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WO2017166962A1 - Melting process for nickel-based alloy containing aluminum, titanium, boron, and zirconium - Google Patents

Melting process for nickel-based alloy containing aluminum, titanium, boron, and zirconium Download PDF

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Publication number
WO2017166962A1
WO2017166962A1 PCT/CN2017/074564 CN2017074564W WO2017166962A1 WO 2017166962 A1 WO2017166962 A1 WO 2017166962A1 CN 2017074564 W CN2017074564 W CN 2017074564W WO 2017166962 A1 WO2017166962 A1 WO 2017166962A1
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Prior art keywords
nickel
zirconium
boron
aluminum
titanium
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French (fr)
Chinese (zh)
Inventor
李道乾
刘玉庭
郭建亭
刘云
王光华
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SHANDONG ROITIE NEW MATERIAL SCIENCE AND TECHNOLOGY Co Ltd
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SHANDONG ROITIE NEW MATERIAL SCIENCE AND TECHNOLOGY Co Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/023Alloys based on nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/06Making non-ferrous alloys with the use of special agents for refining or deoxidising
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel

Definitions

  • the invention relates to an alloy smelting process, in particular to a smelting process of a nickel-based alloy containing aluminum titanium boron zirconia.
  • the technical difficulty in vacuum smelting of aerospace and civil superalloys is that the gas content (oxygen, nitrogen, hydrogen) in the alloy is strictly controlled.
  • the oxygen and nitrogen contents of many alloys are generally around 20 ppm. Only by reducing the content of harmful impurities in the alloy, reducing the segregation of alloying elements, and improving the purity of the alloy melt can improve the performance and life of the alloy.
  • the vacuum smelting process is a very complicated thermal processing process, and the design of any one process step will have an important influence on the gas content of the alloy, the impurity content and the properties of the alloy.
  • the carbon deoxygenation reaction progresses, the carbon monoxide gas overflows, and the hydrogen and nitrogen harmful gases in the alloy are carried out.
  • the lower the oxygen content the more easily the metal melt evaporates, and the low melting point harmful impurity elements in the alloy are also easily eliminated. Therefore, deoxidation is a key step in the vacuum smelting process.
  • the deoxidation effect directly determines the content of harmful impurities in the alloy, which determines whether the alloy performance and life can be improved.
  • the components In alloys used in aviation, the components generally include several low melting point elements such as aluminum, titanium, boron, and zirconium.
  • low-melting-point elements such as aluminum, titanium, boron, and zirconium.
  • the timing, temperature, and degree of vacuum are not strictly controlled, large burning and volatilization occur, and the chemical composition of the alloy is difficult to control, resulting in waste.
  • the degree of vacuum is too low or the equipment leak rate is large, and a large amount of aluminum, titanium, boron, and zirconium elements are oxidized and burned, and the composition is difficult to control.
  • the object of the present invention is to provide a smelting process of a nickel-based alloy containing aluminum-titanium-boron-zirconium having uniform chemical composition, low-melting-point element burning loss and low volatilization, long-lasting properties of the alloy and high tensile properties at room temperature.
  • the smelting process of the nickel-based alloy containing aluminum titanium boron borax according to the present invention comprises the following steps:
  • the temperature is raised to 1570 ⁇ 1590 ° C, the remaining graphite is added to the crucible, refined, and then cooled;
  • Cool down wait until the temperature drops to 1360 ⁇ 1380 ° C, and then heat up to 1450 ⁇ 1470 ° C, using a ceramic filter while filtering and tapping.
  • Step (1) Graphite is a particle in which the spectral graphite electrode is broken up to 2 to 5 mm.
  • Step (1) The smelting temperature is 1560 to 1580 ° C, and the smelting time is 20 to 30 min.
  • Step (2) The temperature is raised to 1570 to 1590 ° C, and the remaining graphite is added to the crucible, and refined at a power of 80 KW for 20 to 30 minutes.
  • step (3) After all the metal calcium added in step (3) is melted, the temperature is raised to 1550 to 1570 ° C, and refining is carried out at 80 KW for 10 min. After refining for 5 min, the crucible is started to be shaken, so that the scum floating up to the molten metal level is discharged. The rear part of the wall is slag-treated.
  • Step (3) The amount of metal calcium is 0.02 to 0.05% of the total mass of the superalloy. If the amount of calcium added is too large, deoxidation inclusions will form in the molten metal, so the amount of metal calcium added must be strictly controlled. It is also important to carry out slagging treatment after adding metal calcium for deep deoxidation.
  • Step (4) is heated until aluminum and titanium are all melted, and then stirred for 3 to 5 minutes.
  • Step (5) is heated to a nickel-boron alloy, and the zirconium is melted, and then stirred for 3 to 5 minutes.
  • the degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ⁇ 0.1 Pa. Boron should be added in the late stage of smelting before tapping. When aluminum and titanium are added in a large amount, they should be added in two or more batches. When aluminum is about 3 wt.%, and titanium is about 3 wt.%, it can be added twice. If more aluminum and titanium content should be considered, more times should be added.
  • Step (6) Cooling the molten metal melt can be in the form of natural cooling after power failure, and other cooling forms can also be used.
  • the invention preferably takes the form of a natural cooling of power outages.
  • the invention adopts a secondary carbon deep deoxidation process and a metal calcium deoxidation process, and adds one-half of the graphite which accounts for the total carbon content of the alloy before the start of the high-temperature alloy smelting, and the graphite is added to the bottom of the crucible.
  • the metal is completely melted, it is raised to a certain temperature, and subjected to a secondary carbon addition operation to further perform deep deoxidation, and then metal calcium is added for calcium deoxidation; at the same time, the chemical composition of the alloy is controlled by controlling the timing and temperature of the addition of aluminum, titanium, boron, and zirconium.
  • frozen metal melt makes the harmful gas dissolved in the molten metal float in the process of cooling and solidification of the molten metal, and the negative pressure difference generated by vacuum furnace smelting will be harmful gas Further removed.
  • the metal melt is further purified to obtain a high-quality high-temperature alloy, and the content of harmful gases such as O, N, H and low-melting harmful impurities in the high-temperature alloy are minimized to achieve a pure alloy.
  • the melt reduces the segregation of alloying elements and ensures the properties of the alloy.
  • the invention improves the long-term performance and the tensile property at room temperature of the high-temperature alloy, and the comprehensive mechanical properties of the alloy and the quality of the alloy all reach the level of high-quality alloys at home and abroad.
  • the vacuum smelting process of the present invention is used for production, and the chemical composition thereof is shown in Table 1, and the performance parameters are shown in Table 2.
  • the vacuum smelting process of the present invention is as follows:
  • the temperature was raised to 1580 ⁇ 10 ° C, and the remaining graphite was added into the crucible, and refined at a power of 80 KW for 25 min, and then cooled;
  • Cool down wait until the temperature drops to 1370 ⁇ 10 ° C, and then heat up to 1460 ⁇ 10 ° C, using a ceramic filter while filtering and tapping.
  • the degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ⁇ 0.1 Pa.
  • element C Si Mn P S Cr Fe range 0.03/0.07 ⁇ 0.50 ⁇ 0.25 ⁇ 0.015 ⁇ 0.015 11.0/13.0 ⁇ 0.5 Measured 0.054 0.037 0.050 0.0065 0.0013 11.78 0.15 element Mo Cu Nb Ti Co Al Zr range 3.80/5.20 ⁇ 0.5 1.50/2.50 0.40/1.00 ⁇ 1.0 5.50/6.50 0.05/0.15 Measured 4.71 0.038 2.21 0.82 0.49 6.13 0.080 element B Pb Ag Bi Ni O ppm N ppm range 0.005/0.015 ⁇ 0.0010 ⁇ 0.0005 ⁇ 0.00020 Yu —— —— Measured 0.013 0.0005 0.00003 0.00005 Yu 7.5 6.8
  • the vacuum smelting process of the present invention was carried out in accordance with the standard of the K418B alloy, and the chemical composition thereof is shown in Table 3, and the performance parameters are shown in Table 4.
  • the vacuum smelting process of the present invention is as follows:
  • the temperature was raised to 1570 ⁇ 10 ° C, and the remaining graphite was added into the crucible, and refined at a power of 80 KW for 20 min, and then cooled;
  • Cool down wait until the temperature drops to 1360 ⁇ 10 ° C, and then heat up to 1470 ⁇ 10 ° C, using a ceramic filter while filtering and tapping.
  • the degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ⁇ 0.1 Pa.
  • the rest is as in Example 1.
  • element C Si Mn P S Cr Fe range 0.03/0.07 ⁇ 0.50 ⁇ 0.25 ⁇ 0.015 ⁇ 0.015 11.0/13.0 ⁇ 0.5 Measured 0.055 0.039 0.050 0.0067 0.0013 11.81 0.18 element Mo Cu Nb Ti Co Al Zr range 3.80/5.20 ⁇ 0.5 1.50/2.50 0.40/1.00 ⁇ 1.0 5.50/6.50 0.05/0.15 Measured 4.75 0.035 2.29 0.78 0.52 6.18 0.083 element B Pb Ag Bi Ni O ppm N ppm range 0.005/0.015 ⁇ 0.0010 ⁇ 0.0005 ⁇ 0.00020 Yu —— —— Measured 0.010 0.0004 0.00003 0.00004 Yu 7.7 6.5
  • the vacuum smelting process of the present invention is used for production, and the chemical composition thereof is shown in Table 5, and the performance parameters are shown in Table 6.
  • the vacuum smelting process of the present invention is as follows:
  • the temperature was raised to 1590 ⁇ 10 ° C, and the remaining graphite was added into the crucible, and refined at a power of 80 KW for 30 min, and then cooled;
  • Cool down wait until the temperature drops to 1380 ⁇ 10 ° C, and then heat up to 1450 ⁇ 10 ° C, using a ceramic filter while filtering and tapping.
  • the degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ⁇ 0.1 Pa.
  • the rest is as in Example 1.
  • element C Si Mn P S Cr Fe range 0.03/0.07 ⁇ 0.50 ⁇ 0.25 ⁇ 0.015 ⁇ 0.015 11.0/13.0 ⁇ 0.5 Measured 0.057 0.041 0.049 0.0061 0.0014 11.95 0.17 element Mo Cu Nb Ti Co Al Zr range 3.80/5.20 ⁇ 0.5 1.50/2.50 0.40/1.00 ⁇ 1.0 5.50/6.50 0.05/0.15 Measured 4.82 0.039 2.35 0.85 0.58 6.25 0.091 element B Pb Ag Bi Ni O ppm N ppm range 0.005/0.015 ⁇ 0.0010 ⁇ 0.0005 ⁇ 0.00020 Yu —— —— Measured 0.99 0.0006 0.00004 0.00003 Yu 7.6 6.7
  • the content of oxygen and nitrogen in the K418B alloy is very low. Due to the secondary carbon deep deoxidation process, the metal calcium deoxidation process, the alloying process, the frozen metal melt process, and the filtration process, the content of other harmful impurities in the alloy is significantly reduced. The most prominent is that the alloy's room temperature tensile properties and high temperature durability are greatly improved.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Abstract

Disclosed is a melting process for a nickel-based alloy containing aluminum, titanium, boron, and zirconium, comprising: adding graphite accounting for 50% of a total carbon-containing mass of an alloy into a crucible of a vacuum furnace and placing the graphite at the bottommost portion of the crucible, and adding all elements, except for aluminum, titanium, boron, zirconium, and nickel, in the alloy into the crucible of the vacuum furnace to be molten; raising the temperature, adding the remaining graphite into the crucible, and carrying out refining and then cooling; adding calcium metal into the crucible, and after the calcium metal is completely molten, carrying out refining and then cooling; adding aluminum and titanium into the crucible, and raising the temperature until the aluminum and the titanium are completely molten; adding a nickel-boron alloy and zirconium into the crucible, and raising the temperature until the nickel-boron alloy and the zirconium are completely molten; and cooling the molten metal, filtering, and carrying out tapping and pouring. The process method reduces the content of harmful gas and low-melting-point harmful impurities in an alloy, and achieves the purposes of purifying an alloy melt, reducing segregation of alloy elements, and ensuring alloy performance.

Description

含有铝钛硼锆的镍基合金的冶炼工艺Smelting process of nickel-based alloy containing aluminum titanium boron zirconia 技术领域Technical field

本发明涉及合金冶炼工艺,具体涉及一种含有铝钛硼锆的镍基合金的冶炼工艺。The invention relates to an alloy smelting process, in particular to a smelting process of a nickel-based alloy containing aluminum titanium boron zirconia.

背景技术Background technique

航空航天以及民用高温合金真空冶炼的技术难点在于,严格控制合金中的气体含量(氧,氮,氢),目前按照企业标准,许多合金中氧、氮含量一般在20ppm左右。只有降低合金中的有害杂质含量,减少合金元素的偏析,提高合金熔液的纯净度,才能达到提高合金的使用性能和寿命。然而,真空冶炼过程是一个十分复杂的热加工工艺过程,任何一个工艺步骤的设计都会对合金的气体含量,杂质含量以及合金的性能有重要影响。The technical difficulty in vacuum smelting of aerospace and civil superalloys is that the gas content (oxygen, nitrogen, hydrogen) in the alloy is strictly controlled. At present, according to the enterprise standard, the oxygen and nitrogen contents of many alloys are generally around 20 ppm. Only by reducing the content of harmful impurities in the alloy, reducing the segregation of alloying elements, and improving the purity of the alloy melt can improve the performance and life of the alloy. However, the vacuum smelting process is a very complicated thermal processing process, and the design of any one process step will have an important influence on the gas content of the alloy, the impurity content and the properties of the alloy.

合金中的O,N,S在合金溶液中会形成非金属夹杂物,如(Al2O3),(Ti,Ta)C/N,(Ti,Ta)S合金中非金属夹杂物的多少和形态都会对合金综合性能有重大影响。此外合金熔液的纯净度是衡量母合金锭质量和制造水平的重要指标。真空冶炼中是以碳为主要脱氧元素,由于碳的分解反应而达到将金属溶液的氧脱除,从而达到减少合金中的气体含量,纯净金属溶液,提高合金质量的目的。随着碳脱氧反应的进行,一氧化碳气体的溢出,将合金中的氢、氮有害气体带出。氧含量越低,金属熔液更易蒸发,合金中的低熔点有害杂质元素也易于排除。因而,脱氧是真空冶炼过程的一个关键步骤,脱氧效果直接决定了合金中的有害杂质含量,决定着能否提高合金使用性能和寿命。O, N, S in the alloy will form non-metallic inclusions in the alloy solution, such as (Al 2 O 3 ), (Ti, Ta) C / N, the number of non-metallic inclusions in the (Ti, Ta)S alloy Both the form and the form have a major impact on the overall performance of the alloy. In addition, the purity of the alloy melt is an important indicator for measuring the quality and manufacturing level of the master alloy ingot. In vacuum smelting, carbon is the main deoxidizing element. Due to the decomposition reaction of carbon, the oxygen of the metal solution is removed, thereby reducing the gas content in the alloy, purifying the metal solution, and improving the quality of the alloy. As the carbon deoxygenation reaction progresses, the carbon monoxide gas overflows, and the hydrogen and nitrogen harmful gases in the alloy are carried out. The lower the oxygen content, the more easily the metal melt evaporates, and the low melting point harmful impurity elements in the alloy are also easily eliminated. Therefore, deoxidation is a key step in the vacuum smelting process. The deoxidation effect directly determines the content of harmful impurities in the alloy, which determines whether the alloy performance and life can be improved.

在航空使用的合金中,组分一般都包括铝、钛、硼、锆等几种低熔点元素。在加入这些低熔点元素进行合金化处理时,如果不严格控制加入的时机、温度、真空度等因素,则会产生较大的烧损和挥发,使合金化学成分难以控制,从而产生废品。具体来说,加入铝、钛、硼、锆时的真空度过低或设备漏气率大,大量的铝、钛、硼、锆元素会产生氧化烧损,成分难以控制。加入铝、钛时金属熔液温度过高,大量的铝、钛则会由于放热放应而产生烧损和挥发。向金属熔液中加入铝、钛时,会产生剧烈的放热反应,尤其是加入量较大时,金属熔液放热反应就大。即使铝、钛加入时金属熔液温度适宜,但由于一次加入量过大,同样会产生烧损和真空挥发使合金化学成分难以控制。另外,由于铝、钛、硼、锆自身较轻,密度小,在加入到金属熔液中后,漂浮在金属熔液表面,如果没有进行充分的搅拌极易产生偏析,会严重影响合金的综合性能。特别的是,硼的加入时间也非常重要,加入过早,极易烧损,加入过晚,易分布不均,因此掌握好硼加入的时间就显得非常重要。In alloys used in aviation, the components generally include several low melting point elements such as aluminum, titanium, boron, and zirconium. When these low-melting-point elements are added for alloying treatment, if the timing, temperature, and degree of vacuum are not strictly controlled, large burning and volatilization occur, and the chemical composition of the alloy is difficult to control, resulting in waste. Specifically, when aluminum, titanium, boron, and zirconium are added, the degree of vacuum is too low or the equipment leak rate is large, and a large amount of aluminum, titanium, boron, and zirconium elements are oxidized and burned, and the composition is difficult to control. When aluminum and titanium are added, the temperature of the molten metal is too high, and a large amount of aluminum and titanium are burnt and volatilized due to the exothermic release. When aluminum or titanium is added to the molten metal, a severe exothermic reaction occurs, and especially when the amount of addition is large, the exothermic reaction of the molten metal is large. Even if the temperature of the molten metal is suitable when aluminum and titanium are added, the chemical composition of the alloy is hard to control because the amount of the primary addition is too large, and the burning and vacuum volatilization are also caused. In addition, since aluminum, titanium, boron, and zirconium are lighter in themselves and have a low density, they float on the surface of the molten metal after being added to the molten metal. If sufficient agitation is not performed, segregation is easily generated, which seriously affects the synthesis of the alloy. performance. In particular, the addition time of boron is also very important. It is too early to be burned, and it is easy to burn. It is too late to be distributed, so it is very important to master the time of boron addition.

鉴于目前现有技术的情况,亟需开发一种化学成分均匀、低熔点元素烧损及挥发少、合金持久性能和室温拉伸性能强的含有铝钛硼锆的镍基合金的冶炼工艺。 In view of the current state of the art, it is urgent to develop a smelting process of a nickel-based alloy containing aluminum, titanium, boron, and zirconium, which has uniform chemical composition, low melting point and low volatilization, and long-lasting properties of the alloy and tensile properties at room temperature.

发明内容Summary of the invention

本发明的目的是提供一种化学成分均匀、低熔点元素烧损及挥发少、合金持久性能和室温拉伸性能强的含有铝钛硼锆的镍基合金的冶炼工艺。SUMMARY OF THE INVENTION The object of the present invention is to provide a smelting process of a nickel-based alloy containing aluminum-titanium-boron-zirconium having uniform chemical composition, low-melting-point element burning loss and low volatilization, long-lasting properties of the alloy and high tensile properties at room temperature.

本发明所述的含有铝钛硼锆的镍基合金的冶炼工艺,包括以下步骤:The smelting process of the nickel-based alloy containing aluminum titanium boron borax according to the present invention comprises the following steps:

(1)第一步碳脱氧:(1) First step carbon deoxidation:

将占高温合金总含碳质量50%的石墨加入到真空炉坩埚内,置于坩埚最底部,向真空炉坩埚内加入除铝、钛、硼、锆、镍之外的高温合金中的所有元素进行冶炼;Adding 50% of the total carbon content of the superalloy to the vacuum furnace, placing it at the bottom of the crucible, adding all the elements in the superalloy except aluminum, titanium, boron, zirconium and nickel into the vacuum furnace. Smelting;

(2)第二步碳脱氧:(2) The second step of carbon deoxidation:

温度升至1570~1590℃,向坩埚内加入剩余的石墨,精炼,之后降温;The temperature is raised to 1570 ~ 1590 ° C, the remaining graphite is added to the crucible, refined, and then cooled;

(3)金属钙脱氧:(3) Metal calcium deoxidation:

加入金属钙,全部熔化后,升温至1550~1570℃,进行精炼,精炼过程中摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部;Adding metal calcium, after melting all, heating to 1550 ~ 1570 ° C, refining, shaking in the refining process, so that the floating slag floating up to the molten metal surface is discharged to the back of the wall;

(4)加入铝、钛:(4) Add aluminum and titanium:

降温至1370~1390℃,向其中加入铝、钛,升温至铝、钛全部熔化;Cooling to 1370 ~ 1390 ° C, adding aluminum, titanium, heating up to aluminum, titanium all melted;

(5)加入镍硼合金、锆:(5) Adding nickel-boron alloy and zirconium:

保持温度1410~1430℃,向其中加入镍硼合金、锆,升温至镍硼合金、锆全部熔化;Maintaining a temperature of 1410 to 1430 ° C, adding a nickel-boron alloy and zirconium thereto, and heating the mixture to a nickel-boron alloy and zirconium;

(6)冷冻金属熔液、过滤、出钢浇注:(6) Frozen metal melt, filtration, tapping and pouring:

降温,待温度降至1360~1380℃,再升温至1450~1470℃,采用陶瓷过滤器一边过滤一边出钢浇注。Cool down, wait until the temperature drops to 1360 ~ 1380 ° C, and then heat up to 1450 ~ 1470 ° C, using a ceramic filter while filtering and tapping.

其中:among them:

步骤(1)石墨为光谱石墨电极破碎至2~5mm的颗粒。Step (1) Graphite is a particle in which the spectral graphite electrode is broken up to 2 to 5 mm.

步骤(1)冶炼温度1560~1580℃,冶炼时间20~30min。Step (1) The smelting temperature is 1560 to 1580 ° C, and the smelting time is 20 to 30 min.

步骤(2)温度升至1570~1590℃,向坩埚内加入剩余的石墨,于功率80KW下精炼20~30min。Step (2) The temperature is raised to 1570 to 1590 ° C, and the remaining graphite is added to the crucible, and refined at a power of 80 KW for 20 to 30 minutes.

步骤(3)加入的金属钙全部熔化后,再将温度升至1550~1570℃,于80KW下进行精炼10min,精炼5min时,开始摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部,进行排渣处理。After all the metal calcium added in step (3) is melted, the temperature is raised to 1550 to 1570 ° C, and refining is carried out at 80 KW for 10 min. After refining for 5 min, the crucible is started to be shaken, so that the scum floating up to the molten metal level is discharged. The rear part of the wall is slag-treated.

步骤(3)金属钙的用量为高温合金总质量的0.02~0.05%。金属钙加入量过大,会在金属熔液中形成脱氧反应夹杂物,因此要严格控制金属钙的加入量。加入金属钙进行深脱氧后要进行排渣处理也十分重要。Step (3) The amount of metal calcium is 0.02 to 0.05% of the total mass of the superalloy. If the amount of calcium added is too large, deoxidation inclusions will form in the molten metal, so the amount of metal calcium added must be strictly controlled. It is also important to carry out slagging treatment after adding metal calcium for deep deoxidation.

步骤(4)升温至铝、钛全部熔化后,再搅拌3~5min。 Step (4) is heated until aluminum and titanium are all melted, and then stirred for 3 to 5 minutes.

步骤(5)升温至镍硼合金、锆熔化后,再搅拌3~5min。Step (5) is heated to a nickel-boron alloy, and the zirconium is melted, and then stirred for 3 to 5 minutes.

加入铝、钛、镍硼合金、锆时的真空度≤0.1Pa。硼应在熔炼后期,出钢浇注之前加入。铝、钛加入量大时,应分两批或多批加入,一般铝为3wt.%左右时,钛为3wt.%左右时,两次加入即可。如果更多的铝钛含量时应考虑更多次地加入。The degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ≤ 0.1 Pa. Boron should be added in the late stage of smelting before tapping. When aluminum and titanium are added in a large amount, they should be added in two or more batches. When aluminum is about 3 wt.%, and titanium is about 3 wt.%, it can be added twice. If more aluminum and titanium content should be considered, more times should be added.

步骤(6)降温进行冷冻金属熔液可以采用停电后,自然降温的形式,也可以采用其他降温形式。本发明优选停电自然降温的形式。Step (6) Cooling the molten metal melt can be in the form of natural cooling after power failure, and other cooling forms can also be used. The invention preferably takes the form of a natural cooling of power outages.

本发明的有益效果如下:The beneficial effects of the present invention are as follows:

本发明采用二次加碳深脱氧工艺及金属钙脱氧工艺,在开始高温合金冶炼前加入占合金总含碳量的二分之一的石墨,石墨加在坩埚的底部。待金属全部熔化后升到一定温度,进行二次加碳操作进一步进行深脱氧,再加入金属钙进行钙脱氧;同时,通过控制铝、钛、硼、锆加入时机及温度,使得合金的化学成分更加均匀,低熔点元素烧损及挥发少;冷冻金属熔液使得在金属熔液降温凝固的过程中,溶解在金属熔液中的有害气体上浮,利用真空炉冶炼产生的负压差将有害气体进一步除去。采用陶瓷过滤器过滤后,进一步纯净金属熔液,从而得到高质量的高温合金,也保证最大限度的降低高温合金中O,N,H有害气体的含量和低熔点有害杂质的含量,达到纯净合金熔液,减少合金元素的偏析,保证合金性能的目的。本发明提高了高温合金的持久性能和室温拉伸性能,合金的综合力学性能及合金的质量均达到国内外优质合金的水平。The invention adopts a secondary carbon deep deoxidation process and a metal calcium deoxidation process, and adds one-half of the graphite which accounts for the total carbon content of the alloy before the start of the high-temperature alloy smelting, and the graphite is added to the bottom of the crucible. After the metal is completely melted, it is raised to a certain temperature, and subjected to a secondary carbon addition operation to further perform deep deoxidation, and then metal calcium is added for calcium deoxidation; at the same time, the chemical composition of the alloy is controlled by controlling the timing and temperature of the addition of aluminum, titanium, boron, and zirconium. More uniform, low melting point elements burn less and less volatile; frozen metal melt makes the harmful gas dissolved in the molten metal float in the process of cooling and solidification of the molten metal, and the negative pressure difference generated by vacuum furnace smelting will be harmful gas Further removed. After filtering with a ceramic filter, the metal melt is further purified to obtain a high-quality high-temperature alloy, and the content of harmful gases such as O, N, H and low-melting harmful impurities in the high-temperature alloy are minimized to achieve a pure alloy. The melt reduces the segregation of alloying elements and ensures the properties of the alloy. The invention improves the long-term performance and the tensile property at room temperature of the high-temperature alloy, and the comprehensive mechanical properties of the alloy and the quality of the alloy all reach the level of high-quality alloys at home and abroad.

具体实施方式detailed description

以下结合实施例对本发明做进一步描述。The invention will be further described below in conjunction with the embodiments.

实施例1Example 1

按照K418B合金的标准采用本发明的真空冶炼工艺进行生产,其化学成分如表1所示,性能参数如表2所示。According to the standard of K418B alloy, the vacuum smelting process of the present invention is used for production, and the chemical composition thereof is shown in Table 1, and the performance parameters are shown in Table 2.

以200Kg真空炉为例,本发明的真空冶炼工艺如下:Taking a 200 Kg vacuum furnace as an example, the vacuum smelting process of the present invention is as follows:

(1)第一步碳脱氧:(1) First step carbon deoxidation:

将占高温合金总含碳质量50%的石墨加入到真空炉坩埚内,置于坩埚最底部,向真空炉坩埚内加入除铝、钛、硼、锆、镍之外的高温合金中的所有元素进行冶炼;石墨为光谱石墨电极破碎至2~5mm的颗粒;冶炼温度1570±10℃,冶炼时间25min;Adding 50% of the total carbon content of the superalloy to the vacuum furnace, placing it at the bottom of the crucible, adding all the elements in the superalloy except aluminum, titanium, boron, zirconium and nickel into the vacuum furnace. Smelting; graphite is a graphite electrode crushed to 2 ~ 5mm particles; smelting temperature 1570 ± 10 ° C, smelting time 25min;

(2)第二步碳脱氧:(2) The second step of carbon deoxidation:

温度升至1580±10℃,向坩埚内加入剩余的石墨,于功率80KW下精炼25min,之后降温;The temperature was raised to 1580±10 ° C, and the remaining graphite was added into the crucible, and refined at a power of 80 KW for 25 min, and then cooled;

(3)金属钙脱氧: (3) Metal calcium deoxidation:

加入金属钙,全部熔化后,升温至1560±10℃,于80KW下进行精炼10min,精炼5min时,开始摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部;金属钙的用量为高温合金总质量的0.03%。Adding metal calcium, after melting all, heating to 1560 ± 10 ° C, refining at 80 KW for 10 min, refining for 5 min, starting to shake the crucible, so that the scum floating up to the molten metal surface is discharged to the back of the crucible wall; The amount of calcium used is 0.03% of the total mass of the superalloy.

(4)加入铝、钛:(4) Add aluminum and titanium:

降温至1380±10℃,向其中加入铝、钛,升温至铝、钛全部熔化,再搅拌5min;Cooling to 1380 ± 10 ° C, adding aluminum, titanium, heating to aluminum, titanium all melted, and then stirred for 5 min;

(5)加入镍硼合金、锆:(5) Adding nickel-boron alloy and zirconium:

保持温度1420±10℃,向其中加入镍硼合金、锆,升温至镍硼合金熔化,再搅拌3min;Maintaining a temperature of 1420 ± 10 ° C, adding nickel boron alloy, zirconium, heating to nickel boron alloy melting, and stirring for 3 min;

(6)冷冻金属熔液、过滤、出钢浇注:(6) Frozen metal melt, filtration, tapping and pouring:

降温,待温度降至1370±10℃,再升温至1460±10℃,采用陶瓷过滤器一边过滤一边出钢浇注。Cool down, wait until the temperature drops to 1370 ± 10 ° C, and then heat up to 1460 ± 10 ° C, using a ceramic filter while filtering and tapping.

加入铝、钛、镍硼合金、锆时的真空度≤0.1Pa。The degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ≤ 0.1 Pa.

表1实施例1合金成分参数表Table 1 Example 1 alloy composition parameter table

元素element CC SiSi MnMn PP SS CrCr FeFe 范围range 0.03/0.070.03/0.07 ≤0.50≤0.50 ≤0.25≤0.25 ≤0.015≤0.015 ≤0.015≤0.015 11.0/13.011.0/13.0 ≤0.5≤0.5 实测Measured 0.0540.054 0.0370.037 0.0500.050 0.00650.0065 0.00130.0013 11.7811.78 0.150.15 元素element MoMo CuCu NbNb TiTi CoCo AlAl ZrZr 范围range 3.80/5.203.80/5.20 ≤0.5≤0.5 1.50/2.501.50/2.50 0.40/1.000.40/1.00 ≤1.0≤1.0 5.50/6.505.50/6.50 0.05/0.150.05/0.15 实测Measured 4.714.71 0.0380.038 2.212.21 0.820.82 0.490.49 6.136.13 0.0800.080 元素element BB PbPb AgAg BiBi NiNi O ppmO ppm N ppmN ppm 范围range 0.005/0.0150.005/0.015 ≤0.0010≤0.0010 ≤0.0005≤0.0005 ≤0.00020≤0.00020 Yu ———— ———— 实测Measured 0.0130.013 0.00050.0005 0.000030.00003 0.000050.00005 Yu 7.57.5 6.86.8

用德国进口ON900型氧氮分析仪测定:氧(O)7.5ppm氮(N)6.8ppm。It was measured by a German imported ON900 type oxygen nitrogen analyzer: oxygen (O) 7.5 ppm nitrogen (N) 6.8 ppm.

表2实施例1合金性能参数表Table 2 Example 1 alloy performance parameter table

室温拉伸性能Room temperature tensile properties σb/MPaσ b /MPa σ0.2/MPaσ 0.2 /MPa δS/%δ S /% 标准standard ≥760≥760 ≥690≥690 ≥5.0≥5.0 实测Measured 892892 756756 7.57.5

Figure PCTCN2017074564-appb-000001
Figure PCTCN2017074564-appb-000001

实施例2Example 2

按照K418B合金的标准采用本发明的真空冶炼工艺进行生产,其化学成分如表3所示,性能参数如表4所示。The vacuum smelting process of the present invention was carried out in accordance with the standard of the K418B alloy, and the chemical composition thereof is shown in Table 3, and the performance parameters are shown in Table 4.

以200Kg真空炉为例,本发明的真空冶炼工艺如下:Taking a 200 Kg vacuum furnace as an example, the vacuum smelting process of the present invention is as follows:

(1)第一步碳脱氧:(1) First step carbon deoxidation:

将占高温合金总含碳质量50%的石墨加入到真空炉坩埚内,置于坩埚最底部,向真空炉坩埚内加入除铝、钛、硼、锆、镍之外的高温合金中的所有元素进行冶炼;石墨为光谱石墨电极破碎至2~5mm的颗粒;冶炼温度1580±10℃,冶炼时间20min;Adding 50% of the total carbon content of the superalloy to the vacuum furnace, placing it at the bottom of the crucible, adding all the elements in the superalloy except aluminum, titanium, boron, zirconium and nickel into the vacuum furnace. Smelting; graphite is broken by spectral graphite electrode to 2 ~ 5mm particles; smelting temperature is 1580 ± 10 ° C, smelting time 20min;

(2)第二步碳脱氧:(2) The second step of carbon deoxidation:

温度升至1570±10℃,向坩埚内加入剩余的石墨,于功率80KW下精炼20min,之后降温;The temperature was raised to 1570±10 ° C, and the remaining graphite was added into the crucible, and refined at a power of 80 KW for 20 min, and then cooled;

(3)金属钙脱氧:(3) Metal calcium deoxidation:

加入金属钙,全部熔化后,升温至1570±10℃,于80KW下进行精炼10min,精炼5min时,开始摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部;金属钙的用量为高温合金总质量的0.04%。Adding metal calcium, after melting all, heating to 1570±10 ° C, refining at 80 KW for 10 min, refining for 5 min, starting to shake the crucible, so that the scum floating up to the molten metal surface is discharged to the back of the crucible wall; The amount of calcium used is 0.04% of the total mass of the superalloy.

(4)加入铝、钛:(4) Add aluminum and titanium:

降温至1390±10℃,向其中加入铝、钛,升温至铝、钛全部熔化,再搅拌3min;Cooling to 1390 ± 10 ° C, adding aluminum, titanium, heating to aluminum, titanium all melted, and then stirred for 3 min;

(5)加入镍硼合金、锆:(5) Adding nickel-boron alloy and zirconium:

保持温度1410±10℃,向其中加入镍硼合金、锆,升温至镍硼合金熔化,再搅拌5min;Maintaining a temperature of 1410 ± 10 ° C, adding nickel boron alloy, zirconium, heating to nickel boron alloy melting, and stirring for 5 min;

(6)冷冻金属熔液、过滤、出钢浇注:(6) Frozen metal melt, filtration, tapping and pouring:

降温,待温度降至1360±10℃,再升温至1470±10℃,采用陶瓷过滤器一边过滤一边出钢浇注。Cool down, wait until the temperature drops to 1360 ± 10 ° C, and then heat up to 1470 ± 10 ° C, using a ceramic filter while filtering and tapping.

加入铝、钛、镍硼合金、锆时的真空度≤0.1Pa。其余如实施例1。The degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ≤ 0.1 Pa. The rest is as in Example 1.

表3实施例2合金成分参数表Table 3 Example 2 alloy composition parameter table

元素element CC SiSi MnMn PP SS CrCr FeFe 范围range 0.03/0.070.03/0.07 ≤0.50≤0.50 ≤0.25≤0.25 ≤0.015≤0.015 ≤0.015≤0.015 11.0/13.011.0/13.0 ≤0.5≤0.5 实测Measured 0.0550.055 0.0390.039 0.0500.050 0.00670.0067 0.00130.0013 11.8111.81 0.180.18 元素element MoMo CuCu NbNb TiTi CoCo AlAl ZrZr 范围range 3.80/5.203.80/5.20 ≤0.5≤0.5 1.50/2.501.50/2.50 0.40/1.000.40/1.00 ≤1.0≤1.0 5.50/6.505.50/6.50 0.05/0.150.05/0.15 实测Measured 4.754.75 0.0350.035 2.292.29 0.780.78 0.520.52 6.186.18 0.0830.083 元素element BB PbPb AgAg BiBi NiNi O ppmO ppm N ppmN ppm 范围range 0.005/0.0150.005/0.015 ≤0.0010≤0.0010 ≤0.0005≤0.0005 ≤0.00020≤0.00020 Yu ———— ———— 实测Measured 0.0100.010 0.00040.0004 0.000030.00003 0.000040.00004 Yu 7.77.7 6.56.5

用德国进口ON900型氧氮分析仪测定:氧(O)7.7ppm氮(N)6.5ppm。It was measured by a German imported ON900 type oxygen nitrogen analyzer: oxygen (O) 7.7 ppm nitrogen (N) 6.5 ppm.

表4实施例2合金性能参数表Table 4 Example 2 alloy performance parameter table

室温拉伸性能Room temperature tensile properties σb/MPaσ b /MPa σ0.2/MPaσ 0.2 /MPa δS/%δ S /% 标准standard ≥760≥760 ≥690≥690 ≥5.0≥5.0 实测Measured 895895 761761 8.28.2

Figure PCTCN2017074564-appb-000002
Figure PCTCN2017074564-appb-000002

实施例3Example 3

按照K418B合金的标准采用本发明的真空冶炼工艺进行生产,其化学成分如表5所示,性能参数如表6所示。According to the standard of K418B alloy, the vacuum smelting process of the present invention is used for production, and the chemical composition thereof is shown in Table 5, and the performance parameters are shown in Table 6.

以200Kg真空炉为例,本发明的真空冶炼工艺如下:Taking a 200 Kg vacuum furnace as an example, the vacuum smelting process of the present invention is as follows:

(1)第一步碳脱氧:(1) First step carbon deoxidation:

将占高温合金总含碳质量50%的石墨加入到真空炉坩埚内,置于坩埚最底部,向真空炉坩埚内加入除铝、钛、硼、锆、镍之外的高温合金中的所有元素进行冶炼;石墨为光谱石墨电极破碎至2~5mm的颗粒;冶炼温度1560±10℃,冶炼时间30min;Adding 50% of the total carbon content of the superalloy to the vacuum furnace, placing it at the bottom of the crucible, adding all the elements in the superalloy except aluminum, titanium, boron, zirconium and nickel into the vacuum furnace. Smelting; graphite is broken by spectral graphite electrode to 2 ~ 5mm particles; smelting temperature is 1560 ± 10 ° C, smelting time 30min;

(2)第二步碳脱氧:(2) The second step of carbon deoxidation:

温度升至1590±10℃,向坩埚内加入剩余的石墨,于功率80KW下精炼30min,之后降温;The temperature was raised to 1590±10 ° C, and the remaining graphite was added into the crucible, and refined at a power of 80 KW for 30 min, and then cooled;

(3)金属钙脱氧:(3) Metal calcium deoxidation:

加入金属钙,全部熔化后,升温至1550±10℃,于80KW下进行精炼10min,精炼5min时,开始摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部;金属钙的用量为高温合金总质量的0.05%。Adding metal calcium, after melting all, heating to 1550 ± 10 ° C, refining at 80 KW for 10 min, refining for 5 min, starting to shake the crucible, so that the scum floating up to the molten metal surface is discharged to the back of the crucible wall; The amount of calcium used is 0.05% of the total mass of the superalloy.

(4)加入铝、钛:(4) Add aluminum and titanium:

降温至1370±10℃,向其中加入铝、钛,升温至铝、钛全部熔化,再搅拌4min;Cooling to 1370 ± 10 ° C, adding aluminum, titanium, heating to aluminum, titanium all melted, and then stirred for 4 min;

(5)加入镍硼合金、锆:(5) Adding nickel-boron alloy and zirconium:

保持温度1430±10℃,向其中加入镍硼合金、锆,升温至镍硼合金熔化,再搅拌4min; Maintaining a temperature of 1430 ± 10 ° C, adding nickel boron alloy, zirconium, heating to nickel boron alloy melting, and stirring for 4 min;

(6)冷冻金属熔液、过滤、出钢浇注:(6) Frozen metal melt, filtration, tapping and pouring:

降温,待温度降至1380±10℃,再升温至1450±10℃,采用陶瓷过滤器一边过滤一边出钢浇注。Cool down, wait until the temperature drops to 1380 ± 10 ° C, and then heat up to 1450 ± 10 ° C, using a ceramic filter while filtering and tapping.

加入铝、钛、镍硼合金、锆时的真空度≤0.1Pa。其余如实施例1。The degree of vacuum when adding aluminum, titanium, nickel boron alloy, or zirconium is ≤ 0.1 Pa. The rest is as in Example 1.

表5实施例3合金成分参数表Table 5 Example 3 alloy composition parameter table

元素element CC SiSi MnMn PP SS CrCr FeFe 范围range 0.03/0.070.03/0.07 ≤0.50≤0.50 ≤0.25≤0.25 ≤0.015≤0.015 ≤0.015≤0.015 11.0/13.011.0/13.0 ≤0.5≤0.5 实测Measured 0.0570.057 0.0410.041 0.0490.049 0.00610.0061 0.00140.0014 11.9511.95 0.170.17 元素element MoMo CuCu NbNb TiTi CoCo AlAl ZrZr 范围range 3.80/5.203.80/5.20 ≤0.5≤0.5 1.50/2.501.50/2.50 0.40/1.000.40/1.00 ≤1.0≤1.0 5.50/6.505.50/6.50 0.05/0.150.05/0.15 实测Measured 4.824.82 0.0390.039 2.352.35 0.850.85 0.580.58 6.256.25 0.0910.091 元素element BB PbPb AgAg BiBi NiNi O ppmO ppm N ppmN ppm 范围range 0.005/0.0150.005/0.015 ≤0.0010≤0.0010 ≤0.0005≤0.0005 ≤0.00020≤0.00020 Yu ———— ———— 实测Measured 0.0090.99 0.00060.0006 0.000040.00004 0.000030.00003 Yu 7.67.6 6.76.7

用德国进口ON900型氧氮分析仪测定:氧(O)7.6ppm氮(N)6.7ppm。It was measured by a German imported ON900 type oxygen nitrogen analyzer: oxygen (O) 7.6 ppm nitrogen (N) 6.7 ppm.

表6实施例3合金性能参数表Table 6 Example 3 alloy performance parameter table

室温拉伸性能Room temperature tensile properties σb/MPaσ b /MPa σ0.2/MPaσ 0.2 /MPa δS/%δ S /% 标准standard ≥760≥760 ≥690≥690 ≥5.0≥5.0 实测Measured 890890 764764 7.77.7

Figure PCTCN2017074564-appb-000003
Figure PCTCN2017074564-appb-000003

通过表1-6可以看出,K418B合金中氧、氮的含量很低。由于采用了二次加碳深脱氧工艺、金属钙脱氧工艺、合金化工艺、冷冻金属熔液工艺、过滤工艺,合金中的其它有害杂质含量明显下降。最为突出的是合金的室温拉伸性能和高温持久性能都有很大地提高。 As can be seen from Table 1-6, the content of oxygen and nitrogen in the K418B alloy is very low. Due to the secondary carbon deep deoxidation process, the metal calcium deoxidation process, the alloying process, the frozen metal melt process, and the filtration process, the content of other harmful impurities in the alloy is significantly reduced. The most prominent is that the alloy's room temperature tensile properties and high temperature durability are greatly improved.

Claims (9)

一种含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于包括以下步骤:A smelting process for a nickel-based alloy containing aluminum titanium boron zirconia, comprising the steps of: (1)第一步碳脱氧:(1) First step carbon deoxidation: 将占高温合金总含碳质量50%的石墨加入到真空炉坩埚内,置于坩埚最底部,向真空炉坩埚内加入除铝、钛、硼、锆、镍之外的高温合金中的所有元素进行冶炼;Adding 50% of the total carbon content of the superalloy to the vacuum furnace, placing it at the bottom of the crucible, adding all the elements in the superalloy except aluminum, titanium, boron, zirconium and nickel into the vacuum furnace. Smelting; (2)第二步碳脱氧:(2) The second step of carbon deoxidation: 温度升至1570~1590℃,向坩埚内加入剩余的石墨,精炼,之后降温;The temperature is raised to 1570 ~ 1590 ° C, the remaining graphite is added to the crucible, refined, and then cooled; (3)金属钙脱氧:(3) Metal calcium deoxidation: 加入金属钙,全部熔化后,升温至1550~1570℃,进行精炼,精炼过程中摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部;Adding metal calcium, after melting all, heating to 1550 ~ 1570 ° C, refining, shaking in the refining process, so that the floating slag floating up to the molten metal surface is discharged to the back of the wall; (4)加入铝、钛:(4) Add aluminum and titanium: 降温至1370~1390℃,向其中加入铝、钛,升温至铝、钛全部熔化;Cooling to 1370 ~ 1390 ° C, adding aluminum, titanium, heating up to aluminum, titanium all melted; (5)加入镍硼合金、锆:(5) Adding nickel-boron alloy and zirconium: 保持温度1410~1430℃,向其中加入镍硼合金、锆,升温至镍硼合金、锆全部熔化;Maintaining a temperature of 1410 to 1430 ° C, adding a nickel-boron alloy and zirconium thereto, and heating the mixture to a nickel-boron alloy and zirconium; (6)冷冻金属熔液、过滤、出钢浇注:(6) Frozen metal melt, filtration, tapping and pouring: 降温,待温度降至1360~1380℃,再升温至1450~1470℃,采用陶瓷过滤器一边过滤一边出钢浇注。Cool down, wait until the temperature drops to 1360 ~ 1380 ° C, and then heat up to 1450 ~ 1470 ° C, using a ceramic filter while filtering and tapping. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(1)石墨为光谱石墨电极破碎至2~5mm的颗粒。The smelting process for a nickel-based alloy containing aluminum-titanium-boron-zirconium according to claim 1, wherein the step (1) graphite is a particle in which the spectral graphite electrode is broken to 2 to 5 mm. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(1)冶炼温度1560~1580℃,冶炼时间20~30min。The smelting process of the aluminum-based boron-zirconium-containing nickel-based alloy according to claim 1, characterized in that the step (1) smelting temperature is 1560 to 1580 ° C, and the smelting time is 20 to 30 min. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(2)温度升至1570~1590℃,向坩埚内加入剩余的石墨,于功率80KW下精炼20~30min。The smelting process of the aluminum-based boron-zirconium-containing nickel-based alloy according to claim 1, wherein the temperature of the step (2) is raised to 1570 to 1590 ° C, and the remaining graphite is added to the crucible, and refined at a power of 80 KW. ~30min. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(3)加入的金属钙全部熔化后,再将温度升至1550~1570℃,于80KW下进行精炼10min,精炼5min时,开始摇动坩埚,使得上浮到金属熔液液面的浮渣排到坩埚壁的后部。The smelting process of a nickel-based alloy containing aluminum titanium borate and zirconium according to claim 1, wherein after the metal calcium added in the step (3) is completely melted, the temperature is raised to 1550 to 1570 ° C, and the temperature is 80 KW. After refining for 10 min, when refining for 5 min, the crucible is started to be shaken, so that the scum floating up to the molten metal level is discharged to the rear of the crucible wall. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(3)金属钙的用量为高温合金总质量的0.02~0.05%。The smelting process for a nickel-based alloy containing aluminum-titanium-boron-zirconium according to claim 1, wherein the amount of the metal calcium in the step (3) is 0.02 to 0.05% of the total mass of the high-temperature alloy. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(4)升温至铝、钛全部熔化后,再搅拌3~5min。The smelting process of the aluminum-based boron-zirconium-containing nickel-based alloy according to claim 1, wherein the step (4) is heated until the aluminum and the titanium are all melted, and then stirred for 3 to 5 minutes. 根据权利要求1所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:步骤(5)升温至镍硼合金、锆全部熔化后,再搅拌3~5min。 The smelting process of the aluminum-based boron-zirconium-containing nickel-based alloy according to claim 1, wherein the step (5) is heated until the nickel-boron alloy and the zirconium are all melted, and then stirred for 3 to 5 minutes. 根据权利要求1~8任一所述的含有铝钛硼锆的镍基合金的冶炼工艺,其特征在于:加入铝、钛、镍硼合金、锆时的真空度≤0.1Pa。 The smelting process for a nickel-based alloy containing aluminum-titanium-boron-zirconium according to any one of claims 1 to 8, characterized in that the degree of vacuum when aluminum, titanium, nickel-boron alloy or zirconium is added is ≤ 0.1 Pa.
PCT/CN2017/074564 2016-03-30 2017-02-23 Melting process for nickel-based alloy containing aluminum, titanium, boron, and zirconium Ceased WO2017166962A1 (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110408803A (en) * 2019-07-31 2019-11-05 江苏美特林科特殊合金股份有限公司 A kind of sublimate method of smelting for nickel base superalloy master alloy
CN113981293A (en) * 2021-10-29 2022-01-28 承德天大钒业有限责任公司 Aluminum-molybdenum-zirconium intermediate alloy and preparation method thereof
CN114892012A (en) * 2022-04-25 2022-08-12 中国航发成都发动机有限公司 Remelting purification method of nickel-based superalloy return material
CN115232996A (en) * 2022-06-20 2022-10-25 中国航发哈尔滨东安发动机有限公司 ZL105A aluminum alloy smelting method
CN115323206A (en) * 2022-07-20 2022-11-11 中国航发北京航空材料研究院 A smelting process for accurately controlling the content of trace element boron in GH4169D alloy
CN116949309A (en) * 2023-09-20 2023-10-27 江苏美特林科特殊合金股份有限公司 Method for preparing porous superalloy
CN117646127A (en) * 2023-12-01 2024-03-05 美特林科航空科技(安徽)有限公司 Purifying smelting method for carbon-free nickel-based monocrystal superalloy

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106636757B (en) * 2016-12-29 2018-11-06 西部超导材料科技股份有限公司 A kind of nickel base superalloy multistage deoxidation vacuum induction melting method
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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4144057A (en) * 1976-08-26 1979-03-13 Bbc Brown, Boveri & Company, Limited Shape memory alloys
JPS61210141A (en) * 1985-03-14 1986-09-18 Mitsui Eng & Shipbuild Co Ltd Ni-ti alloy having superior shock resistance and its manufacture
RU2353688C1 (en) * 2007-12-29 2009-04-27 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Melting method of carbon-free foundry heat-resistant alloys on basis of nickel
CN101586202A (en) * 2009-06-15 2009-11-25 袁书强 High-temperature alloy material and a method of producing the same
CN101994019A (en) * 2010-10-22 2011-03-30 沈阳黎明航空发动机(集团)有限责任公司 Method for preparing nickel-based alloy by stepwise adding carbon in melting process
CN102719686A (en) * 2012-06-29 2012-10-10 山西太钢不锈钢股份有限公司 Method for smelting nickel-based high temperature alloy in vacuum induction furnace

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1098027A (en) * 1993-07-24 1995-02-01 冶金工业部长沙矿冶研究院 Catalyst for self-sharpening diamond and its preparing process
CN1137275C (en) * 2000-12-21 2004-02-04 中国科学院金属研究所 High-temp vacuum induction smelting and desulfurizing technology for preparing super-purity alloy
CN1210422C (en) * 2003-05-09 2005-07-13 沈阳黎明航空发动机(集团)有限责任公司 Method for producing high-temp.-and wear-resistant high strength alloy
US10266926B2 (en) * 2013-04-23 2019-04-23 General Electric Company Cast nickel-base alloys including iron
CN104018015B (en) * 2014-06-13 2016-03-30 四川法拉特不锈钢铸造有限公司 A kind of smelting degassing method of nickel alloy solution

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4144057A (en) * 1976-08-26 1979-03-13 Bbc Brown, Boveri & Company, Limited Shape memory alloys
JPS61210141A (en) * 1985-03-14 1986-09-18 Mitsui Eng & Shipbuild Co Ltd Ni-ti alloy having superior shock resistance and its manufacture
RU2353688C1 (en) * 2007-12-29 2009-04-27 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Melting method of carbon-free foundry heat-resistant alloys on basis of nickel
CN101586202A (en) * 2009-06-15 2009-11-25 袁书强 High-temperature alloy material and a method of producing the same
CN101994019A (en) * 2010-10-22 2011-03-30 沈阳黎明航空发动机(集团)有限责任公司 Method for preparing nickel-based alloy by stepwise adding carbon in melting process
CN102719686A (en) * 2012-06-29 2012-10-10 山西太钢不锈钢股份有限公司 Method for smelting nickel-based high temperature alloy in vacuum induction furnace

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110408803A (en) * 2019-07-31 2019-11-05 江苏美特林科特殊合金股份有限公司 A kind of sublimate method of smelting for nickel base superalloy master alloy
CN110408803B (en) * 2019-07-31 2020-11-03 江苏美特林科特殊合金股份有限公司 Purification smelting method for nickel-based high-temperature alloy master alloy
CN113981293A (en) * 2021-10-29 2022-01-28 承德天大钒业有限责任公司 Aluminum-molybdenum-zirconium intermediate alloy and preparation method thereof
CN114892012A (en) * 2022-04-25 2022-08-12 中国航发成都发动机有限公司 Remelting purification method of nickel-based superalloy return material
CN115232996A (en) * 2022-06-20 2022-10-25 中国航发哈尔滨东安发动机有限公司 ZL105A aluminum alloy smelting method
CN115232996B (en) * 2022-06-20 2023-11-28 中国航发哈尔滨东安发动机有限公司 ZL105A aluminum alloy smelting method
CN115323206A (en) * 2022-07-20 2022-11-11 中国航发北京航空材料研究院 A smelting process for accurately controlling the content of trace element boron in GH4169D alloy
CN116949309A (en) * 2023-09-20 2023-10-27 江苏美特林科特殊合金股份有限公司 Method for preparing porous superalloy
CN116949309B (en) * 2023-09-20 2023-12-01 江苏美特林科特殊合金股份有限公司 Method for preparing porous superalloy
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