CN111318835A - Nickel-based alloy welding wire for high-temperature alloy fusion welding and preparation method and application thereof - Google Patents
Nickel-based alloy welding wire for high-temperature alloy fusion welding and preparation method and application thereof Download PDFInfo
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- 238000003466 welding Methods 0.000 title claims abstract description 162
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title claims abstract description 106
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 76
- 239000000956 alloy Substances 0.000 title claims abstract description 76
- 229910052759 nickel Inorganic materials 0.000 title claims abstract description 52
- 230000004927 fusion Effects 0.000 title claims abstract description 51
- 238000002360 preparation method Methods 0.000 title abstract description 10
- 229910000601 superalloy Inorganic materials 0.000 claims abstract description 45
- 238000000034 method Methods 0.000 claims abstract description 25
- 239000000463 material Substances 0.000 claims abstract description 22
- 238000007711 solidification Methods 0.000 claims abstract description 13
- 230000008023 solidification Effects 0.000 claims abstract description 13
- 239000000126 substance Substances 0.000 claims abstract description 11
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 14
- 239000000919 ceramic Substances 0.000 claims description 13
- 238000002844 melting Methods 0.000 claims description 12
- 230000008018 melting Effects 0.000 claims description 12
- 239000007788 liquid Substances 0.000 claims description 10
- 239000010953 base metal Substances 0.000 claims description 9
- 238000010438 heat treatment Methods 0.000 claims description 6
- 230000006698 induction Effects 0.000 claims description 5
- 230000002045 lasting effect Effects 0.000 claims description 4
- 238000003723 Smelting Methods 0.000 claims description 3
- 239000013078 crystal Substances 0.000 claims description 3
- 238000009617 vacuum fusion Methods 0.000 claims description 2
- 238000001556 precipitation Methods 0.000 claims 3
- 238000005728 strengthening Methods 0.000 claims 3
- 239000000203 mixture Substances 0.000 abstract description 17
- 229910052782 aluminium Inorganic materials 0.000 abstract description 8
- 229910052804 chromium Inorganic materials 0.000 abstract description 7
- 229910052742 iron Inorganic materials 0.000 abstract description 6
- 229910052750 molybdenum Inorganic materials 0.000 abstract description 6
- 229910052758 niobium Inorganic materials 0.000 abstract description 6
- 229910052721 tungsten Inorganic materials 0.000 abstract description 5
- 230000007547 defect Effects 0.000 abstract description 4
- 238000005266 casting Methods 0.000 abstract description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 10
- 230000000052 comparative effect Effects 0.000 description 6
- 229910000679 solder Inorganic materials 0.000 description 6
- 230000032683 aging Effects 0.000 description 5
- 239000002981 blocking agent Substances 0.000 description 5
- 238000000227 grinding Methods 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 239000006104 solid solution Substances 0.000 description 5
- 230000035945 sensitivity Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005495 investment casting Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
- 241001062472 Stokellia anisodon Species 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3033—Ni as the principal constituent
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
- B23K31/02—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to soldering or welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
- B23K35/0261—Rods, electrodes, wires
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/40—Making wire or rods for soldering or welding
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- Mechanical Engineering (AREA)
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Abstract
本发明公开了一种高温合金熔化焊用镍基合金焊丝及其制备方法和应用,属于高温合金熔化焊材料技术领域。该焊丝化学成分(wt.%):C 0~1%,Cr 5.0~25.0%,Co 1.5~25.5%,Al 1~12.5%,W 0.5~20.5%,Mo 1.5~10.5%,Nb 0.8~12.5%,Y 0~1.0%,Fe 0~1.0%,Si 0~2.0%,Ni为余量。该焊丝采用定向凝固法制备,用于高温合金熔化焊连接。焊接电流为20‑35A,电压为10‑12V。本发明解决了沉淀强化镍基高温合金的铸造缺陷修复问题,以及镍基高温合金抗变形性强导致镍基高温合金焊丝难以制备的现状,具有重要的应用价值。The invention discloses a nickel-based alloy welding wire for high-temperature alloy fusion welding, a preparation method and application thereof, and belongs to the technical field of high-temperature alloy fusion welding materials. The chemical composition of the welding wire (wt.%): C 0~1%, Cr 5.0~25.0%, Co 1.5~25.5%, Al 1~12.5%, W 0.5~20.5%, Mo 1.5~10.5%, Nb 0.8~12.5 %, Y 0-1.0%, Fe 0-1.0%, Si 0-2.0%, Ni is the balance. The welding wire is prepared by the directional solidification method and is used for fusion welding of high temperature alloys. The welding current is 20‑35A and the voltage is 10‑12V. The invention solves the problem of repairing the casting defects of the precipitation-strengthened nickel-based superalloy and the current situation that the nickel-based superalloy is difficult to prepare due to the strong deformation resistance of the nickel-based superalloy, and has important application value.
Description
技术领域technical field
本发明涉及高温合金连接技术领域,具体涉及一种高温合金熔化焊用镍基合金焊丝及其制备方法和应用,该焊丝适用于高温合金熔化焊连接。The invention relates to the technical field of high-temperature alloy connection, in particular to a nickel-based alloy welding wire for high-temperature alloy fusion welding, a preparation method and application thereof, and the welding wire is suitable for high-temperature alloy fusion welding connection.
背景技术Background technique
随着整体精密铸造技术的发展,铸造高温合金逐渐在航空航天产业大量应用。但随着先进航空发动机涡轮前进气口温度及推重比越来越高,以及对发动机减重的要求越来越严格。由于高温合金结构件的结构越来越复杂,精密度越来越高,制造难度增大,单凭精密铸造无法实现最终结构,必须与可靠的焊接技术及其它先进的加工制造技术相结合,才可以实现高温合金结构件分体铸造。另外,熔化焊方法不仅可以实现高温合金结构件的连接,还可以实现缺陷的修复,有效提高航空发动机的工作可靠性和经济性。一般而言,镍基高温合金具有优良的高温性能,但高温合金中含有较高焊料的Al、Ti及W、Mo等高熔点元素,熔焊过程中易形成裂纹,可焊性差,而镍基高温合金结构件的焊接位置必须具有优良的承温能力,不能有焊接缺陷。我国现有的焊丝中,可用于高温合金,特别是高温性能优良的镍基高温合金熔化焊的焊丝较少,只要是因为焊接高温合金过程中容易形成裂纹,无法满足使用要求。而且,高温合金高性能焊接的焊丝材料通常化学成分与高温合金相似,高温强度优良,高温抗变形能力强,不能通过传统的拉拔方法制备成丝材。因此,迫切需要开发一种高温合金熔化焊用镍基合金焊丝材料满足高温合金零部件的焊接要求。With the development of integral precision casting technology, cast superalloys are gradually being widely used in the aerospace industry. However, as the air inlet temperature and thrust-weight ratio before the turbine of advanced aero-engines become higher and higher, and the requirements for engine weight reduction are becoming more and more stringent. As the structure of superalloy structural parts is becoming more and more complex, the precision is getting higher and higher, and the manufacturing difficulty is increasing. The final structure cannot be realized by precision casting alone, and must be combined with reliable welding technology and other advanced manufacturing It can realize the split casting of superalloy structural parts. In addition, the fusion welding method can not only realize the connection of the superalloy structural parts, but also realize the repair of defects, which can effectively improve the working reliability and economy of the aero-engine. In general, nickel-based superalloys have excellent high-temperature performance, but superalloys contain high melting point elements such as Al, Ti, W, and Mo, which are relatively high in solder. The welding position of superalloy structural parts must have excellent temperature bearing capacity, and there must be no welding defects. Among the existing welding wires in my country, there are few welding wires that can be used for high-temperature alloys, especially nickel-based high-temperature alloys with excellent high-temperature performance. As long as cracks are easily formed during welding of high-temperature alloys, they cannot meet the requirements for use. Moreover, the welding wire materials for high-performance welding of superalloys are usually similar in chemical composition to superalloys, have excellent high-temperature strength, and have strong high-temperature deformation resistance, and cannot be prepared into wires by traditional drawing methods. Therefore, it is urgent to develop a nickel-based alloy wire material for superalloy fusion welding to meet the welding requirements of superalloy parts.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种高温合金熔化焊用镍基合金焊丝材料及制备方法,所制备的焊丝成分与镍基高温合金母材相似,可有效解决在苛刻环境应用的高温合金机匣等零部件的连接和修复问题,具有重要应用价值。The purpose of the present invention is to provide a nickel-based alloy welding wire material for high-temperature alloy fusion welding and a preparation method. The prepared welding wire has a composition similar to that of the nickel-based high-temperature alloy base material, which can effectively solve the problems of high-temperature alloy casings and other parts used in harsh environments. The connection and repair of components has important application value.
为实现上述目的,本发明的技术方案如下:For achieving the above object, technical scheme of the present invention is as follows:
一种高温合金熔化焊用镍基合金焊丝,该焊丝为镍基合金丝材,按重量百分含量计,该焊丝的化学成分如下:A nickel-based alloy welding wire for high-temperature alloy fusion welding, the welding wire is a nickel-based alloy wire, and the chemical composition of the welding wire is as follows in terms of weight percentage:
C 0~1%,Cr 5.0~25.0%,Co 1.5~25.5%,Al 1~12.5%,W 0.5~20.5%,Mo1.5~10.5%,Nb 0.8~12.5%,Y 0~1.0%,Fe 0~1.0%,Si 0~2.0%,Ni为余量。C 0~1%, Cr 5.0~25.0%, Co 1.5~25.5%, Al 1~12.5%, W 0.5~20.5%, Mo1.5~10.5%, Nb 0.8~12.5%, Y 0~1.0%, Fe 0 to 1.0%, Si 0 to 2.0%, and Ni is the balance.
按重量百分含量计,该焊丝优选的化学成分如下:By weight percentage, the preferred chemical composition of the welding wire is as follows:
C 0.1~1%,Cr 5.0~25.0%,Co 1.5~25.5%,Al 1~12.5%,W 0.5~20.5%,Mo 1.5~10.5%,Nb 0.8~12.5%,Y 0.1~1.0%,Fe 0.1~1.0%,Si 0.5~2.0%,Ni为余量。C 0.1~1%, Cr 5.0~25.0%, Co 1.5~25.5%, Al 1~12.5%, W 0.5~20.5%, Mo 1.5~10.5%, Nb 0.8~12.5%, Y 0.1~1.0%, Fe 0.1 ~1.0%, Si 0.5~2.0%, Ni is the balance.
所述焊丝为直径1-2mm的圆柱形丝材,长度大于200mm。The welding wire is a cylindrical wire with a diameter of 1-2 mm and a length greater than 200 mm.
所述高温合金熔化焊用镍基合金焊丝的制备方法,包括如下步骤:The preparation method of the nickel-based alloy welding wire for high-temperature alloy fusion welding includes the following steps:
(1)按照所述焊丝的化学成分配料,采用真空感应炉熔炼出母合金锭;(1) according to the chemical composition batching of described welding wire, adopt vacuum induction furnace to smelt out master alloy ingot;
(2)将母合金锭采用定向凝固炉熔化,将熔化的母合金熔体浇注在氧化铝陶瓷型壳中,注满后,将陶瓷型壳以一定速度从炉中抽拉进入室温真空室内,实现焊丝的定向凝固;(2) The master alloy ingot is melted in a directional solidification furnace, and the molten master alloy melt is poured into an alumina ceramic shell. After filling, the ceramic shell is pulled from the furnace at a certain speed into a room temperature vacuum chamber, To achieve directional solidification of the welding wire;
(3)将凝固冷却的陶瓷型壳破碎,取出焊丝,去除焊丝在无心磨上去除氧化皮,即获得所述焊丝产品。(3) Breaking the solidified and cooled ceramic shell, taking out the welding wire, removing the welding wire and removing the oxide scale on the centerless grinding, thus obtaining the welding wire product.
步骤(1)中,所述熔炼过程为:先升温至1550~1600℃保温1min,然后升温至1450~1550℃保温10min,再升温至1300~1400℃保温10min,1400~1450℃浇注。In step (1), the smelting process is as follows: firstly heating to 1550-1600°C for 1 min, then heating to 1450-1550°C for 10min, then heating to 1300-1400°C for 10min, and pouring at 1400-1450°C.
步骤(2)中,所述熔化温度为1400~1600℃,熔化后的母合金液注入氧化铝陶瓷型壳。In step (2), the melting temperature is 1400-1600° C., and the molten master alloy liquid is injected into the alumina ceramic shell.
步骤(2)中,所述氧化铝陶瓷型壳内部分布100-200个直径1.1-2.1mm的圆柱形空腔。In step (2), 100-200 cylindrical cavities with diameters of 1.1-2.1 mm are distributed inside the alumina ceramic shell.
步骤(2)中,所述将陶瓷型壳抽拉过程,控制抽拉速度为1~10mm/min,以保证焊丝的成型性。In step (2), in the process of pulling the ceramic shell, the pulling speed is controlled to be 1-10 mm/min, so as to ensure the formability of the welding wire.
所述高温合金熔化焊用镍基合金焊丝用于沉淀强化镍基高温合金的熔化焊,熔化焊连接过程中,将焊丝放置在两个待焊母材之间,用夹具固定后,将固定夹装好的样品放置于真空熔化焊炉内进行熔化焊,焊接电流为20-35A,电压为10-12V。The nickel-based alloy welding wire for fusion welding of superalloys is used for fusion welding of precipitation-strengthened nickel-based superalloys. During the fusion welding process, the welding wire is placed between two base metals to be welded, and after being fixed with a clamp, the fixing clamp is The loaded sample is placed in a vacuum fusion welding furnace for fusion welding, the welding current is 20-35A, and the voltage is 10-12V.
所述熔化焊连接后,连接接头内无晶界,焊缝区成分与所需连接沉淀强化镍基高温合金相似,抗拉强度可以达到沉淀强化镍基高温合金的80%以上,980℃、66MPa的持久寿命≥100h。After the fusion welding connection, there is no grain boundary in the connection joint, and the composition of the weld zone is similar to that of the precipitation-strengthened nickel-based superalloy to be connected. The lasting life of ≥ 100h.
本发明设计思想及原理如下:The design idea and principle of the present invention are as follows:
为解决沉淀强化镍基高温合金的铸造缺陷修复问题,研发一种镍基高温合金用高性能焊丝材料,该焊丝成分与沉淀强化镍基合金相似,因此具有和镍基高温合金匹配的焊缝强度。但是,针对镍基高温合金抗变形性强,使得镍基高温合金焊丝难以制备的现状,本发明在成分设计方面,在一定范围内,降低了Al、W等增加裂纹敏感性的元素,提高Cr、Co等增加合金塑性和降低裂纹敏感性的元素,此外,考虑到Nb取代Ta有利于提高塑性,C的添加略微提高了热影响区裂纹敏感性,而B的添加明显提高了裂纹敏感性,适当调控几种元素的含量,从而获得了焊接强度高,焊接性良好的焊丝材料。In order to solve the problem of repairing casting defects of precipitation-strengthened nickel-based superalloys, a high-performance welding wire material for nickel-based superalloys was developed. The composition of the welding wire is similar to that of precipitation-strengthened nickel-based superalloys. . However, in view of the current situation that nickel-based superalloys have strong deformation resistance, making it difficult to prepare nickel-based superalloy welding wires, the present invention, in terms of component design, reduces elements that increase crack sensitivity such as Al and W within a certain range, and improves Cr , Co and other elements that increase the plasticity of the alloy and reduce the crack sensitivity. In addition, considering that Nb replaces Ta is beneficial to improve the plasticity, the addition of C slightly increases the crack sensitivity of the heat-affected zone, while the addition of B significantly improves the crack sensitivity. The content of several elements is properly adjusted, so as to obtain the welding wire material with high welding strength and good weldability.
本发明的有益效果是:The beneficial effects of the present invention are:
采用本发明制备的镍基高温合金焊丝及熔化焊工艺,所得焊接接头中不存在裂纹,避免高温使役条件下产生失效,且熔化焊温度高、流动性适中、对基体材料溶蚀小,焊接接头的力学性能与基体材料接近,与传统高温熔化焊材料相比,本发明熔化焊材料更适宜于镍基单晶高温合金的熔化焊。By adopting the nickel-based superalloy welding wire and the fusion welding process prepared by the invention, there are no cracks in the obtained welded joints, so as to avoid failure under high-temperature service conditions, and the melting welding temperature is high, the fluidity is moderate, and the corrosion to the base material is small, and the welding joints are less corrosive. The mechanical properties are close to the base material, and compared with the traditional high-temperature fusion welding material, the fusion welding material of the present invention is more suitable for fusion welding of nickel-based single crystal superalloy.
附图说明Description of drawings
图1为采用实施例1制备的焊丝熔化焊K4951合金的接头显微组织;其中:(a)为微观形貌;(b)为宏观照片。Fig. 1 shows the microstructure of the joint of K4951 alloy by fusion welding of the welding wire prepared in Example 1; wherein: (a) is the microscopic appearance; (b) is a macroscopic photo.
图2为对比例1中熔化焊K4951合金的接头显微组织。FIG. 2 shows the joint microstructure of fusion-welded K4951 alloy in Comparative Example 1. FIG.
图3为对比例2中熔化焊K4951合金的接头显微组织。FIG. 3 shows the joint microstructure of fusion-welded K4951 alloy in Comparative Example 2. FIG.
具体实施方式Detailed ways
以下结合附图和实施例详述本发明。The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
实施例1Example 1
本实施例待焊母材为镍基高温合金K4951。The base material to be welded in this embodiment is a nickel-based superalloy K4951.
本实施例焊丝化学成分为(wt.%):C 0.8%,Cr 15.0%,Co 15.5%,Al 8.5%,W5.5%,Mo 4.5%,Nb 4.5%,Y 0.5%,Fe 0.5%,Si 0.5%,其余为Ni,通过真空熔炼炉熔炼母合金锭,采用真空感应炉熔炼出母合金锭,熔炼过程为:1550℃/1min→1450℃/10min→1300℃/10min,1400℃浇注,制得母合金锭。The chemical composition of the welding wire in this embodiment is (wt.%): C 0.8%, Cr 15.0%, Co 15.5%, Al 8.5%, W5.5%, Mo 4.5%, Nb 4.5%, Y 0.5%, Fe 0.5%, Si 0.5%, the rest is Ni, the master alloy ingot is smelted by a vacuum melting furnace, and the master alloy ingot is smelted by a vacuum induction furnace. A master alloy ingot was prepared.
焊丝制备方法:将母合金锭采用定向凝固炉熔化,熔炼温度为1400℃,将熔化的母合金液体通过出液口进入空腔直径为2.1mm的氧化铝陶瓷型壳中,注满后,将陶瓷型壳拉出,拉出速度为1mm/min,进行定向凝固;将凝固冷却的陶瓷型壳破碎,取出焊丝,将焊丝在无心磨上去除氧化皮,即获得所述直径为2mm的焊丝材料。Welding wire preparation method: The master alloy ingot is melted in a directional solidification furnace, and the melting temperature is 1400 ° C. The molten master alloy liquid enters the alumina ceramic shell with a cavity diameter of 2.1 mm through the liquid outlet. The ceramic shell is pulled out, and the pull-out speed is 1mm/min, and the directional solidification is carried out; the solidified and cooled ceramic shell is broken, the welding wire is taken out, and the oxide scale is removed on the welding wire on the centerless grinding, that is, the welding wire material with a diameter of 2 mm is obtained. .
焊接方法:焊接前,将固溶态镍基高温合金K4951的样品,使用800号砂纸打磨待焊接面,在丙酮中超声波清洗15min以去除待焊样品表面油污,将焊丝置于待焊母材之间,用夹具固定后,在样品外表涂抹阻流剂氧化铝粉防止熔化焊过程中焊料流失,焊接时,采用焊接电流为20A,电压为10V。并进行时效处理。熔化焊连接后,连接接头内无晶界,焊缝区成分与K4951合金相似,抗拉强度为K4951合金的80%,980℃/66MPa持久寿命为125h。Welding method: Before welding, a sample of solid solution nickel-based superalloy K4951 was polished with 800 grit sandpaper on the surface to be welded, ultrasonically cleaned in acetone for 15 minutes to remove the oil stain on the surface of the sample to be welded, and the welding wire was placed on the base metal to be welded. During the time, after fixing with a fixture, smear the surface of the sample with aluminum oxide powder as a flow blocking agent to prevent the loss of solder during the fusion welding process. During welding, the welding current is 20A and the voltage is 10V. and aging treatment. After fusion welding, there is no grain boundary in the joint, the composition of the weld zone is similar to that of K4951 alloy, the tensile strength is 80% of that of K4951 alloy, and the durable life at 980℃/66MPa is 125h.
实施例2Example 2
本实施例待焊母材为镍基高温合金K4951。The base material to be welded in this embodiment is a nickel-based superalloy K4951.
本实施例焊丝化学成分为(wt.%):C 0.5%,Cr 5.0%,Co 1.5%,Al 2.5%,W2.5%,Mo 1.5%,Nb 1.8%,Y 0.5%,Fe 0.5%,Si 0.3%,其余为Ni,通过真空熔炼炉熔炼母合金锭,采用真空感应炉熔炼出母合金锭,熔炼过程为:1600℃/1min→1550℃/10min→1400℃/10min,1450℃浇注。,制得母合金锭。The chemical composition of the welding wire in this embodiment is (wt.%): C 0.5%, Cr 5.0%, Co 1.5%, Al 2.5%, W2.5%, Mo 1.5%, Nb 1.8%, Y 0.5%, Fe 0.5%, Si 0.3%, the rest is Ni, the master alloy ingot is smelted by a vacuum melting furnace, and the master alloy ingot is smelted by a vacuum induction furnace. , the master alloy ingot was obtained.
焊丝制备方法:将母合金锭采用定向凝固炉熔化,熔炼温度为1600℃,将熔化的母合金液体通过出液口进入空腔直径为1.1mm的氧化铝陶瓷型壳中,注满后,将陶瓷型壳拉出,拉出速度为1mm/min,进行定向凝固;将凝固冷却的陶瓷型壳破碎,取出焊丝,将焊丝在无心磨上去除氧化皮,即获得所述直径为1mm的焊丝材料。Welding wire preparation method: The mother alloy ingot is melted in a directional solidification furnace, and the melting temperature is 1600 ° C. The molten mother alloy liquid enters the alumina ceramic shell with a cavity diameter of 1.1 mm through the liquid outlet. The ceramic shell is pulled out, and the pull-out speed is 1mm/min, and the directional solidification is carried out; the solidified and cooled ceramic shell is broken, the welding wire is taken out, and the oxide scale is removed from the welding wire on the centerless grinding, that is, the welding wire material with a diameter of 1 mm is obtained. .
焊接方法:焊接前,将固溶态镍基高温合金K4951的样品,使用800号砂纸打磨待焊接面,在丙酮中超声波清洗15min以去除待焊样品表面油污,将焊丝置于待焊母材之间,用夹具固定后,在样品外表涂抹阻流剂氧化铝粉防止熔化焊过程中焊料流失,焊接时,采用焊接电流为25A,电压为12V。并进行时效处理。熔化焊连接后,连接接头内无晶界,焊缝区成分与K4951合金相似,抗拉强度为K4951合金的85%,980℃/66MPa持久寿命为120h。Welding method: Before welding, a sample of solid solution nickel-based superalloy K4951 was polished with 800 grit sandpaper on the surface to be welded, ultrasonically cleaned in acetone for 15 minutes to remove the oil stain on the surface of the sample to be welded, and the welding wire was placed on the base metal to be welded. During the time, after fixing with a fixture, apply a flow blocking agent alumina powder on the surface of the sample to prevent the loss of solder during the fusion welding process. During welding, the welding current is 25A and the voltage is 12V. and aging treatment. After fusion welding, there is no grain boundary in the joint, and the composition of the weld zone is similar to that of K4951 alloy.
实施例3Example 3
本实施例待焊母材为镍基高温合金K4951。The base material to be welded in this embodiment is a nickel-based superalloy K4951.
本实施例焊丝化学成分为(wt.%):C 0.3%,Cr 10.0%,Co 2.5%,Al 4.5%,W7.5%,Mo 8.5%,Nb 7.5%,Y 0.5%,Fe 0.3%,Si0.5%,其余为Ni,通过真空熔炼炉熔炼母合金锭,采用真空感应炉熔炼出母合金锭,熔炼过程为:1575℃/1min→1475℃/10min→1350℃/10min→1450℃浇注,制得母合金锭。The chemical composition of the welding wire in this embodiment is (wt.%): C 0.3%, Cr 10.0%, Co 2.5%, Al 4.5%, W7.5%, Mo 8.5%, Nb 7.5%, Y 0.5%, Fe 0.3%, Si0.5%, the rest is Ni, the master alloy ingot is smelted by vacuum melting furnace, and the master alloy ingot is smelted by vacuum induction furnace. The melting process is: 1575℃/1min→1475℃/10min→1350℃/10min→1450℃ pouring , the master alloy ingot was obtained.
焊丝制备方法:将母合金锭采用定向凝固炉熔化,熔炼温度为1500℃,将熔化的母合金液体通过出液口进入空腔直径为1.9mm的氧化铝陶瓷型壳中,注满后,将陶瓷型壳拉出,拉出速度为1mm/min,进行定向凝固;将凝固冷却的陶瓷型壳破碎,取出焊丝,将焊丝在无心磨上去除氧化皮,即获得所述直径为1.8mm的焊丝材料。Welding wire preparation method: The mother alloy ingot is melted in a directional solidification furnace, and the melting temperature is 1500 ° C. The molten mother alloy liquid enters the alumina ceramic shell with a cavity diameter of 1.9 mm through the liquid outlet. The ceramic shell is pulled out, and the pull-out speed is 1 mm/min, and directional solidification is performed; the solidified and cooled ceramic shell is broken, the welding wire is taken out, and the oxide scale is removed on the welding wire on the centerless grinding, that is, the welding wire with a diameter of 1.8 mm is obtained. Material.
焊接方法:焊接前,将固溶态镍基高温合金K4951的样品,使用800号砂纸打磨待焊接面,在丙酮中超声波清洗15min以去除待焊样品表面油污,将焊丝置于待焊母材之间,用夹具固定后,在样品外表涂抹阻流剂氧化铝粉防止熔化焊过程中焊料流失,焊接时,采用焊接电流为22A,电压为10V。并进行时效处理。熔化焊连接后,连接接头内无晶界,焊缝区成分与K4951合金相似,抗拉强度为K4951合金的90%,980℃/66MPa持久寿命为110h。Welding method: Before welding, a sample of solid solution nickel-based superalloy K4951 was polished with 800 grit sandpaper on the surface to be welded, ultrasonically cleaned in acetone for 15 minutes to remove the oil stain on the surface of the sample to be welded, and the welding wire was placed on the base metal to be welded. During the time, after fixing with a fixture, smear the surface of the sample with aluminum oxide powder as a flow blocking agent to prevent the loss of solder during the fusion welding process. During welding, the welding current is 22A and the voltage is 10V. and aging treatment. After fusion welding, there is no grain boundary in the joint, and the composition of the weld zone is similar to that of K4951 alloy.
对比例1Comparative Example 1
本例待焊母材为镍基高温合金K4951。The base metal to be welded in this example is a nickel-based superalloy K4951.
焊丝制备方法:将K4951锭采用定向凝固炉熔化,熔炼温度为1450℃,将熔化的母合金液体通过出液口进入空腔直径为2.1mm的氧化铝陶瓷型壳中,注满后,将陶瓷型壳拉出,拉出速度为1mm/min,进行定向凝固;将凝固冷却的陶瓷型壳破碎,取出焊丝,将焊丝在无心磨上去除氧化皮,即获得所述直径为2mm的焊丝材料。Welding wire preparation method: The K4951 ingot is melted in a directional solidification furnace, and the melting temperature is 1450 ° C. The molten mother alloy liquid enters the alumina ceramic shell with a cavity diameter of 2.1 mm through the liquid outlet. The shell is pulled out at a pull-out speed of 1 mm/min, and directional solidification is carried out; the solidified and cooled ceramic shell is broken, the welding wire is taken out, and the oxide scale is removed on the welding wire on a centerless grinding, that is, the welding wire material with a diameter of 2 mm is obtained.
焊接前,将固溶态镍基高温合金K4951的样品,使用800号砂纸打磨待焊接面,在丙酮中超声波清洗15min以去除待焊样品表面油污,将焊丝置于待焊母材之间,用夹具固定后,在样品外表涂抹阻流剂氧化铝粉防止熔化焊过程中焊料流失,焊接时,采用焊接电流为22A,电压为10V。并进行时效处理。熔化焊连接后,连接接头内无晶界,焊缝区成分与K4951合金相似,抗拉强度为K4951合金的50%,980℃/66MPa持久寿命为60h。Before welding, the sample of solid solution nickel-based superalloy K4951 was polished with 800 grit sandpaper on the surface to be welded, ultrasonically cleaned in acetone for 15 minutes to remove the oil stain on the surface of the sample to be welded, and the welding wire was placed between the base metals to be welded. After the fixture is fixed, the surface of the sample is smeared with alumina powder as a flow blocking agent to prevent the loss of solder during the fusion welding process. During welding, the welding current is 22A and the voltage is 10V. and aging treatment. After fusion welding, there is no grain boundary in the joint, and the composition of the weld zone is similar to that of K4951 alloy.
对比例2Comparative Example 2
本例待焊母材为镍基高温合金K4951。The base metal to be welded in this example is a nickel-based superalloy K4951.
焊丝制备方法:将K4951锭采进行机械加工,得到焊丝材料。Welding wire preparation method: the K4951 ingot is machined to obtain welding wire material.
焊接前,将固溶态镍基高温合金K4951的样品,使用800号砂纸打磨待焊接面,在丙酮中超声波清洗15min以去除待焊样品表面油污,将焊丝置于待焊母材之间,用夹具固定后,在样品外表涂抹阻流剂氧化铝粉防止熔化焊过程中焊料流失,焊接时,采用焊接电流为22A,电压为10V。并进行时效处理。熔化焊连接后,连接接头内无晶界,焊缝区成分与K4951合金相似,抗拉强度为K4951合金的40%,980℃/66MPa持久寿命为40h。Before welding, the sample of solid solution nickel-based superalloy K4951 was polished with 800 grit sandpaper on the surface to be welded, ultrasonically cleaned in acetone for 15 minutes to remove the oil stain on the surface of the sample to be welded, and the welding wire was placed between the base metals to be welded. After the fixture is fixed, the surface of the sample is smeared with alumina powder as a flow blocking agent to prevent the loss of solder during the fusion welding process. During welding, the welding current is 22A and the voltage is 10V. and aging treatment. After fusion welding, there is no grain boundary in the joint, the composition of the weld zone is similar to that of K4951 alloy, the tensile strength is 40% of that of K4951 alloy, and the durable life at 980℃/66MPa is 40h.
由上述实施例中样品熔化焊接头的显微组织以及宏观照片可以看出(图1),焊接接头中不存在裂纹,避免了高温使役条件下发生失效。实施例焊接后的样品焊缝区成分与K4951合金相似,抗拉强度达到K4951合金的80%以上,980℃/66MPa持久寿命大于100h。说明与传统高温合金熔化焊材料相比,本发明熔化焊丝更适宜于镍基单晶高温合金的熔化焊。It can be seen from the microstructure and macroscopic photos of the fusion welded joint of the sample in the above embodiment (Fig. 1) that there is no crack in the welded joint, which avoids failure under high temperature service conditions. The composition of the welded seam area of the sample after welding in the example is similar to that of the K4951 alloy, the tensile strength reaches more than 80% of that of the K4951 alloy, and the lasting life at 980°C/66MPa is more than 100h. It shows that compared with the traditional superalloy fusion welding material, the fusion welding wire of the present invention is more suitable for the fusion welding of nickel-based single crystal superalloy.
由上述对比例中样品熔化焊接头的显微组织图中(图2-图3)可以看出,相较于实施例,其熔化焊接头中存在较多裂纹,这会导致接头的高温性能降低。由对比例中连接后样品抗拉强度测试结果可以看出,连接后焊接接头抗拉强度和持久寿命均无法满足接头的抗拉强度要求。It can be seen from the microstructure diagrams of the fusion welded joints of the samples in the above comparative examples (Figure 2-Figure 3) that compared with the examples, there are more cracks in the fusion welded joints, which will reduce the high temperature performance of the joints. . It can be seen from the tensile strength test results of the samples after connection in the comparative example that the tensile strength and lasting life of welded joints after connection cannot meet the tensile strength requirements of the joints.
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CN111958193A (en) * | 2020-09-14 | 2020-11-20 | 北京北冶功能材料有限公司 | Preparation method of alloy wire difficult to deform |
CN111958193B (en) * | 2020-09-14 | 2022-05-24 | 北京北冶功能材料有限公司 | Preparation method of alloy wire difficult to deform |
CN112410617A (en) * | 2020-11-17 | 2021-02-26 | 丹阳润泽新材料科技有限公司 | Nickel alloy welding wire and preparation method thereof |
CN112410617B (en) * | 2020-11-17 | 2022-04-12 | 丹阳润泽新材料科技有限公司 | Nickel alloy welding wire and preparation method thereof |
CN112522544A (en) * | 2020-11-19 | 2021-03-19 | 中国科学院金属研究所 | Grain boundary regulation and control method for improving weldability of cast high-temperature alloy and welding process |
CN112522544B (en) * | 2020-11-19 | 2022-02-01 | 中国科学院金属研究所 | Grain boundary regulation and control method for improving weldability of cast high-temperature alloy and welding process |
CN112518172A (en) * | 2020-11-24 | 2021-03-19 | 中国华能集团有限公司 | Nickel-cobalt-based high-temperature alloy welding wire |
CN113249619A (en) * | 2021-06-24 | 2021-08-13 | 北京科技大学 | Matrix component design method of delta-phase reinforced nickel-based superalloy |
CN113857718A (en) * | 2021-11-01 | 2021-12-31 | 中国航发沈阳黎明航空发动机有限责任公司 | Welding material for repairing directional alloy blade, preparation method and fusion welding repair method |
CN114888482A (en) * | 2022-05-09 | 2022-08-12 | 西南交通大学 | Design method of aluminum alloy welding wire |
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