Detailed description of preferred embodiments
Systematic study work shows: people can realize the optimum allocation of these elements in austenite and ferrite by well balanced composite component Cr, Mo, Ni, N, Mn and Co, this just can realize a kind of very corrosion-resistant material, and only has it measure negligible σ phase in this material.Described material has also obtained good workability, and this makes it possible to extrusion molding is weldless steel tube.This work also shows, in order to obtain the combination of high corrosion resistance and satisfactory texture stability, need carry out narrower combination to alloying element in this material in the present invention.Alloy according to the present invention includes (wt%):
C at the most 0.03%
Si at the most 0.5%
Mn?????????????????0-3.0%
Cr?????????????????24.0-30.0%
Ni?????????????????4.9-10.0%
Mo?????????????????3.0-5.0%
N??????????????????0.28-0.5%
B??????????????????0-0.0030%
S at the most 0.010%
Co?????????????????0-3.5%
W??????????????????0-3.0%
Cu?????????????????0-2.0%
Ru?????????????????0-0.3%
Al?????????????????0-0.03%
Ca?????????????????0-0.010%
Equal amount Fe and normal impurity and the additive that occurs, wherein ferritic volumn concentration is 40-65%.
Carbon (C) solubleness in ferrite and austenite is limited.Limited solubleness means the danger that has chromium carbide to separate out, so the content of carbon can not surpass 0.03wt%, preferably is no more than 0.02wt%.
Silicon (Si) is used as reductive agent in steel production, it has improved flowability in production and welding process simultaneously.But the intermetallic phase that the Si too high levels can cause not expecting to have is separated out, so the content of Si 0.5wt% at the most, preferably is no more than 0.3wt%.
Manganese (Mn) adds the solubleness that is used for improving N in the material, and still verified, Mn is limited to the influence of N solubleness in the alloy of described type.On the contrary, found other element higher to the influence of this solubleness.In addition, Mn combines meeting with high-load S and causes forming manganese sulfide, and this is as the starting point of tubercular corrosion, so the content of Mn should be limited in being preferably 0.5-1.2wt% between the 0-3.0wt%.
Chromium (Cr) is a kind of quite useful element, can improve the resistibility to most of form of corrosion.In addition, high-load chromium means can obtain extraordinary N solubleness in material.Therefore require to make Cr content to keep high as far as possible so that improve corrosion resistance.The chromium content that corrosion resistance is good should reach 24.0wt% at least, is preferably 27.0-29.0wt%.But high-load chromium can increase the danger of intermetallic precipitate, the content of chromium must be limited in the 30wt% for this reason.
Nickel (Ni) is used as the austenite stable element, adds the ferrite that an amount of nickel can also obtain desired content.For in volume percent being obtains desired austenite mutually and the ratio between the ferritic phase in the ferrite of 40-65%, need to add 4.9-10.0wt%, be preferably the nickel of 4.9-8.0wt%.
Aluminium (Mo) is a kind of useful element, and it can improve the corrosion resistance in chloride environment and reductive acid environment.Too high-load Mo can combine with high-load Cr, this means that the danger that produces the intermetallic precipitate increases, and Mo content in the present invention should be preferably 3.6-4.7wt% in the scope of 3.0-5.0wt%, especially be 4.0-4.3wt%.
Nitrogen (N) is very useful element, and it can improve erosion resistance, structural stability and the intensity of material.In addition, high-load N can improve the austenitic recovery in welding back, and this has given good performance in solder joint.More obvious for the effect that makes N, should add 0.28% N at least.Under N content condition with higher, especially when the content while of chromium was also very high, the danger that produces the chromium nitride precipitate increased, in addition, because N excessive dissolution in melting, so high N content means that porous danger occurring increases.Therefore, N content should be restricted to 0.5wt% at the most, the preferred N that adds greater than 0.35-0.45wt%.
Boron (B) is to add the hot workability that is used for improving material.Under the too high situation of B content, erosion resistance and weldability meeting variation, therefore, B content should be restricted to 0.0030wt%.
Sulphur (S) has a negative impact to erosion resistance by forming soluble sulfide, and in addition, therefore the hot workability variation is restricted to S content and is no more than 0.010wt%.
Cobalt (Co) adding is used at first improving erosion resistance and structural stability.Co is a kind of austenite stable element.In order to produce useful effect, the content of Co should be at least 0.5wt%, preferably is at least 1.5wt%.Because Co is relatively costly element, therefore the addition with cobalt is restricted to 3.5wt% at the most.
TungstenCan improve anti-spot corrosion and crevice corrosion performance, but the Cr of the tungsten that adds too high amount and high level and Mo combine and mean the danger increase that the intermetallic precipitate occurs.W content in the present invention should be preferably between the 0.5-1.8wt% in the 0-3.0wt% scope.
CopperAdd and to be used for improving at the sour environment general corrosion resistance in the sulfuric acid for example.Cu can influence stability of structure simultaneously.But high-load Cu means will surpass solid solubility, and therefore, Cu content should be restricted to 2.0wt% at the most, is preferably at 0.5-1.5wt%.
Ruthenium (Ru) adds and to be used for improving erosion resistance, because ruthenium is very expensive element, so content should be limited in 0.3wt% at the most, is preferably 0-0.1wt%.
Aluminium (Al) and calcium (Ca) are used as reductor in product made from steel, the content of Al should be limited in 0.03wt% scope at the most the formation with the restriction nitride.Ca can produce useful effect to hot ductility, and still, the content of Ca should be restricted to 0.010wt% to avoid occurring undesirable slag inclusion.
In order to obtain favorable mechanical performance, corrosion resistance and good weldability energy, ferritic content is extremely important.Consider that from the angle of erosion resistance and weldability the ferrite content of 40-65% is an ideal for obtaining superperformance.In addition, high-load ferrite means shock strength and the brittle resistibility deterioration to being caused by hydrogen at low temperatures, and therefore, ferritic volume percent content is 40-65%, is preferably 42-60%, especially is 45-55%.
In the following embodiments, provided the component of many test samples, these embodiment have illustrated the effect of different-alloy element on performance.Sample 605182 is represented one with reference to component, is not the part in field of the present invention therefore.Remaining sample should not thought to limit the invention, also should only not only limit to the embodiment of these samples, these embodiment have set forth the present invention who limits according to claim.
Although there be not clear and definite mentioning, always specific PRE number or value are considered to calculate according to the PREW formula.
Embodiment 1
The test sample of this embodiment is produced by following steps: cast out the steel ingot that weight is 170kg in the laboratory, subsequently its forge hot is become round steel.They are hot extruded into bar (band steel and round steel), wherein from these round steel, choose test materials.In addition, band steel is annealed before cold rolling carrying out, obtain other experiment material subsequently.Consider that from the material engineering angle described process can be taken as the representative of more scale operation, for example produces stainless steel tube by extrusion method, carries out cold rolling afterwards.Table 1 demonstrates the component of first experimental sample.
The composition of table 1 experimental sample, wt%
Sample | ????Mn | ?????Cr | ????Ni | ????Mo | ????W | ????Co | ????V | ????La | ????Ti | ????N |
???605193 | ???1.03 | ????27.90 | ???8.80 | ???4.00 | ???0.01 | ???0.02 | ???0.04 | ???0.01 | ???0.01 | ???0.36 |
???605195 | ???0.97 | ????27.90 | ???9.80 | ???4.00 | ???0.01 | ???0.97 | ???0.55 | ???0.01 | ???0.35 | ???0.48 |
???605197 | ???1.07 | ????28.40 | ???8.00 | ???4.00 | ???1.00 | ???1.01 | ???0.04 | ???0.01 | ???0.01 | ???0.44 |
???605178 | ???0.91 | ????27.94 | ???7.26 | ???4.01 | ???0.99 | ???0.10 | ???0.07 | ???0.01 | ???0.03 | ???0.44 |
???605183 | ???1.02 | ????28.71 | ???6.49 | ???4.03 | ???0.01 | ???0.03 | ???0.54 | ???0.01 | ???0.01 | ???0.28 |
???605184 | ???0.99 | ????28.09 | ???7.83 | ???4.01 | ???0.01 | ???0.03 | ???0.54 | ???0.01 | ???0.01 | ???0.44 |
???605187 | ???2.94 | ????27.74 | ???4.93 | ???3.98 | ???0.01 | ???0.98 | ???0.06 | ???0.01 | ???0.01 | ???0.44 |
???605153 | ???2.78 | ????27.85 | ???6.93 | ???4.03 | ???1.01 | ???0.02 | ???0.06 | ???0.02 | ???0.01 | ???0.34 |
???605182 | ???0.17 | ????23.48 | ???7.88 | ???5.75 | ???0.01 | ???0.05 | ???0.04 | ???0.01 | ???0.10 | ???0.26 |
In order to study the structural stability of sample, the described sample of choosing from each sample is annealed for going forward one by one with 50 ℃ under 900-1150 ℃ respectively, subsequently respectively at air or quenching-in water.Under a minimum temperature, form intermetallic phase.By in opticmicroscope, studying to determine the intermetallic phase negligible minimum temperature that becomes.Afterwards under described temperature to from the fresh sample of respective samples annealing constant temperature 5 minutes, with 140 ℃/minute constant speed of cooling these samples are cooled to room temperature afterwards, form the area part that the digital scanning picture is determined σ phase in these materials with back scattered electron subsequently under scanning electronic microscope, the result is as shown in table 2.
T
Maxσ is calculated by Thermo-Calc (the TC type N thermodynamic data storehouse of TCFE99 steel) according to the eigenwert of all element-specific in different variablees.T
Maxσ is the solvent temperature of σ phase, and high solvent temperature is represented lower structural stability.
Table 2
Sample | Thermal treatment | σ content (Vol%) | ???T
maxσ
|
???605193 | 1100 ℃, 5 minutes | ?????7.5% | ????1016 |
???605195 | 1150 ℃, 5 minutes | ?????32% | ????1047 |
???605197 | 1100 ℃, 5 minutes | ?????18% | ????1061 |
???605178 | 1100 ℃, 5 minutes | ?????14% | ????1038 |
???605183 | 1050 ℃, 5 minutes | ?????0.4% | ?????997 |
???605184 | 1100 ℃, 5 minutes | ?????0.4% | ?????999 |
???605187 | 1050 ℃, 5 minutes | ?????0.3% | ?????962 |
???605153 | 1100 ℃, 5 minutes | ?????3.5% | ????1032 |
???605182 | 1100 ℃, 5 minutes | ?????2.0% | ????1028 |
The purpose of this research is can be according to structural stability with the material classification, and promptly this is not the σ real content mutually in the sample of Overheating Treatment and quenching before corrosion test for example.The T that calculates by Thermo-Calc as can be seen
Maxσ does not have directly consistent with the σ phasor that measures, but obviously has the minimum T that calculates
MaxThe experimental sample of σ includes the σ phase of the minimum quantity in this experimentation.
Carry out the classification experiment of spot corrosion performance in so-called " Green Death " solution, described solution comprises 1% FeCl
3, 1% CuCl
2, 11% H
2SO
4With 1.2% HCl.Experimental procedure is with identical according to the spot corrosion of ASTM G48C experiment, but it finishes in more acrid " Green Death ", and in addition, some samples are according to ASTM G48C experimentize (each sample carries out 2 experiments).Also in containing 3%NaCl, carry out electrochemistry experiment (each sample carries out 6 experiments).The result of critical pitting temperature (CPT) form that draws from all experiments is as shown in table 3, for example for whole compositions and austenite, ferritic PREW value (Cr+3.3 (Mo+0.5W)+16N) in the alloy.Symbol is represented ferrite, and γ represents austenite.
Table 3
Sample | ???PRE
α | ???PRE
γ | ????PRE
γ??????/PRE
α | ???PRE | The ASTM G48C Green death of CPT ℃ of correction | ?????CPT℃ ????????ASTM?G48C ????6%FeCl
3 | ???CPT℃ ????????3% ????NaCl |
??605193 | ???51.3 | ???49.0 | ???0.9552 | ??46.9 | ???????90/90 | | ????64 |
??605195 | ???51.5 | ???48.9 | ???0.9495 | ??48.7 | ???????90/90 | | ????95 |
??605197 | ???53.3 | ???53.7 | ???1.0075 | ??50.3 | ???????90/90 | ??????>95 | ???>95 |
??605178 | ???50.7 | ???52.5 | ???1.0355 | ??49.8 | ???????75/80 | | ????94 |
??905183 | ???48.9 | ???48.9 | ???1.0000 | ??46.5 | ???????85/85 | ???????90 | ????93 |
??605184 | ???48.9 | ???51.7 | ???1.0573 | ??48.3 | ???????80/80 | | ????72 |
??605187 | ???48.0 | ???54.4 | ???1.1333 | ??48.0 | ???????70/75 | | ????77 |
??605182 | ???54.4 | ???46.2 | ???0.8493 | ??46.6 | ???????75/70 | ???????85 | ????62 |
??654SMO | | | | | ???????90/85 | | |
??SAF2507 | | | | | ???????70/70 | | |
??SAF2609 | | | | | ???????60/50 | | |
People determine to have linear scaling between minimum PRE value in duplex stainless steel austenite or the ferrite and the CPT value, can not be used for explaining the CPT value separately but the result in the table 3 shows the PRE value.Fig. 1 shows the CPT value that is obtained through the ASTM G48C experiment of revising in the mode of chart.Comprise dual phase steel SAF2507, SAF2906 and high alloy austenitic steel 654SMO as a reference.Can know from these results and see that all experiment materials demonstrate than SAF2507 and the better CPT value of SAF2906 in through the ASTM G48C experiment of revising.In addition, some experiment materials demonstrate with 654SMO in through the ASTM G48C experiment of revising and are equal to or better CPT result.Although utilize the cobalt-base alloy change experimental sample 605183 it include High Content Chromium and molybdenum, under controlled rate of cooling (140 ℃/minute), demonstrate good structural stability, and demonstrate the result who is better than SAF2507 and SAF2906.Studies show that a higher PRE value can not be used for explaining separately the CPT value, under the situation that should not concern, PRE
Austenite/ PRE
FerritePerformance for more heavy alloyed duplex stainless steel is vital, need between alloying element, carry out tight and accurately balanced so that obtain the optimization ratio, described ratio should be preferably 0.9-1.05 between 0.9-1.15, also be convenient to obtain to be higher than 46 PRE value simultaneously.In table 3, provided at the PRE that concerns through the CPT value of the sample in the ASTM G48C experiment of revising
Austenite/ PRE
Ferrite
Determine intensity and the shock strength under room temperature (RT) of all samples under room temperature (RT), 100 ℃ and 200 ℃, and represent with the mean value of 3 experiments.
Produce stretching experiment sample (DR-5C50) by φ 20mm extrusion bar, under according to the temperature of table 2, these samples are carried out thermal treatment in 20 minutes, cooling (specimen coding is respectively 605195,605197,605184) in air or water subsequently.Experimental result is shown in table 4 and table 5.The result of these stretching experiments shows that chromium, nitrogen and tungsten are very big to the shock strength influence of material.Except that 605153, it is 25% requirement that all samples have all satisfied under room temperature (RT) under tension test unit elongation.
Table 4 shock strength
Sample | Temperature | ??R
p0.2 | ?????R
p1.0 | ?????R
m | ????A5 | ????Z |
| | ??(MPa) | ?????(MPa) | ????(MPa) | ???(%) | ???(%) |
???605193 | ????RT | ???652 | ??????791 | ?????916 | ???29.7 | ????38 |
| ???100℃ | ???513 | ??????646 | ?????818 | ???30.4 | ????36 |
| ???200℃ | ???511 | ??????583 | ?????756 | ???29.8 | ????36 |
???605195 | ????RT | ???671 | ??????773 | ?????910 | ???38.0 | ????66 |
| ???100℃ | ???563 | ??????637 | ?????825 | ???39.3 | ????68 |
| ???200℃ | ???504 | ??????563 | ?????769 | ???38.1 | ????64 |
???605197 | ????RT | ???701 | ??????799 | ?????939 | ???38.4 | ????66 |
| ???100℃ | ???564 | ??????652 | ?????844 | ???40.7 | ????69 |
| ???200℃ | ???502 | ??????577 | ?????802 | ???35.0 | ????65 |
???605178 | ????RT | ???712 | ??????828 | ?????925 | ???27.0 | ????37 |
| ???100℃ | ???596 | ??????677 | ?????829 | ???31.9 | ????45 |
| ???200℃ | ???535 | ??????608 | ?????763 | ???27.1 | ????36 |
???605183 | ????RT | ???677 | ??????775 | ?????882 | ???32.4 | ????67 |
| ???100℃ | ???560 | ??????642 | ?????788 | ???33.0 | ????59 |
| ???200℃ | ???499 | ??????578 | ?????737 | ???29.9 | ????52 |
???605184 | ????RT | ???702 | ??????793 | ?????915 | ???32.5 | ????60 |
| ???100℃ | ???569 | ??????657 | ?????821 | ???34.5 | ????61 |
| ???200℃ | ???526 | ??????581 | ?????774 | ???31.6 | ????56 |
???605187 | ????RT | ???679 | ??????777 | ?????893 | ???35.7 | ????61 |
| ???100℃ | ???513 | ??????628 | ?????799 | ???38.9 | ????64 |
| ???200℃ | ???505 | ??????558 | ?????743 | ???35.8 | ????58 |
???605153 | ????RT | ???715 | ??????845 | ?????917 | ???20.7 | ????24 |
| ???100℃ | ???572 | ??????692 | ?????817 | ???29.3 | ????27 |
| ???200℃ | ???532 | ??????611 | ?????749 | ???23.7 | ????31 |
???605182 | ????RT | ???627 | ??????754 | ?????903 | ???28.4 | ????43 |
| ???100℃ | ???493 | ??????621 | ?????802 | ???31.8 | ????42 |
Table 5 shock strength
Sample | Annealing [℃/minute] | Cooling | Shock strength [J] | Annealing [℃/minute] | Cooling | Shock strength [J] |
??605193 | ????1100/20 | Air | ????35 | ????1100/20 | Water | ????242 |
??605195 | ????1150/20 | Water | ????223 | | | |
??605197 | ????1100/20 | Water | ????254 | ????1130/20 | Water | ????259 |
??605178 | ????1100/20 | Air | ????62 | ????1100/20 | Water | ????234 |
??905183 | ????1050/20 | Air | ????79 | ????1050/20 | Water | ????244 |
??605184 | ????1100/20 | Water | ????81 | ????1100/20 | Air | ????78 |
??605187 | ????1050/20 | Air | ????51 | ????1100/20 | Water | ????95 |
??605153 | ????1100/20 | Air | ????50 | ????1100/20 | Water | ????246 |
??605182 | ????1100/20 | Air | ????22 | ????1100/20 | Water | ????324 |
This research shows that most clearly shrend is absolutely necessary for obtaining best structure and therefore obtaining good shock strength numerical value.Except that 605184 and 605187, all samples have at room temperature all passed through the intensity of essential 100J, and the former is also very near required value certainly.
Fig. 6 demonstrates from the result that tungsten-rare gas element remelting experiment (hereinafter to be referred as TIG) draws, and wherein (Heat AffectedZone is hereinafter to be referred as HAZ) demonstrates good structure to sample 605193,605183,605184 and 605253 in the heat affected zone.The sample that contains Ti demonstrates in HAZ has TiN.Too high chromium and nitrogen content cause Cr
2N separates out, because this can make the degradation of this material, thereby should avoid occurring this situation.
Table 6
Sample | Precipitate protection gas Ar (99.99%) |
???605193 | HAZ: good |
???605195 | HAZ: a large amount of TiN and σ are mutually |
???605197 | HAZ: contain a spot of Cr in the δ crystal grain
2N, few
|
???605178 | HAZ: the Cr that contains in the δ crystal grain
2N, other are good
|
???605183 | HAZ: good |
???605184 | HAZ: good |
???605187 | ?HAZ:Cr
2N approaches the melted join thing, and further precipitation does not produce
|
???605153 | HAZ: good |
???605182 | HAZ:TiN and crystal boundary δ/δ with decorative pattern |
Embodiment 2
In the following embodiments, provided the component of other test sample of producing in order to find optimal component.From the result shown in the embodiment 1, from the performance of sample, begin these samples are changed with satisfactory texture stability and high corrosion resistance.All samples in the table 7 have comprised component of the present invention, and the sample that wherein is numbered 1-8 number includes only the statistical test pattern, and are numbered the alloy that has added in e-n number the sample in the scope of the present invention.
Described sample becomes round steel to obtain by the steel ingot of 270kg by casting, forge hot.With these round steel extrusion moldings is bar, thereby chooses test sample.Before cold rolling one-tenth band steel, bar is annealed afterwards, choose further test material afterwards.Table 7 demonstrates the component of these test samples.
Table 7
| Sample | ?????Mn | ????Cr | ????Ni | ?????Mo | ????W | ????Co | ????Cu | ????Ru | ??????B | ?????N |
???1 | ???605258 | ????1.1 | ???29.0 | ???6.5 | ????4.23 | | ????1.5 | | | ????0.0018 | ???0.46 |
???2 | ???605249 | ????1.0 | ???28.8 | ???7.0 | ????4.23 | | ????1.5 | | | ????0.0026 | ???0.38 |
???3 | ???605259 | ????1.1 | ???29.0 | ???6.8 | ????4.23 | | ????0.6 | | | ????0.0019 | ???0.45 |
???4 | ???605260 | ????1.1 | ???27.5 | ???5.9 | ????4.22 | | ????1.5 | | | ????0.0020 | ???0.44 |
???5 | ???605250 | ????1.1 | ???28.8 | ???7.6 | ????4.24 | | ????0.6 | | | ????0.0019 | ???0.40 |
???6 | ???605251 | ????1.0 | ???28.1 | ???6.5 | ????4.24 | | ????1.5 | | | ????0.0021 | ???0.38 |
???7 | ???605261 | ????1.0 | ???27.8 | ???6.1 | ????4.22 | | ????0.6 | | | ????0.0021 | ???0.43 |
???8 | ???605252 | ????1.1 | ???28.4 | ???6.9 | ????4.23 | | ????0.5 | | | ????0.0018 | ???0.37 |
???e | ???605254 | ????1.1 | ???26.9 | ???6.5 | ????4.8 | | ????1.0 | | | ????0.0021 | ???0.38 |
???f | ???605255 | ????1.0 | ???28.6 | ???6.5 | ????4.0 | | ????3.0 | | | ????0.0020 | ???0.31 |
???g | ???605262 | ????2.7 | ???27.6 | ???6.9 | ????3.9 | ????1.0 | ????1.0 | | | ????0.0019 | ???0.36 |
???h | ???605263 | ????1.0 | ???28.7 | ???6.6 | ????4.0 | ????1.0 | ????1.0 | | | ????0.0020 | ???0.40 |
???i | ???605253 | ????1.0 | ???28.8 | ???7.0 | ????4.16 | | ????1.5 | | | ????0.0019 | ???0.37 |
???j | ???605266 | ????1.1 | ???30.0 | ???7.1 | ????4.02 | | | | | ????0.0018 | ???0.38 |
???k | ???605269 | ????1.0 | ???28.5 | ???7.0 | ????3.97 | ????1.0 | ????1.0 | | | ????0.0020 | ???0.45 |
???l | ???605268 | ????1.1 | ???28.2 | ???6.6 | ????4.0 | ????1.0 | ????1.0 | ????1.0 | | ????0.0021 | ???0.43 |
???m | ???605270 | ????1.0 | ???28.8 | ???7.0 | ????4.2 | | ????1.5 | | ????0.1 | ????0.0021 | ???0.41 |
???n | ???605267 | ????1.1 | ???29.3 | ???6.5 | ????4.23 | | | ????1.5 | | ????0.0019 | ???0.38 |
Table 8.Thermo-Calc
Variable | α formula empirical value | ?αT-C | Whole PRE | ???PRE
α | ???PRE
γ | ??T
maxσ
| ?T
maxCr
2N
|
???1 | ????46 | ???50 | ???50.2 | ???47.8 | ???50.5 | ???1006 | ???1123 |
???2 | ????52 | ???50 | ???49.1 | ???48.4 | ???49.8 | ???1019 | ???1084 |
???3 | ????45 | ???50 | ???50.2 | ???47.9 | ???52.6 | ???1007 | ???1097 |
???4 | ????46 | ???50 | ???49.2 | ???46.5 | ???49.8 | ????986 | ???1121 |
???5 | ????47 | ???50 | ???49.1 | ???48.5 | ???49.7 | ???1028 | ???1038 |
???6 | ????52 | ???50 | ???48.1 | ???47.1 | ???49.2 | ????998 | ???1086 |
???7 | ????44 | ???50 | ???49.2 | ???46.6 | ???52.0 | ????985 | ???1081 |
???8 | ????46 | ???50 | ???48.1 | ???47.2 | ???49.1 | ???1008 | ???1044 |
???e | ????46 | ???53 | ???49.3 | ???48.4 | ???49.5 | ???1010 | ???1099 |
???f | ????65 | ???52 | ???46.7 | ???47.2 | ???46.1 | ???1008 | ???1090 |
???g | ????48 | ???51 | ???48.4 | ???48.4 | ???48.3 | ???1039 | ????979 |
???h | ????50 | ???53 | ???50.0 | ???48.4 | ???51.7 | ???1035 | ???1087 |
???i | ????52 | ???50 | ???49.1 | ???48.4 | ???49.8 | ???1019 | ???1084 |
Thermo-Calc value according to table 8 (the TC type N thermodynamic data storehouse of TCFE99 steel) is based on the characteristic quantity of all element-specific in different variablees.Ferrite and austenitic PRE value are based on they balanced components under 1100 ℃.T
Maxσ is the solvent temperature of σ phase, and high solvent temperature means lower structural stability.
Utilize microprobe analysis to alloying element the distribution in ferrite and austenite study, the result is as shown in table 9.
Table 9
Sample | Crystalline phase | ???Cr | ???Mn | ??Ni | ???Mo | ?W | ???Co | ??Cu | ???N |
?605258 | Ferrite | ??29.8 | ??1.3 | ??4.8 | ??5.0 | | ???1.4 | | ??0.11 |
| Austenite | ??28.3 | ??1.4 | ??7.3 | ??3.4 | | ???1.5 | | ??0.60 |
?605249 | Ferrite | ??29.8 | ??1.1 | ??5.4 | ??5.1 | | ???1.3 | | ??0.10 |
| Austenite | ???27.3 | ????1.2 | ???7.9 | ????3.3 | | ????1.6 | | ???0.53 |
??605259 | Ferrite | ???29.7 | ????1.3 | ???5.3 | ????5.3 | | ????0.5 | | ???0.10 |
| Austenite | ???28.1 | ????1.4 | ???7.8 | ????3.3 | | ???0.58 | | ???0.59 |
??605260 | Ferrite | ???28.4 | ????1.3 | ???4.4 | ????5.0 | | ????1.4 | | ???0.08 |
| Austenite | ???26.5 | ????1.4 | ???6.3 | ????3.6 | | ????1.5 | | ???0.54 |
??605250 | Ferrite | ???30.1 | ????1.3 | ???5.6 | ????5.1 | | ???0.46 | | ???0.07 |
| Austenite | ???27.3 | ????1.4 | ???8.8 | ????3.4 | | ???0.53 | | ???0.52 |
??605251 | Ferrite | ???29.6 | ????1.2 | ???5.0 | ????5.2 | | ????1.3 | | ???0.08 |
| Austenite | ???26.9 | ????1.3 | ???7.6 | ????3.5 | | ????1.5 | | ???0.53 |
??605261 | Ferrite | ???28.0 | ????1.2 | ???4.5 | ????4.9 | | ???0.45 | | ???0.07 |
| Austenite | ???26.5 | ????1.4 | ???6.9 | ????3.3 | | ???0.56 | | ???0.56 |
??605252 | Ferrite | ???29.6 | ????1.3 | ???5.3 | ????5.2 | | ???0.42 | | ???0.09 |
| Austenite | ???27.1 | ????1.4 | ???8.2 | ????3.3 | | ???0.51 | | ???0.48 |
??605254 | Ferrite | ???28.1 | ????1.3 | ???4.9 | ????5.8 | | ???0.89 | | ???0.08 |
| Austenite | ???26.0 | ????1.4 | ???7.6 | ????3.8 | | ????1.0 | | ???0.48 |
??605255 | Ferrite | ???30.1 | ????1.3 | ???5.0 | ????4.7 | | ????2.7 | | ???0.08 |
| Austenite | ???27.0 | ????1.3 | ???7.7 | ????3.0 | | ????3.3 | | ???0.45 |
??605262 | Ferrite | ???28.8 | ????3.0 | ???5.3 | ????4.8 | ????1.4 | ????0.9 | | ???0.08 |
| Austenite | ???26.3 | ????3.2 | ???8.1 | ????3.0 | ???0.85 | ????1.1 | | ???0.46 |
??605263 | Ferrite | ???29.7 | ????1.3 | ???5.1 | ????5.1 | ????1.3 | ???0.91 | | ???0.07 |
| Austenite | ???27.8 | ????1.4 | ???7.7 | ????3.2 | ???0.79 | ????1.1 | | ???0.51 |
??605253 | Ferrite | ???30.2 | ????1.3 | ???5.4 | ????5.0 | | ????1.3 | | ???0.09 |
| Austenite | ???27.5 | ????1.4 | ???8.4 | ????3.1 | | ????1.5 | | ???0.48 |
??605266 | Ferrite | ???31.0 | ????1.4 | ???5.7 | ????4.8 | | | | ???0.09 |
| Austenite | ???29.0 | ????1.5 | ???8.4 | ????3.1 | | | | ???0.52 |
??605269 | Ferrite | ???28.7 | ????1.3 | ???5.2 | ????5.1 | ????1.4 | ????0.9 | | ???0.11 |
| Austenite | ???26.6 | ????1.4 | ???7.8 | ????3.2 | ???0.87 | ????1.1 | | ???0.52 |
??605268 | Ferrite | ???29.1 | ????1.3 | ???5.0 | ????4.7 | ????1.3 | ???0.91 | ????0.84 | ???0.12 |
| Austenite | ???26.7 | ????1.4 | ???7.5 | ????3.2 | ???0.97 | ????1.0 | ????1.2 | ???0.51 |
??605270 | Ferrite | ???30.2 | ????1.2 | ???5.3 | ????5.0 | | ????1.3 | | ???0.11 |
| Austenite | ???27.7 | ????1.3 | ???8.0 | ????3.2 | | ????1.4 | | ???0.47 |
??605267 | Ferrite | ???30.1 | ????1.3 | ???5.1 | ????4.9 | | | ????1.3 | ???0.08 |
| Austenite | ???27.8 | ????1.4 | ???7.6 | ????3.1 | | | ????1.8 | ???0.46 |
The spot corrosion characteristic of all samples all (contains 1% FeCl at " Green Death " solution
3, 1% CuCl
2, 11% H
2SO
4With 1.2% HCl) in test grading.Experimental procedure is with identical according to the spot corrosion of ASTM G48C experiment, but this experiment is than 6%FeCl
3More acrid solution carries out in promptly so-called " Green Death " solution.And before carrying out the dew point experiment, in 2%HCl, carry out general corrosion test (each sample experiment 2 times) so that carry out classification.From table 10, Fig. 2 and Fig. 3, can see the result who obtains by all tests.The performance of all experimental samples in " Green Death " solution all is better than SAF2507, the PRE of all samples
Austenite/ PRE
FerriteProportional limit is preferably 0.9-1.05 in the 0.9-1.5 scope, simultaneously austenite and ferritic PRE value be all above 44, most of sample even substantially exceed 44, some samples even the value of reaching capacity 50.Although it should be noted that the chromium content in the sample 605251 is lower, the performance of sample 605251 in " Green Death " solution that contains the 1.5wt% cobalt almost is equal to the sample 605250 that cobalt contents is 0.6wt%.Especially amazing and interestedly be that because ca. (calculatings) the PRE value of sample 605251 is up to 48, this has surpassed some present commercial super duplex alloys, its T of while
MaxThe σ value is lower than 1010 ℃, this means on the basis based on table 2 train value in the example 1 to have good structural stability.
In table 10, listed the whole compositions of measuring with microprobe of this alloy mean P REW value (%Cr+3.3% (Mo+0.5%W)+16%N) and austenite and in ferrite based on the PRE value (rounding up) of the component of these phases.Carry out after under 1100 ℃, heat-treating measuring ferritic content after the Water Quenching.
Table 10
Sample | α-stagnation point (halt) | Whole PREW | ???PRE
α | ???PRE
γ | ??PRE
α/PRE
γ | ????CPT℃ ?Green?death |
??605258 | ????48.2 | ???50.3 | ???48.1 | ????49.1 | ????1.021 | |
??605249 | ????59.8 | ???48.9 | ???48.3 | ????46.6 | ????0.967 | ????75/80 |
??605259 | ????49.2 | ???50.2 | ???48.8 | ????48.4 | ????0.991 | |
??605260 | ????53.4 | ???48.5 | ???46.1 | ????47.0 | ????1.019 | |
??605250 | ????53.6 | ???49.2 | ???48.1 | ????46.8 | ????0.974 | ????95/80 |
??605251 | ????54.2 | ???48.2 | ???48.1 | ????46.9 | ????0.976 | ????90/80 |
??605261 | ???50.8 | ???48.6 | ???45.2 | ???46.3 | ????1.024 | |
??605252 | ???56.6 | ???48.2 | ???48.2 | ???45.6 | ????0.946 | ????80/75 |
??605254 | ???53.2 | ???48.8 | ???48.5 | ???46.2 | ????0.953 | ????90/75 |
??605255 | ???57.4 | ???46.9 | ???46.9 | ???44.1 | ????0.940 | ????90/80 |
??605262 | ???57.2 | ???47.9 | ???48.3 | ???45.0 | ????0.931 | |
??605263 | ???53.6 | ???49.7 | ???49.8 | ???47.8 | ????0.959 | |
??605253 | ???52.6 | ???48.4 | ???48.2 | ???45.4 | ????0.942 | ????85/75 |
??605266 | ???62.6 | ???49.4 | ???48.3 | ???47.6 | ????0.986 | |
??605269 | ???52.8 | ???50.5 | ???49.6 | ???46.9 | ????0.945 | |
??605268 | ???52.0 | ???49.9 | ???48.7 | ???47.0 | ????0.965 | |
??605270 | ???57.0 | ???49.2 | ???48.5 | ???45.7 | ????0.944 | |
??605267 | ???59.8 | ???49.3 | ???47.6 | ???45.4 | ????0.953 | |
In order to study structural stability in great detail, under 1080 ℃, 1100 ℃ and 1150 ℃, these samples are carried out annealing in 20 minutes, then at quenching-in water.By in opticmicroscope, studying to determine the intermetallic phase negligible temperature that becomes.To comparing, show which sample more may comprise the σ phase that does not expect to have through the sample structure that carries out after 1080 ℃ of annealing after the Water Quenching.In Figure 11, demonstrate these results.Structure controlled demonstrate, sample 605249,605251,605252,605253,605254,605255,605259,605260,605266 and 605267 σ that do not expect to have are mutually.In addition, the sample 605249 that contains cobalt 1.5wt% does not contain the σ phase, and 605250 on the sample that contains cobalt 0.6wt% contains the σ phase of very few number.These samples contain High Content Chromium that is about 29.0wt% and the molybdenum that is approximately 4.25wt%.If at the σ phase content component in sample 605249,605250,605251 and 605252 is compared, very obviously the structural stability aspect is very narrow for the compositional range of most optimum materials in this case.It also demonstrates, and 605268 on sample comprises the σ phase that is equivalent to sample 605263, and sample 605263 comprises a lot of σ phases.The key distinction between these samples is, is added with copper in the sample 605268.Although sample 605266 and 605267 contains in high-load chromium and the latter's alloy and also contains copper, but they do not contain the σ phase, in addition, the sample 605262 and 605263 that is added with 1.0wt% demonstrates has many σ structure mutually, it should be noted that simultaneously and also contain 1.0% tungsten but demonstrate its σ phase content obviously still less with respect to sample 605262 and the higher sample 605269 of 605263 its nitrogen contents.Therefore, need for example carry out the balance of well-tuned between chromium and the molybdenum at the different-alloy element that is in these high alloy content, so that obtain good structure properties.
Table 11 demonstrates from the result who carries out after 20 minutes through 1080 ℃ of annealing obtaining the shrend optical observation afterwards.The σ phasor is represented that by 1-5 wherein 1 representative is not found the σ phase in detecting, and 5 expressions are found high-load σ phase in detecting.
Table 11
Sample | The σ phase | ????Cr | ????Mo | ????W | ????Co | ???Cu | ?????N | ????Ru |
?605249 | ???1 | ???28.8 | ???4.23 | | ????1.5 | | ????0.38 | |
?605250 | ???2 | ???28.8 | ???4.24 | | ????0.6 | | ????0.40 | |
?605251 | ???1 | ???28.1 | ???4.24 | | ????1.5 | | ????0.38 | |
?605252 | ???1 | ???28.4 | ???4.23 | | ????0.5 | | ????0.37 | |
?605253 | ???1 | ???28.8 | ???4.16 | | ????1.5 | | ????0.37 | |
?605254 | ???1 | ???26.9 | ???4.80 | | ????1.0 | | ????0.38 | |
?605255 | ???1 | ???28.6 | ???4.04 | | ????3.0 | | ????0.31 | |
?605258 | ???2 | ???29.0 | ???4.23 | | ????1.5 | | ????0.46 | |
?605259 | ???1 | ???29.0 | ???4.23 | | ????0.6 | | ????0.45 | |
?605260 | ???1 | ???27.5 | ???4.22 | | ????1.5 | | ????0.44 | |
?605261 | ???2 | ???27.8 | ???4.22 | | ????0.6 | | ????0.43 | |
?605262 | ???4 | ???27.6 | ???3.93 | ????1.0 | ????1.0 | | ????0.36 | |
?605263 | ???5 | ???28.7 | ???3.96 | ????1.0 | ????1.0 | | ????0.40 | |
?605266 | ???1 | ???30.0 | ???4.02 | | | | ????0.38 | |
?605267 | ???1 | ???29.3 | ???4.23 | | | ???1.5 | ????0.38 | |
?605268 | ???2 | ???28.2 | ???3.98 | ????1.0 | ????1.0 | ???1.0 | ????0.43 | |
?605269 | ???3 | ???28.5 | ???3.97 | ????1.0 | ????1.0 | | ????0.45 | |
?605270 | ???3 | ???28.8 | ???4.19 | | ????1.5 | | ????0.41 | ????0.1 |
Be displayed in Table 12 out from some samples are carried out shock strength and test resulting result.These results are very high, and this shows after carrying out shrend then through 1100 ℃ of annealing to have good structure properties, and all test samples can satisfy the requirement of 100J with big surplus.
Table 12
Sample | Annealing [℃/minute] | Quench | Shock strength [J] | Shock strength [J] | Shock strength [J] |
??605249 | ???1100/20 | Water | ????>300 | ????>300 | ?????>300 |
??605250 | ???1100/20 | Water | ????>300 | ????>300 | ?????>300 |
??605251 | ???1100/20 | Water | ????>300 | ????>300 | ?????>300 |
??605252 | ???1100/20 | Water | ????>300 | ????>300 | ?????>300 |
??605253 | ???1100/20 | Water | ?????258 | ?????267 | ??????257 |
??605254 | ???1100/20 | Water | ????>300 | ????>300 | ?????>300 |
??605255 | ???1100/20 | Water | ????>300 | ????>300 | ?????>300 |
Fig. 4 demonstrates from most of samples being carried out the result that the high-temperature ductility experiment is drawn.Good workability is for material being made bar, tubing for example welded tube and seamless tube, sheet material, band, wire rod, welding rod and vital such as yes for the structural parts of pump, valve, flange, junctor one class.The sample 605249,605250,605251,605252,605255,605266 and 605267 that major part contains the nitrogen of about 0.38wt% can improve high-temperature ductility numerical value to a certain extent.
Experimental result is summed up
Have good structural stability, hot workability and weldability simultaneously in order to make material obtain good erosion resistance, this material should be according to following described being optimized:
● the PRE value in the ferrite should preferably be at least 47 greater than 45.
● the PRE value in the austenite should preferably be at least 47 greater than 45.
● the PRE value of whole alloy should preferably be at least 46.
● PRE
Austenite/ PRE
FerriteRatio should be between 0.9-1.15, preferably in the 0.9-1.05 scope.
● ferritic volume percent content is preferably in the 45-55% scope.
● T
Maxσ should be above 1010 ℃.
● nitrogen content should in the scope of 0.35-0.48wt%, more preferably be 0.38-0.40wt% preferably in the 0.28-0.5wt% scope.
● cobalt contents should be preferably 1.0-2.0wt%, more preferably 1.3-1.7wt% in the 0-3.5wt% scope.
● in order to ensure the high-dissolvability of nitrogen, that is, be under the situation of 0.38-0.40wt% at nitrogen content, need add the Cr of 29wt% and the Mo of 3.0wt% at least, the total content of element Cr, Mo and N satisfies the requirement to described PRE value like this.