 C CN 100546732C CN B2007100461440 A CNB2007100461440 A CN B2007100461440A CN 200710046144 A CN200710046144 A CN 200710046144A CN 100546732 C CN100546732 C CN 100546732C
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- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims abstract description 51
- 239000010936 titanium Substances 0.000 title claims abstract description 35
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 35
- 238000000034 method Methods 0.000 title claims abstract description 16
- 239000000463 material Substances 0.000 claims abstract description 77
- 238000000137 annealing Methods 0.000 claims abstract description 31
- 238000010438 heat treatment Methods 0.000 claims abstract description 24
- 238000001291 vacuum drying Methods 0.000 claims abstract description 24
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 20
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 20
- 238000005097 cold rolling Methods 0.000 claims abstract description 13
- 238000005098 hot rolling Methods 0.000 claims abstract description 13
- 239000002994 raw material Substances 0.000 claims abstract description 12
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 11
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 11
- 238000003723 Smelting Methods 0.000 claims abstract description 10
- 229910052742 iron Inorganic materials 0.000 claims abstract description 10
- 238000002844 melting Methods 0.000 claims abstract description 10
- 230000008018 melting Effects 0.000 claims abstract description 10
- 239000001301 oxygen Substances 0.000 claims abstract description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 15
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 10
- 239000012535 impurity Substances 0.000 claims description 10
- 229910052739 hydrogen Inorganic materials 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 5
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 5
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 5
- 239000004411 aluminium Substances 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 239000001257 hydrogen Substances 0.000 claims description 5
- 229910052750 molybdenum Inorganic materials 0.000 claims description 5
- 239000011733 molybdenum Substances 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000010703 silicon Substances 0.000 claims description 5
- 229910052720 vanadium Inorganic materials 0.000 claims description 5
- 229910052725 zinc Inorganic materials 0.000 claims description 5
- 239000011701 zinc Substances 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- 239000003513 alkali Substances 0.000 claims description 4
- 238000005554 pickling Methods 0.000 claims description 4
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 claims 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims 1
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 abstract description 16
- 239000002253 acid Substances 0.000 abstract description 16
- 238000005516 engineering process Methods 0.000 abstract description 14
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 9
- 238000004140 cleaning Methods 0.000 abstract description 5
- 238000005242 forging Methods 0.000 abstract description 4
- 238000003825 pressing Methods 0.000 abstract description 4
- 238000003754 machining Methods 0.000 abstract description 3
- 238000005096 rolling process Methods 0.000 description 10
- 239000002131 composite material Substances 0.000 description 8
- 229910001069 Ti alloy Inorganic materials 0.000 description 7
- 229910010038 TiAl Inorganic materials 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 238000012545 processing Methods 0.000 description 6
- 238000002360 preparation method Methods 0.000 description 4
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 4
- 239000013078 crystal Substances 0.000 description 3
- 229910000765 intermetallic Inorganic materials 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 238000011056 performance test Methods 0.000 description 3
- 238000005070 sampling Methods 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 230000004927 fusion Effects 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 238000010009 beating Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 230000005764 inhibitory process Effects 0.000 description 1
- 230000003434 inspiratory effect Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000000399 orthopedic effect Effects 0.000 description 1
- 230000000505 pernicious effect Effects 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
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- Metal Rolling (AREA)
- Laminated Bodies (AREA)
Abstract
What the present invention relates to is the super plastic forming method of the plate type heat converter special titanium plate in a kind of Machining Technology field.Comprise the steps: 1. to select for use titanium sponge as the melting raw material; 2. titanium sponge is inserted the vacuum beam-plasma smelting furnace, direct pouring becomes slab; 3. through heating, hot rolling, soda acid wash, again heating, hot rolling again, soda acid wash, once annealing, form the thick sheet material of 2.0～2.4mm; 4. the thick sheet material of 2.0～2.4mm after vacuum drying oven annealing, cold rolling, cleaning, double annealing, more cold rolling, soda acid wash, three annealing, obtaining thickness at last is the titanium sheet material of 0.5～0.6mm.The titanium slab that the present invention adopts the higher titanium sponge that contains oxygen, iron, nitrogen amount directly to produce in the vacuum beam-plasma smelting furnace without forging and pressing, directly is rolled into the technology of plate.
Description
Technical field
What the present invention relates to is the super plastic forming method of the method in a kind of Machining Technology field, particularly a kind of plate type heat converter special titanium plate.
Background technology
At present, the superplasticforming of titanium alloy is global the recognized standard industrial technology.Superplasticity is meant that metal material under the strain rate of rational (height) forming temperature and (little) macroscopical constriction does not take place and produces the ability of very big plastic strain, and superplasticity has following requirement: deformation temperature should reach about half of fusion temperature; Rate of deformation must be low.Superplasticforming is exactly to utilize material to have the phenomenon of big plastic strain capacity under a certain certain conditions, and material is carried out machining deformation.For the trade mark is the titanium plate slab of GR1, and its plasticity has only 40～50% under the normal temperature, but reaches the half (being generally 900 ℃) of its fusion temperature in temperature, and its plasticity is easy to surpass 1000%.This numerical value is rolling for the titanium plate, greatly reduces draught pressure, has reduced rolling difficulty, and reduction in pass obtains increasing, and makes to add can reach same overall reduction (total deformation) by rolling pass still less man-hour.And the increase of each reduction in pass more can make crystal grain fully broken, and the properties of product of gained are more even.
For titanium sheet material, it is higher to process relatively difficulty and cost, is particularly adopting the traditional cold forming technique to make aspect the thin plate.And higher processing cost causes the application of titanium plate to be subjected to very big restriction.The 4th international advanced material superplasticity meeting of Osaka in 1991 descended a generic definition for superplasticity for the first time: superplasticity is meant that polycrystalline material presents the ability of high tensile elongation before inefficacy, have anisotropy usually.Experimental demonstration, nearly all polycrystalline material all presents high stretcher strain under suitable temperature and strain rate, prerequisite is that these materials can form enough tiny grain structure in the hot forming process, and shows the ability of sufficiently high inhibition grain growth.
Find Chinese patent application number by prior art documents: 200510009906, publication number: 1672918, denomination of invention: a kind of TiAl intermetallic compound-titanium alloy composite board and preparation method thereof.This technology readme: a kind of TiAl intermetallic compound-titanium alloy composite board and preparation method thereof, it relates to a kind of TiAl intermetallic compound-titanium alloy composite board and preparation technology thereof.Composite board of the present invention comprise at least one deck material be the sheet material (1) of TiAl intermetallic compound and at least one deck material be the sheet material (2) of pure titanium or titanium alloy, processing method is: be that the sheet material of TiAl intermetallic compound or bulk and material are the sheet material of pure titanium or titanium alloy or bulk polishes or polishing to material before rolling, adopt the pack rolling method to prepare composite board then, technological parameter is: 600～1400 ℃ of temperature, pass deformation 2～40%, rolling total deformation 5～95%.The composite board that the present invention obtains combines the lightweight of TiAl intermetallic compound, heat-resisting and titanium alloy is high-strength, plasticity is good advantage, the room temperature tensile strength of composite board is 550～950Mpa, temperature-room type plasticity is 2.5～5%, 700 ℃ of tensile strength are 500～700Mpa, and 700 ℃ of plasticity surpass 8%.The composite board of this technology preparation is to become a slice with the ply rolling of multi-disc plate, and its plasticity is changed the plasiticity index of special-purpose titanium plate again well below plate.
Also find Chinese patent application number in the retrieval: 200510089940, publication number: 1824409, the applying date: on August 8th, 2005, denomination of invention: external beating metal plate material high temperature ultrahigh water pressure once shaping technology, method and apparatus.Wherein manufacturing process is: a kind of huge inner high voltage that utilizes water at high temperature to be produced is a blank with sheet material, 1. with topped up with water in the high-pressure bottle; 2. sheet material is covered above the container; 3. the spill seal groove is alignd descending mould with male adapter; 4. screw screw, sheet material is sealed between high-pressure bottle and the mould; 5. the working water in the heating high-pressure container is to high temperature; 6. when surpassing the tension force that sheet material can bear by pressure that high-temperature water produced in the container, sheet material is to the female mold deep-drawing deformation, until consistent with the internal mold surface.This technology is difficult for from inside to outside carrying out deep-drawing deformation at tubular material, utilizing under the high temperature water can produce bigger pressure makes it that deep-drawing deformation take place, but one production line also can only be processed single part, and each part all needs just can finish through dress water, sealing, heating, distortion, cooling, dismounting, and step is complicated.Run into the product of different bores, also will redesign overcoat and sealing device, be unfavorable for processing polytype product to guarantee its sealing.
Summary of the invention
The objective of the invention is to overcome deficiency of the prior art, a kind of super plastic forming method of plate type heat converter special titanium plate is provided.Make its titanium slab that adopts the higher titanium sponge that contains oxygen, iron, nitrogen amount in the vacuum beam-plasma smelting furnace, directly to produce,, directly be rolled into the technology of plate without forging and pressing.
The present invention is achieved by the following technical solutions, the present invention includes following steps:
1. select for use titanium sponge as the melting raw material;
The component of described titanium sponge and mass percent: 0.05%≤iron≤0.08%, 0.05%≤oxygen≤0.08%, 0.008%≤nitrogen≤0.015%, 0＜carbon≤0.03%, 0＜hydrogen≤0.008%, other impurity content＜0.4%, surplus is a titanium.
Described other impurity is meant all common relict elements such as nickel, silicon, aluminium, vanadium, zinc, molybdenum, zirconium.
Described titanium sponge, HB is: 100～110.
2. titanium sponge is inserted the vacuum beam-plasma smelting furnace, direct pouring becomes slab;
The cuboid of described slab: H * B * L=220mm * 900mm * 1000mm or similar sizes.
3. through heating, hot rolling, soda acid wash, again heating, hot rolling again, soda acid wash, once annealing, form the thick sheet material of 2.0～2.4mm;
Described heating is meant: in the heating furnace heating, temperature is controlled at 900～920 ℃.
Described hot rolling is meant: the thick sheet material of 8～9mm is made in the slab hot rolling.
Described soda acid is washed, and heats in the alkali pot, and temperature is controlled at 440～500 ℃, peels off oxide skin through the quick-fried laggard pickling tube of water, and water cleans the back oven dry again.
Described heating again is meant: in the heating furnace heating, temperature is controlled at 800～850 ℃.
Described hot rolling again is meant: the sheet material that 8～9mm is thick hot rolling is again made the thick sheet material of 2.0～2.4mm.
Described once annealing is annealed in vacuum drying oven, and temperature and time is: 720 ℃ ± 10 ℃, and 1～2h.
4. the thick sheet material of 2.0～2.4mm after vacuum drying oven annealing, cold rolling, cleaning, double annealing, more cold rolling, soda acid wash, three annealing, obtaining thickness at last is the titanium sheet material of 0.5～0.6mm.
Described cold rolling, be meant: the sheet material that 2.0～2.4mm is thick is cold rolling, makes the thick sheet material of 1.0～1.2mm.
Described double annealing is meant: anneal in vacuum drying oven, temperature and time is: 720 ℃ ± 10 ℃, and 1h.
Described cold rolling again, be meant: the sheet material that 1.0～1.2mm is thick is cold rolling, makes the thick sheet material of 0.5～0.6mm.
Described three annealing are annealed in vacuum drying oven, and temperature and time is: 680～720 ℃, and 1～2h.
The raw material that the present invention relates to is the titanium slab that the higher titanium sponge that contains oxygen, iron, nitrogen amount that is easier at present to obtain is directly produced in the vacuum beam-plasma smelting furnace, without forging and pressing, directly is rolled into the technology of plate.The present invention adopts the hot rolling technology of aximal deformation value, in conjunction with vacuum annealing process repeatedly, make the crystal grain of metal material fully broken, obtain more tiny grain structure and crystal boundary more closely, and guarantee less temperature error, make the mechanical performance of material reach the requirement of superplasticforming, be convenient to the processing of slab.The present invention produces with less hot rolling and cold rolling number of times, reduce the heating number of times and the heat treated number of times of plate, reduce the inspiratory capacity of plate, reduce the generation of α layer, also adopt vacuum annealing to handle and reduce pernicious gas elements such as material processing is adsorbed through multi-pass H, O, N, reduce impurity content, guarantee product quality.Because the plate yield strength is higher under the normal temperature state, hot rolling is rolled plate thin as far as possible, reduce cold rolling total deformation, and guarantee the deflection of cold rolling one way, at last with the vacuum creep of annealing for three times to plate soften, orthopedic.
Beneficial effect of the present invention: at present, produce plate type heat converter special titanium plate in the world because the difficulty that grades of raw materials differ and melting is controlled, be difficult to produce in enormous quantities the titanium ingot of the low impurity of high-purity, thereby the production of plate type heat converter special titanium plate is restricted.The titanium slab that the present invention adopts the higher titanium sponge that contains oxygen, iron, nitrogen amount directly to produce in the vacuum beam-plasma smelting furnace without forging and pressing, directly is rolled into the technology of plate.Produce plate type heat converter special titanium plate, reduced requirement, increased the output of plate type heat converter special titanium plate greatly, improved productivity effect supplied materials.Use the present invention to produce plate type heat converter special titanium plate, improved 30%, and output is also increasing than the monthly output of using conventional method.The end properties index also all satisfies and is better than the standard that plate changes product.The superplasticity that the present invention utilizes material itself to have is carried out processing to it, greatly reduces the production difficulty, the reduction of ingredient requirement, and the simplification of difficulty of processing will inevitably make output increase substantially, and satisfies market demand.
The specific embodiment
Below embodiments of the invention are elaborated: present embodiment has provided detailed embodiment and process being to implement under the prerequisite with the technical solution of the present invention, but protection scope of the present invention is not limited to following embodiment.
Example 1
1, adopt titanium sponge as the melting raw material;
Its mass percent is respectively: oxygen=0.05%, iron=0.05%, nitrogen=0.01%, carbon=0.015%, hydrogen=0.005%, and other impurity nickel, silicon, aluminium, vanadium, zinc, molybdenum, zirconium content 0.39%, surplus is a titanium, HB=100.
2, direct pouring becomes slab after the melting of vacuum beam-plasma smelting furnace.
Slab specification: H * B * L=220mm * 900mm * 1000mm.
3, be heated to 900 ℃ in heating furnace, heating once and rolling becomes the thick sheet material of 8mm then.
4, the sheet material that 8mm is thick is washed, after the reconditioning, is heated to 820 ℃ through heating furnace again through soda acid, is hot-rolled down to the thick sheet material of 2.0mm.
5, the sheet material that 2.0mm is thick is washed, after the reconditioning, is annealed in vacuum drying oven through soda acid again.The annealing standard: 710 ℃, 2h.
6, the thick sheet material of 2.0mm after vacuum drying oven annealing is cold-rolled to the sheet material of 1.0mm.
7, the sheet material of 1.0mm carries out 710 ℃ in vacuum drying oven after oil removing, cleaning, 1h annealing.
8, the sheet material of the 1.0mm after vacuum drying oven annealing is cold-rolled to the sheet material of 0.5mm.
9, the sheet material that is cold-rolled to 0.5mm is annealed in vacuum drying oven after soda acid is washed, annealing: 700 ℃, and 100min.
Performance test is done in sampling to finished product, and the result is:
Example 2
1, adopt titanium sponge as the melting raw material;
Its mass percent is respectively: oxygen=0.08%, iron=0.08%, nitrogen=0.008%, carbon=0.03%, hydrogen=0.007%, and other impurity nickel, silicon, aluminium, vanadium, zinc, molybdenum, zirconium content 0.39%, surplus is a titanium.HB＝110。
2, direct pouring becomes slab after the melting of vacuum beam-plasma smelting furnace.
Slab specification: H * B * L=240mm * 900mm * 1000mm.
3, be heated to 920 ℃ in heating furnace, heating once and rolling becomes the thick sheet material of 9mm then.
4, the sheet material that 9mm is thick is washed, after the reconditioning, is heated to 830 ℃ through heating furnace again through soda acid, is hot-rolled down to the thick sheet material of 2.3mm.
5, the sheet material that 2.3mm is thick is washed, after the reconditioning, is annealed in vacuum drying oven through soda acid again, annealing: 720 ℃, and 2h.
6, the thick sheet material of 2.3mm after vacuum drying oven annealing is cold-rolled to the sheet material of 1.2mm.
7, the sheet material of 1.2mm carries out 710 ℃ in vacuum drying oven after oil removing, cleaning, 1h annealing.
8, the sheet material of the 1.2mm after vacuum drying oven annealing is cold-rolled to the sheet material of 0.6mm.
9, the sheet material that is cold-rolled to 0.6mm is annealed in vacuum drying oven after soda acid is washed, annealing: 710 ℃, and 2h.
Performance test is done in sampling to finished product, and the result is:
Example 3
1, adopt titanium sponge as the melting raw material;
Its mass percent is respectively: oxygen=0.07%, iron=0.06%, nitrogen=0.009%, carbon=0.02%, hydrogen=0.006%, and other impurity nickel, silicon, aluminium, vanadium, zinc, molybdenum, zirconium content 0.39%, surplus is a titanium.HB＝105。
2, direct pouring becomes slab after the melting of vacuum beam-plasma smelting furnace.
Slab specification: H * B * L=200mm * 900mm * 1000mm.
3, be heated to 900 ℃ in heating furnace, heating once and rolling becomes the thick sheet material of 8mm then.
4, the sheet material that 8mm is thick is washed, after the reconditioning, is heated to 800 ℃ through heating furnace again through soda acid, is hot-rolled down to the thick sheet material of 2.0mm.
5, the sheet material that 2.0mm is thick is washed, after the reconditioning, is annealed in vacuum drying oven through soda acid again.Annealing: 700 ℃, 2h.
6, the thick sheet material of 2.0mm after vacuum drying oven annealing is cold-rolled to the sheet material of 1.0mm.
7, the sheet material of 1.0mm carries out 690 ℃ in vacuum drying oven after oil removing, cleaning, 1h annealing.
8, the sheet material of the 1.0mm after vacuum drying oven annealing is cold-rolled to the sheet material of 0.5mm.
9, the sheet material that is cold-rolled to 0.5mm is annealed in vacuum drying oven after soda acid is washed, annealing: 700 ℃, and 100min.
Performance test is done in sampling to finished product, and the result is:
The APV GR1 standard of plate type heat converter special titanium plate:
Both can draw after relatively, and the end properties by embodiments of the invention production can reach or be better than the standard that plate changes product.If, can not reach this standard with same raw material and prior art production.Because the content of raw material iron, nitrogen, oxygen is higher, prior art is produced plate type heat converter special titanium plate must select the lower raw material of impurity content for use, has so not only increased cost, also can cause output not increase because of insufficient raw material.
Claims (3)
1, a kind of super plastic forming method of plate type heat converter special titanium plate is characterized in that, comprises the steps:
1. select for use titanium sponge as the melting raw material;
2. titanium sponge is inserted the vacuum beam-plasma smelting furnace, direct pouring becomes slab; This slab is: highly * and the cuboid of width * length=220mm * 900mm * 1000mm;
3. at first in heating furnace temperature being controlled at 900～920 ℃ heats, and the slab hot rolling made the thick sheet material of 8～9mm, in the alkali pot, heat again, and temperature is controlled at 440～500 ℃, peel off oxide skin through the quick-fried laggard pickling tube of water, water cleans the back oven dry again;
In heating furnace temperature being controlled at 800～850 ℃ then heats again, and the sheet material that 8～9mm is thick again hot rolling make the thick sheet material of 2.0～2.4mm, in the alkali pot, heat again, and temperature be controlled at 440～500 ℃, peel off oxide skin through the quick-fried laggard pickling tube of water, water cleans the back oven dry again;
Anneal in vacuum drying oven at last, temperature and time is: 720 ℃ ± 10 ℃, 1～2 hour, form the thick sheet material of 2.0～2.4mm;
4. the sheet material that 2.0～2.4mm after vacuum drying oven annealing is thick is cold rolling makes the thick sheet material of 1.0～1.2mm and cleans;
Carry out the annealing second time then in vacuum drying oven, temperature and time is: 720 ℃ ± 10 ℃, and 1 hour, and the cold rolling thick sheet material of 0.5～0.6mm of making, in the alkali pot, heat, and temperature is controlled at 440～500 ℃, peel off oxide skin through the quick-fried laggard pickling tube of water, water cleans the back oven dry again;
Anneal for the third time in vacuum drying oven, temperature and time is again: 680～720 ℃, 1～2 hour, obtaining thickness at last was the titanium sheet material of 0.5～0.6mm.
2, the super plastic forming method of plate type heat converter special titanium plate according to claim 1, it is characterized in that, the component of described titanium sponge and mass percent: 0.05%≤iron≤0.08%, 0.05%≤oxygen≤0.08%, 0.008%≤nitrogen≤0.015%, 0＜carbon≤0.03%, 0＜hydrogen≤0.008%, other impurity content＜0.4%, surplus are titanium.
3, the super plastic forming method of plate type heat converter special titanium plate according to claim 2 is characterized in that, described other impurity is meant nickel, silicon, aluminium, vanadium, zinc, molybdenum, zirconium relict element.
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| CN104152746B (en) * | 2014-08-26 | 2016-06-08 | 攀钢集团攀枝花钢铁研究院有限公司 | Improve the production technology of titanium plate longitudinal direction plastic strain ratio |
| CN105179299B (en) * | 2015-09-15 | 2018-09-04 | 宁波龙旋机械制造有限公司 | A kind of fan coupler compound film sheet group and preparation method thereof |
| CN106392483B (en) * | 2016-11-07 | 2019-06-28 | 南昌专腾科技有限公司 | A kind of manufacturing process and system of compound titanium plate |
| CN106637016A (en) * | 2016-12-29 | 2017-05-10 | 广东技术师范学院 | Manufacturing method for producing industrial titanium plate by adoption of 2800-millimeter heavy and medium plate mill |
| CN106636747B (en) * | 2016-12-29 | 2018-06-05 | 广东技术师范学院 | A kind of manufacturing method using heavy and medium plate mill double annealing production technical pure titanium plate |
| CN107723638B (en) * | 2017-09-08 | 2019-09-06 | 洛阳双瑞精铸钛业有限公司 | A kind of preparation method of deep-draw titanium plate |
| CN107604281B (en) * | 2017-09-18 | 2019-04-26 | 南昌航空大学 | A method of improving TC4 titanium alloy plate low temperature superplasticity |
| CN107576216A (en) * | 2017-09-28 | 2018-01-12 | 江苏众众热能科技有限公司 | A kind of heat-exchangers of the plate type titanium plate |
| TWI675709B (en) * | 2018-12-04 | 2019-11-01 | 中國鋼鐵股份有限公司 | Method for manufacturing titanium sheet with excellent formability |
| CN113714286B (en) * | 2021-08-31 | 2022-07-05 | 西北有色金属研究院 | Preparation method of TA15 titanium alloy thin strip |
-
2007
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