CN115323281B - Fe-Cu-C base alloy material containing Al and Ti and preparation method thereof - Google Patents
Fe-Cu-C base alloy material containing Al and Ti and preparation method thereof Download PDFInfo
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- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 68
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 68
- 238000002360 preparation method Methods 0.000 title claims abstract description 18
- 239000000843 powder Substances 0.000 claims abstract description 116
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 81
- 239000010936 titanium Substances 0.000 claims abstract description 71
- 229910052742 iron Inorganic materials 0.000 claims abstract description 39
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 34
- 238000002156 mixing Methods 0.000 claims abstract description 34
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 31
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 30
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 26
- 235000021355 Stearic acid Nutrition 0.000 claims abstract description 26
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 26
- 239000010949 copper Substances 0.000 claims abstract description 26
- 239000000463 material Substances 0.000 claims abstract description 26
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000008117 stearic acid Substances 0.000 claims abstract description 26
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 25
- 229910052802 copper Inorganic materials 0.000 claims abstract description 25
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 claims abstract description 25
- 238000003825 pressing Methods 0.000 claims abstract description 25
- 238000005245 sintering Methods 0.000 claims abstract description 25
- 239000000314 lubricant Substances 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims abstract description 24
- 239000002994 raw material Substances 0.000 claims abstract description 18
- 239000002245 particle Substances 0.000 claims description 45
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 21
- 239000001257 hydrogen Substances 0.000 claims description 16
- 229910052739 hydrogen Inorganic materials 0.000 claims description 16
- 239000011812 mixed powder Substances 0.000 claims description 16
- 229910000838 Al alloy Inorganic materials 0.000 claims description 13
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 claims description 13
- KCZFLPPCFOHPNI-UHFFFAOYSA-N alumane;iron Chemical compound [AlH3].[Fe] KCZFLPPCFOHPNI-UHFFFAOYSA-N 0.000 claims description 11
- 230000006835 compression Effects 0.000 claims description 9
- 238000007906 compression Methods 0.000 claims description 9
- 239000004615 ingredient Substances 0.000 claims description 9
- IXQWNVPHFNLUGD-UHFFFAOYSA-N iron titanium Chemical compound [Ti].[Fe] IXQWNVPHFNLUGD-UHFFFAOYSA-N 0.000 claims description 9
- 230000001681 protective effect Effects 0.000 claims description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 8
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 7
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 claims description 7
- 230000001590 oxidative effect Effects 0.000 claims description 5
- 229910052757 nitrogen Inorganic materials 0.000 claims description 4
- 238000007254 oxidation reaction Methods 0.000 abstract description 58
- 230000003647 oxidation Effects 0.000 abstract description 57
- 238000004663 powder metallurgy Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 9
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- 101710171920 Fumarate reductase flavoprotein subunit Proteins 0.000 description 5
- NOXUYEBNEVPERW-UHFFFAOYSA-N fcc5 Chemical compound Cl.C1C2=CC=CC=C2N2CCN(C(=N)N)CC2C2=CC=CC=C21 NOXUYEBNEVPERW-UHFFFAOYSA-N 0.000 description 5
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
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- 229910052751 metal Inorganic materials 0.000 description 4
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- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- 150000002431 hydrogen Chemical class 0.000 description 3
- RYYKJJJTJZKILX-UHFFFAOYSA-M sodium octadecanoate Chemical compound [Na+].CCCCCCCCCCCCCCCCCC([O-])=O RYYKJJJTJZKILX-UHFFFAOYSA-M 0.000 description 3
- 229910018575 Al—Ti Inorganic materials 0.000 description 2
- 125000004122 cyclic group Chemical group 0.000 description 2
- 238000000724 energy-dispersive X-ray spectrum Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910000601 superalloy Inorganic materials 0.000 description 2
- YPFNIPKMNMDDDB-UHFFFAOYSA-K 2-[2-[bis(carboxylatomethyl)amino]ethyl-(2-hydroxyethyl)amino]acetate;iron(3+) Chemical compound [Fe+3].OCCN(CC([O-])=O)CCN(CC([O-])=O)CC([O-])=O YPFNIPKMNMDDDB-UHFFFAOYSA-K 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 230000003064 anti-oxidating effect Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
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- 229910052710 silicon Inorganic materials 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/10—Metallic powder containing lubricating or binding agents; Metallic powder containing organic material
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
技术领域technical field
本发明涉及粉末冶金材料技术领域,尤其涉及一种含Al和Ti的Fe-Cu-C基合金材料及其制备方法。The invention relates to the technical field of powder metallurgy materials, in particular to an Fe-Cu-C-based alloy material containing Al and Ti and a preparation method thereof.
背景技术Background technique
高温结构件广泛应用于航空航天领域,随着特殊应用场景的不断发展,对高温结构件的高温强度、高温抗氧化性能等关键性能的要求也不断提高。如何通过易于加工且具有优良高温强度和高温抗氧化性能的合金材料替代传统铁基金属材料制备高温结构件,是领域内研究的重点。High-temperature structural parts are widely used in the aerospace field. With the continuous development of special application scenarios, the requirements for key properties such as high-temperature strength and high-temperature oxidation resistance of high-temperature structural parts are also increasing. How to prepare high-temperature structural parts by replacing traditional iron-based metal materials with alloy materials that are easy to process and have excellent high-temperature strength and high-temperature oxidation resistance is the focus of research in this field.
为改善传统铁基材料的抗氧化性能,许多研究者通过在合金表面添加抗氧化涂层来提高合金的抗氧化性能。然而,由于涂层的厚度有限,且涂层、基体层以及在氧化过程中出现的氧化层三者的热膨胀系数不同,在氧化环境中的涂层之间以及涂层与基体层之间均存在内应力,消耗涂层的同时氧化层会发生剥落,造成材料的二次氧化。In order to improve the oxidation resistance of traditional iron-based materials, many researchers have improved the oxidation resistance of the alloy by adding an anti-oxidation coating on the surface of the alloy. However, due to the limited thickness of the coating and the different thermal expansion coefficients of the coating, the substrate layer and the oxide layer that appears during the oxidation process, there are Internal stress, while the coating is consumed, the oxide layer will peel off, resulting in secondary oxidation of the material.
在铁基材料中,通常还会加入如Cr、Ni、Al、Si等合金元素来提高合金的抗氧化性能,各元素对铁基合金高温抗氧化的影响程度大小顺序为Al>Si>Cr>Ni。在实际开发和应用中,上述元素的应用存在以下不足:1)在高温氧化过程中,Ni需要与其他元素的相互作用才能对铁基高温合金的抗氧化性有一定的影响。2)在铁基合金中加入Cr元素,合金在氧化后会形成具有一定保护性的氧化膜,但在富Fe的氧化层中存在大量的裂纹,氧化层不致密。随着氧化时间的延长,氧化外层剥落,从而使得内层发生二次氧化;并且,在Fe基合金中加入Cr元素成本高,因此不利于材料的生产。3)将Al元素加入铁基合金中,在氧化过程中,合金会形成Al2O3的氧化膜,且随着Al含量的增加,合金的抗氧化性能提高,但是Al2O3氧化膜附着力差,Al含量越高,氧化时形成的Al2O3越多且越容易发生剥落,而且Al的加入会显著降低合金的力学性能,使得合金的使用受到限制。In iron-based materials, alloying elements such as Cr, Ni, Al, and Si are usually added to improve the oxidation resistance of the alloy. The order of the influence of each element on the high-temperature oxidation resistance of iron-based alloys is Al>Si>Cr> Ni. In actual development and application, the application of the above elements has the following disadvantages: 1) During the high temperature oxidation process, Ni needs to interact with other elements to have a certain influence on the oxidation resistance of iron-based superalloys. 2) When Cr is added to the iron-based alloy, the alloy will form a protective oxide film after oxidation, but there are a large number of cracks in the Fe-rich oxide layer, and the oxide layer is not dense. As the oxidation time prolongs, the oxidized outer layer peels off, resulting in secondary oxidation of the inner layer; moreover, the cost of adding Cr to the Fe-based alloy is high, which is not conducive to the production of materials. 3) When Al is added to the iron-based alloy, during the oxidation process, the alloy will form an Al 2 O 3 oxide film, and with the increase of Al content, the oxidation resistance of the alloy will increase, but the Al 2 O 3 oxide film will Poor strength, the higher the Al content, the more Al 2 O 3 formed during oxidation and the easier it is to peel off, and the addition of Al will significantly reduce the mechanical properties of the alloy, which limits the use of the alloy.
因此,如何克服现有技术的不足,提高铁基合金材料的高温抗氧化性能,成为亟待解决的技术问题。Therefore, how to overcome the deficiencies of the prior art and improve the high-temperature oxidation resistance of iron-based alloy materials has become a technical problem to be solved urgently.
发明内容Contents of the invention
有鉴于此,为了解决传统铁基粉末冶金材料在氧化过程中氧化膜容易开裂,从而导致合金抗氧化性差的问题,本发明提供了一种具有良好的抗氧化性能的含Al和Ti的Fe-Cu-C基合金材料及其制备方法,通过组分配比和工艺控制提高合金的自抗氧化性能。In view of this, in order to solve the problem that the oxide film of traditional iron-based powder metallurgy materials is easy to crack during the oxidation process, resulting in poor oxidation resistance of the alloy, the present invention provides a Fe- The Cu-C-based alloy material and its preparation method improve the self-oxidation resistance of the alloy through component distribution and process control.
一方面,本发明提供一种含Al和Ti的Fe-Cu-C基合金材料,包括:碳0.5-1.0wt.%,铜5.0-20.0wt.%,铝和钛共3.0-14.0wt.%,硬脂酸类润滑剂0.5-1.0wt.%,余量为铁,其中,铝至少为1.0wt.%,钛至少为2.0wt.%。In one aspect, the present invention provides a Fe-Cu-C-based alloy material containing Al and Ti, including: carbon 0.5-1.0wt.%, copper 5.0-20.0wt.%, aluminum and titanium 3.0-14.0wt.%. , stearic acid lubricant 0.5-1.0wt.%, the balance is iron, wherein, aluminum is at least 1.0wt.%, titanium is at least 2.0wt.%.
进一步地,本发明的含Al和Ti的Fe-Cu-C基合金材料,在1000℃下氧化20h后氧化增重不大于80.4mg/cm2。Furthermore, the Fe-Cu-C-based alloy material containing Al and Ti of the present invention has an oxidation weight gain of not more than 80.4 mg/cm 2 after being oxidized at 1000° C. for 20 hours.
另一方面,本发明提供一种含Al和Ti的Fe-Cu-C基合金材料的制备方法,包括:On the other hand, the present invention provides a kind of preparation method of Fe-Cu-C base alloy material containing Al and Ti, comprising:
一、配料1. Ingredients
按以下配比:碳0.5-1.0wt.%,铜5.0-20.0wt.%,铝和钛共3.0-14.0wt.%,硬脂酸类润滑剂0.5-1.0wt.%,余量为铁,进行配料,其中,铝至少为1.0wt.%,钛至少为2.0wt.%,得到原料粉体和润滑剂;According to the following proportions: carbon 0.5-1.0wt.%, copper 5.0-20.0wt.%, aluminum and titanium 3.0-14.0wt.%, stearic acid lubricant 0.5-1.0wt.%, the balance is iron, Perform batching, wherein, aluminum is at least 1.0wt.%, titanium is at least 2.0wt.%, and raw material powder and lubricant are obtained;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加0.5-1.0wt.%的硬脂酸类润滑剂,混合转速为500-600rpm,混合时间为60-180min,得到混合粉体;The raw material powder is mechanically mixed by a tank mill at room temperature, wherein 0.5-1.0wt.% of stearic acid lubricant is added during mixing, the mixing speed is 500-600rpm, and the mixing time is 60-180min to obtain a mixed Powder;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为400-700MPa,保压时间为30-60s,得到压制生坯;Press the mixed powder with a powder hydraulic press at room temperature, the form of pressing is dry pressing, the pressing pressure is 400-700MPa, and the holding time is 30-60s to obtain a pressed green body;
四、烧结处理4. Sintering treatment
在非氧化性保护气氛中对压制生坯进行烧结,烧结温度为1050-1250℃,烧结时间为60-180min,升温速率为5℃/min,得到含Al和Ti的Fe-Cu-C基合金材料。The pressed green body is sintered in a non-oxidizing protective atmosphere, the sintering temperature is 1050-1250°C, the sintering time is 60-180min, and the heating rate is 5°C/min to obtain a Fe-Cu-C-based alloy containing Al and Ti Material.
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的步骤一中,铁、铜和碳为单质粉末,其中,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm。Further, in step 1 of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention, iron, copper and carbon are elemental powders, wherein the particle size of the iron elemental powder is 30-150 μm, and the particle size of the copper elemental powder is 10-50μm, the particle size of carbon elemental powder is 2-10μm.
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的步骤一中,铝为单质粉末、铝钛合金粉末或铁铝合金粉末中的一种,其中,铝单质粉末粒度为1-5μm,铝钛合金粉末粒度为10-50μm,铁铝合金粉末粒度为50-75μm。Further, in step 1 of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention, aluminum is one of elemental powder, aluminum-titanium alloy powder or iron-aluminum alloy powder, wherein the particle size of the aluminum elemental powder is 1-5μm, the particle size of aluminum-titanium alloy powder is 10-50μm, and the particle size of iron-aluminum alloy powder is 50-75μm.
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的步骤一中,钛为单质粉末、铝钛合金粉末或铁钛合金粉末中的一种,其中,钛单质粉末粒度为1-5μm,铝钛合金粉末粒度为10-50μm,铁钛合金粉末粒度为50-75μm。Further, in step 1 of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention, titanium is one of elemental powder, aluminum-titanium alloy powder or iron-titanium alloy powder, wherein the particle size of the titanium elemental powder is 1-5μm, the particle size of aluminum-titanium alloy powder is 10-50μm, and the particle size of iron-titanium alloy powder is 50-75μm.
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的步骤一中,铝钛合金中Al与Ti的摩尔比为1:3,铁铝合金中Fe与Al的摩尔比为3:1,铁钛合金中Fe与Ti的摩尔比为2:1。Further, in step 1 of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention, the molar ratio of Al to Ti in the aluminum-titanium alloy is 1:3, and the molar ratio of Fe to Al in the iron-aluminum alloy The molar ratio of Fe and Ti in the iron-titanium alloy is 2:1.
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的步骤一中,硬脂酸类润滑剂为硬脂酸或硬脂酸锌中的一种。Further, in step 1 of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention, the stearic acid lubricant is one of stearic acid or zinc stearate.
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的步骤四中,非氧化性保护气氛为纯氢气氛或氮-氢混合气氛。Furthermore, in
进一步地,本发明含Al和Ti的Fe-Cu-C基合金材料制备方法的氮-氢混合气氛中,氮气与氢气的体积比为10:90。Further, in the nitrogen-hydrogen mixed atmosphere of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention, the volume ratio of nitrogen to hydrogen is 10:90.
本发明含Al和Ti的Fe-Cu-C基合金材料及其制备方法,具有以下有益效果:The Fe-Cu-C-based alloy material containing Al and Ti and the preparation method thereof of the present invention have the following beneficial effects:
1.通过添加铝和钛元素,改善合金在氧化过程中样品表面出现优先优化的现象,使得合金材料在氧化过程中形成相对致密的氧化表面,从而提高合金的抗氧化性。1. By adding aluminum and titanium elements, the phenomenon of preferential optimization of the sample surface during the oxidation process of the alloy is improved, so that the alloy material forms a relatively dense oxidized surface during the oxidation process, thereby improving the oxidation resistance of the alloy.
2.通过添加铝和钛元素,改善铁基合金材料氧化过程中氧化层与基体层之间热膨胀系数差异较大的问题,提高氧化层与基体层之间的附着力,避免氧化层的开裂,从而提高合金的抗氧化性。2. By adding aluminum and titanium elements, the problem of large difference in thermal expansion coefficient between the oxide layer and the base layer during the oxidation process of iron-based alloy materials is improved, the adhesion between the oxide layer and the base layer is improved, and cracking of the oxide layer is avoided. Thereby improving the oxidation resistance of the alloy.
3.本发明的制备方法操作简单、能耗小、成本低、生产效率高,适于工业推广应用。3. The preparation method of the present invention has the advantages of simple operation, low energy consumption, low cost and high production efficiency, and is suitable for industrial popularization and application.
附图说明Description of drawings
为了更清楚地说明本发明实施例的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其它的附图。In order to illustrate the technical solutions of the embodiments of the present invention more clearly, the accompanying drawings used in the embodiments will be briefly introduced below. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention. Those of ordinary skill in the art can also obtain other drawings based on these drawings without any creative effort.
图1为本发明示例性实施例1-5的含Al和Ti的Fe-Cu-C基合金材料的制备方法的流程图;Fig. 1 is the flow chart of the preparation method of the Fe-Cu-C base alloy material containing Al and Ti of exemplary embodiment 1-5 of the present invention;
图2是根据本发明示例性实施例1-5以及对比例制备材料试样在1000℃下氧化20h后单位面积增重曲线图;Fig. 2 is a graph showing the weight gain per unit area after the material sample is oxidized at 1000° C. for 20 h according to exemplary embodiments 1-5 of the present invention and comparative examples;
图3为根据本发明示例性实施例2制备材料试样的氧化截面SEM图及EDS谱图;3 is an oxidation cross-sectional SEM diagram and an EDS spectrum diagram of a material sample prepared according to
图4为根据本发明示例性实施例3制备材料试样的氧化表面SEM图;Fig. 4 is the SEM image of the oxidized surface of the material sample prepared according to exemplary embodiment 3 of the present invention;
图5为根据本发明示例性实施例4制备材料试样的氧化截面SEM图及EDS谱图;5 is an oxidation cross-sectional SEM diagram and an EDS spectrum diagram of a material sample prepared according to
图6为根据本发明示例性实施例5制备材料试样的氧化截面SEM图;6 is an oxidation cross-sectional SEM diagram of a material sample prepared according to exemplary embodiment 5 of the present invention;
图7为根据本发明对比例制备材料试样的氧化表面SEM图;Fig. 7 is the SEM figure of the oxidized surface of the material sample prepared according to the comparative example of the present invention;
图8为根据本发明对比例制备材料试样的氧化截面SEM图。Fig. 8 is an oxidation cross-sectional SEM image of a material sample prepared according to a comparative example of the present invention.
具体实施方式Detailed ways
下面结合附图对本发明实施例进行详细描述。Embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.
需说明的是,在不冲突的情况下,以下实施例及实施例中的特征可以相互组合;并且,基于本公开中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本公开保护的范围。It should be noted that, in the case of no conflict, the following embodiments and the features in the embodiments can be combined with each other; and, based on the embodiments in the present disclosure, those of ordinary skill in the art obtained without creative work All other embodiments belong to the protection scope of the present disclosure.
图1为本发明含Al和Ti的Fe-Cu-C基合金材料的制备方法的流程图;本发明实施例1至实施例5为图1所示方法的优选实施例。Fig. 1 is a flow chart of the preparation method of the Fe-Cu-C-based alloy material containing Al and Ti of the present invention; Examples 1 to 5 of the present invention are preferred embodiments of the method shown in Fig. 1 .
实施例1Example 1
一、配料1. Ingredients
按以下配比:碳0.8wt.%,铜5.0wt.%,铝1.0wt.%,钛2.0wt.%,硬脂酸0.7wt.%,余量为铁,进行配料,其中,铁、铜和碳为单质粉末,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm;铝为单质粉末,铝单质粉末粒度为1-5μm;钛为单质粉末,钛单质粉末粒度为1-5μm,得到原料粉体和硬脂酸润滑剂;According to the following proportions: 0.8wt.% carbon, 5.0wt.% copper, 1.0wt.% aluminum, 2.0wt.% titanium, 0.7wt.% stearic acid, and the balance is iron. And carbon is elemental powder, the particle size of iron elemental powder is 30-150 μm, the particle size of copper elemental powder is 10-50 μm, the particle size of carbon elemental powder is 2-10 μm; aluminum is elemental powder, the particle size of aluminum elemental powder is 1-5 μm; titanium is elemental Powder, the particle size of the titanium elemental powder is 1-5 μm, and the raw material powder and stearic acid lubricant are obtained;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加0.7wt.%的硬脂酸作为润滑剂,混合转速为500rpm,混合时间为60min,得到混合粉体;Mechanically mix the raw material powders by means of a tank mill at room temperature, wherein 0.7 wt.% stearic acid is added as a lubricant during mixing, the mixing speed is 500 rpm, and the mixing time is 60 minutes to obtain mixed powders;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为500MPa,保压时间为30s,得到压制生坯,生坯密度为6.60g/cm3;At room temperature, the mixed powder is pressed by a powder hydraulic press, the pressing form is dry pressing, the pressing pressure is 500MPa, and the holding time is 30s to obtain a pressed green body with a green density of 6.60g/cm 3 ;
四、烧结处理4. Sintering treatment
在纯氢气保护气氛中对压制生坯进行烧结,烧结温度为1050℃,烧结时间为180min,升温速率为5℃/min,得到含Al和Ti的Fe-Cu-C基合金材料。The pressed green body was sintered in a protective atmosphere of pure hydrogen, the sintering temperature was 1050°C, the sintering time was 180min, and the heating rate was 5°C/min to obtain the Fe-Cu-C-based alloy material containing Al and Ti.
实施例2Example 2
一、配料1. Ingredients
按以下配比:碳0.8wt.%,铜10.0wt.%,铝为2.0wt.%,钛为2.0wt.%,硬脂酸0.5wt.%,余量为铁,进行配料,其中,铁、铜和碳为单质粉末,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm;铝为单质粉末,铝单质粉末粒度为1-5μm;钛为单质粉末,钛单质粉末粒度为1-5μm,得到原料粉体和硬脂酸润滑剂;According to the following proportions: 0.8wt.% carbon, 10.0wt.% copper, 2.0wt.% aluminum, 2.0wt.% titanium, 0.5wt.% stearic acid, the balance is iron, and the ingredients are carried out, wherein iron , Copper and carbon are elemental powders, the particle size of iron elemental powder is 30-150 μm, the particle size of copper elemental powder is 10-50 μm, the particle size of carbon elemental powder is 2-10 μm; aluminum is elemental powder, the particle size of aluminum elemental powder is 1-5 μm; titanium It is elemental powder, the particle size of titanium elemental powder is 1-5 μm, and raw material powder and stearic acid lubricant are obtained;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加0.5wt.%的硬脂酸作为润滑剂,混合转速为550rpm,混合时间为120min,得到混合粉体;Mechanically mix the raw material powders with a tank mill at room temperature, wherein 0.5wt.% stearic acid is added as a lubricant during mixing, the mixing speed is 550rpm, and the mixing time is 120min to obtain mixed powders;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为550MPa,保压时间为45s,得到压制生坯,生坯密度为6.61g/cm3;At room temperature, the mixed powder is pressed by a powder hydraulic press, the pressing form is dry pressing, the pressing pressure is 550MPa, and the holding time is 45s to obtain a pressed green body with a green density of 6.61g/cm 3 ;
四、烧结处理4. Sintering treatment
在氮气与氢气的体积比为10:90的氮-氢混合气氛中对压制生坯进行烧结,烧结温度为1140℃,烧结时间为90min,升温速率为5℃/min,得到含Al和Ti的Fe-Cu-C基合金材料。The pressed green body was sintered in a nitrogen-hydrogen mixed atmosphere with a volume ratio of nitrogen to hydrogen of 10:90, the sintering temperature was 1140 °C, the sintering time was 90 min, and the heating rate was 5 °C/min to obtain Al and Ti. Fe-Cu-C based alloy material.
实施例3Example 3
一、配料1. Ingredients
按以下配比:碳0.5wt.%,铜15.0wt.%,铝为4.0wt.%,钛为10.0wt.%,硬脂酸钠0.8wt.%,余量为铁,进行配料,其中,铁、铜和碳为单质粉末,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm;铝为单质粉末,铝单质粉末粒度为1-5μm;钛以铁钛合金粉末的形式配比,铁钛合金粉末粒度为50-75μm,铁钛合金中Fe与Ti的摩尔比为2:1,得到原料粉体和硬脂酸钠润滑剂;According to the following proportioning: 0.5wt.% of carbon, 15.0wt.% of copper, 4.0wt.% of aluminum, 10.0wt.% of titanium, 0.8wt.% of sodium stearate, and the balance is iron for batching, wherein, Iron, copper and carbon are elemental powders, the particle size of iron elemental powder is 30-150 μm, the particle size of copper elemental powder is 10-50 μm, the particle size of carbon elemental powder is 2-10 μm; aluminum is elemental powder, the particle size of aluminum elemental powder is 1-5 μm; The titanium is proportioned in the form of iron-titanium alloy powder, the particle size of the iron-titanium alloy powder is 50-75 μm, the molar ratio of Fe and Ti in the iron-titanium alloy is 2:1, and raw material powder and sodium stearate lubricant are obtained;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加0.8wt.%的硬脂酸钠作为润滑剂,混合转速为600rpm,混合时间为120min,得到混合粉体;Mechanically mix the raw material powders at room temperature through a tank mill, wherein 0.8wt.% sodium stearate is added as a lubricant during mixing, the mixing speed is 600rpm, and the mixing time is 120min to obtain mixed powders;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为700MPa,保压时间为40s,得到压制生坯,生坯密度为7.43g/cm3;At room temperature, the mixed powder is pressed by a powder hydraulic press, the pressing form is dry pressing, the pressing pressure is 700MPa, and the holding time is 40s to obtain a pressed green body with a green density of 7.43g/cm 3 ;
四、烧结处理4. Sintering treatment
在纯氢气保护气氛中对压制生坯进行烧结,烧结温度为1100℃,烧结时间为60min,升温速率为5℃/min,得到含Al和Ti的Fe-Cu-C基合金材料。The pressed green body was sintered in a protective atmosphere of pure hydrogen, the sintering temperature was 1100°C, the sintering time was 60min, and the heating rate was 5°C/min to obtain the Fe-Cu-C-based alloy material containing Al and Ti.
实施例4Example 4
一、配料1. Ingredients
按以下配比:碳0.8wt.%,铜20.0wt.%,铝为8.0wt.%,钛为2.0wt.%,硬脂酸0.9wt.%,余量为铁,进行配料,其中,铁、铜和碳为单质粉末,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm。铝以铁铝合金粉末的形式配比,铁铝合金粉末粒度为50-75μm,铁铝合金中Fe与Al的摩尔比为3:1;钛为单质粉末,钛单质粉末粒度为1-5μm,得到原料粉体和润滑剂;According to the following proportions: 0.8wt.% carbon, 20.0wt.% copper, 8.0wt.% aluminum, 2.0wt.% titanium, 0.9wt.% stearic acid, and the balance is iron. , copper and carbon are elemental powders, the particle size of iron elemental powder is 30-150 μm, the particle size of copper elemental powder is 10-50 μm, and the particle size of carbon elemental powder is 2-10 μm. The proportion of aluminum is in the form of iron-aluminum alloy powder, the particle size of iron-aluminum alloy powder is 50-75μm, and the molar ratio of Fe and Al in iron-aluminum alloy is 3:1; titanium is elemental powder, and the particle size of titanium elemental powder is 1-5μm. Obtain raw material powder and lubricant;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加0.9wt.%的硬脂酸作为润滑剂,混合时添加0.9wt.%的硬脂酸类润滑剂,混合转速为600rpm,混合时间为120min,得到混合粉体;At room temperature, the raw material powder is mechanically mixed by a pot mill, wherein 0.9wt.% of stearic acid is added as a lubricant during mixing, and 0.9wt.% of stearic acid lubricant is added during mixing, and the mixing speed is 600rpm, the mixing time is 120min, and the mixed powder is obtained;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为600MPa,保压时间为50s,得到压制生坯,生坯密度为7.31g/cm3;At room temperature, the mixed powder is pressed by a powder hydraulic press, the form of pressing is dry pressing, the pressing pressure is 600MPa, and the holding time is 50s to obtain a pressed green body with a green density of 7.31g/cm 3 ;
四、烧结处理4. Sintering treatment
在纯氢气保护气氛中对压制生坯进行烧结,烧结温度为1100℃,烧结时间为120min,升温速率为5℃/min,得到含Al和Ti的Fe-Cu-C基合金材料。The pressed green body was sintered in a protective atmosphere of pure hydrogen, the sintering temperature was 1100°C, the sintering time was 120min, and the heating rate was 5°C/min to obtain the Fe-Cu-C-based alloy material containing Al and Ti.
实施例5Example 5
一、配料1. Ingredients
按以下配比:碳1.0wt.%,铜15wt.%,铝为1.0wt.%,钛为5.0wt.%,硬脂酸锌1.0wt.%,余量为铁,进行配料,其中,铁、铜和碳为单质粉末,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm;铝和钛均以铝钛合金粉末的形式配比,铝钛合金粉末粒度为10-50μm,铝钛合金中Al与Ti的摩尔比为1:3,得到原料粉体和硬脂酸锌润滑剂;According to the following proportioning: 1.0wt.% carbon, 15wt.% copper, 1.0wt.% aluminum, 5.0wt.% titanium, 1.0wt.% zinc stearate, and the balance is iron. , copper and carbon are elemental powders, the particle size of iron elemental powder is 30-150 μm, the particle size of copper elemental powder is 10-50 μm, and the particle size of carbon elemental powder is 2-10 μm; aluminum and titanium are all in the form of aluminum-titanium alloy powder, aluminum The particle size of the titanium alloy powder is 10-50 μm, the molar ratio of Al to Ti in the aluminum-titanium alloy is 1:3, and the raw material powder and the zinc stearate lubricant are obtained;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加1.0wt.%的硬脂酸锌作为润滑剂,混合转速为550rpm,混合时间为180min,得到混合粉体;The raw material powder was mechanically mixed by a tank mill at room temperature, wherein 1.0 wt.% zinc stearate was added as a lubricant during mixing, the mixing speed was 550 rpm, and the mixing time was 180 min to obtain a mixed powder;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为400MPa,保压时间为60s,得到压制生坯,生坯密度为7.11g/cm3;At room temperature, the mixed powder is pressed by a powder hydraulic press, the pressing form is dry pressing, the pressing pressure is 400MPa, and the holding time is 60s to obtain a pressed green body with a green density of 7.11g/cm 3 ;
四、烧结处理4. Sintering treatment
在氮气与氢气的体积比为10:90的氮-氢混合气氛中对压制生坯进行烧结,烧结温度为1250℃,烧结时间为60min,升温速率为5℃/min,得到含Al和Ti的Fe-Cu-C基合金材料。The pressed green body was sintered in a nitrogen-hydrogen mixed atmosphere with a volume ratio of nitrogen to hydrogen of 10:90, the sintering temperature was 1250 °C, the sintering time was 60 min, and the heating rate was 5 °C/min to obtain Al and Ti. Fe-Cu-C based alloy material.
实施例6(对比例)Embodiment 6 (comparative example)
一、配料1. Ingredients
按以下配比:碳0.8wt.%,铜10wt.%,硬脂酸0.7wt.%,余量为铁,进行配料,其中,铁、铜和碳为单质粉末,铁单质粉末粒度为30-150μm,铜单质粉末粒度为10-50μm,碳单质粉末粒度为2-10μm,得到原料粉体和硬脂酸润滑剂;According to the following proportioning: carbon 0.8wt.%, copper 10wt.%, stearic acid 0.7wt.%, the balance is iron, carry out batching, wherein, iron, copper and carbon are elemental powder, iron elemental powder particle size is 30- 150 μm, the particle size of copper elemental powder is 10-50 μm, and the particle size of carbon elemental powder is 2-10 μm, to obtain raw material powder and stearic acid lubricant;
二、粉末混合2. Powder mixing
在室温下通过罐磨机对原料粉体进行机械混合,其中,混合时添加0.7wt.%的硬脂酸作为润滑剂,混合转速为550rpm,混合时间为120min,得到混合粉体;Mechanically mix the raw material powders with a pot mill at room temperature, wherein 0.7wt.% stearic acid is added as a lubricant during mixing, the mixing speed is 550rpm, and the mixing time is 120min to obtain mixed powders;
三、压制处理3. Compression treatment
在室温下通过粉末液压机对混合粉体进行压制,压制形式为干压成形,压制压力为500MPa,保压时间为45s,得到压制生坯,生坯密度为6.65g/cm3;At room temperature, the mixed powder is pressed by a powder hydraulic press, the pressing form is dry pressing, the pressing pressure is 500MPa, and the holding time is 45s to obtain a pressed green body with a green density of 6.65g/cm 3 ;
四、烧结处理4. Sintering treatment
在纯氢气保护气氛中对压制生坯进行烧结,烧结温度为1100℃,烧结时间为120min,升温速率为5℃/min,得到Fe基材料。The pressed green body was sintered in a pure hydrogen protective atmosphere at a sintering temperature of 1100°C, a sintering time of 120min, and a heating rate of 5°C/min to obtain Fe-based materials.
实施例7Example 7
采用阿基米德排水法对实施例1-5制备的压制生坯以及实施例6制备的压制生坯进行密度测试,测试结果参见表1,其中,在测试过程中所用天平为电子天平,精度为0.0001。试样编号分别为FCC1、FCC2、FCC3、FCC4、FCC5以及FCC0。Adopt the Archimedes drainage method to carry out the density test to the pressed green body prepared by embodiment 1-5 and the pressed green body prepared by
表1Table 1
对实施例1-5制备的含Al和Ti的Fe-Cu-C基合金材料以及实施例6制备的Fe基材料分别进行打磨抛光后,采用线切割将上述材料切割成规格为4mm×4mm×8mm的氧化试样,然后再将氧化试样采用200#、400#、600#、800#、1200#SiC砂纸依次打磨后进行抛光,最后将抛光后的样品进行超声清洗并干燥处理备用,试样编号分别为FCC1、FCC2、FCC3、FCC4、FCC5以及FCC0。After grinding and polishing the Fe-Cu-C-based alloy material containing Al and Ti prepared in Examples 1-5 and the Fe-based material prepared in Example 6, the above-mentioned materials were cut into specifications of 4mm×4mm× 8mm oxidized sample, and then the oxidized sample was polished with 200#, 400#, 600#, 800#, 1200# SiC sandpaper in sequence, and then polished, and finally the polished sample was ultrasonically cleaned and dried for later use. The sample numbers are FCC1, FCC2, FCC3, FCC4, FCC5 and FCC0.
根据中华人民共和国航空工业标准HB 5258-2000《钢及高温合金的抗氧化性测定方法》对根据实施例1-6制备的试样进行抗氧化性测试,其中,氧化实验采用的是循环氧化,具体步骤为:对试样进行尺寸测量和称重,并记录,再将样品放入小坩埚中进行称重备用;将马弗炉升温至目标温度,然后将放有样品的小坩埚放入炉中,待马弗炉温度恢复至目标温度后开始计时,在前10h内均每1.0h取样一次,待坩埚冷却至室温后进行称重并记录,在10.0-20.0h时间内每10h取样一次。将得到的样品氧化增重进行计算,得到各合金样品的单位面积增重。合金氧化20.0h后的单位面积增重数据如表2和图2所示。According to the Aviation Industry Standard HB 5258-2000 of the People's Republic of China "Methods for Determination of Oxidation Resistance of Steel and Superalloys", the samples prepared according to Examples 1-6 were tested for oxidation resistance, wherein the oxidation test adopted cyclic oxidation, The specific steps are: measure and weigh the size of the sample, and record it, then put the sample into a small crucible for weighing; raise the temperature of the muffle furnace to the target temperature, and then put the small crucible with the sample into the furnace In the process, start timing after the temperature of the muffle furnace returns to the target temperature, and take samples every 1.0h in the first 10h, weigh and record the crucible after it cools down to room temperature, and take samples every 10h within 10.0-20.0h. The oxidation weight gain of the obtained samples was calculated to obtain the weight gain per unit area of each alloy sample. The weight gain data per unit area of the alloy after oxidizing for 20.0h is shown in Table 2 and Figure 2.
表2Table 2
如表2和图2所示,各实施例制备的试样在1000℃下氧化20h后的氧化增重不同。在氧化过程中,添加Al和Ti元素后合金的单位面积增重均低于未添加合金,说明其抗氧化性由于在铁基合金中添加了合金元素Al和Ti。结合氧化表面和氧化截面可知,单位面积增重结果与氧化表面和氧化截面图相匹配。As shown in Table 2 and Figure 2, the oxidation weight gain of the samples prepared in each embodiment is different after being oxidized at 1000°C for 20 hours. In the oxidation process, the weight gain per unit area of the alloy after adding Al and Ti elements is lower than that of the alloy without addition, indicating that its oxidation resistance is due to the addition of alloying elements Al and Ti to the iron-based alloy. Combining the oxidized surface and oxidized cross-section, it can be known that the weight gain per unit area results match the oxidized surface and oxidized cross-section diagram.
采用日立SU8020冷场发射扫描电子显微镜对实施例2-6制备的经过1000℃下循环氧化20h后的试样(试样编号分别为FCC2、FCC3、FCC4、FCC5、FCC0)的氧化截面进行表征,实施例2制备试样的氧化截面SEM图和EDS能谱图参见图3;实施例3制备试样的氧化表面SEM图参见图4;实施例4制备试样的氧化截面SEM图和EDS能谱图参见图5;实施例5制备试样的氧化表面SEM图参见图6;实施例6制备试样的氧化表面和截面SEM图分别参见图7和图8。Adopt Hitachi SU8020 cold field emission scanning electron microscope to characterize the oxidation cross-section of the sample (sample numbers are respectively FCC2, FCC3, FCC4, FCC5, FCC0) after cyclic oxidation 20h under 1000 DEG C prepared in embodiment 2-6, carry out Refer to Figure 3 for the oxidation cross-section SEM diagram and EDS energy spectrum of the sample prepared in Example 2; refer to Figure 4 for the oxidation surface SEM diagram of the sample prepared in Example 3; see Figure 4 for the oxidation cross-section SEM diagram and EDS energy spectrum of the sample prepared in Example 4 See Figure 5; see Figure 6 for the SEM image of the oxidized surface of the sample prepared in Example 5; see Figure 7 and Figure 8 for the SEM image of the oxidized surface and cross-section of the sample prepared in Example 6.
如图3所示,实施例2制备的材料的氧化层与基体层结合良好,未发现明显的开裂。从能谱结果可以看出,氧元素含量从外到内逐渐减少。As shown in Figure 3, the oxide layer of the material prepared in Example 2 is well bonded to the base layer, and no obvious cracks are found. From the results of energy spectrum, it can be seen that the oxygen content gradually decreases from the outside to the inside.
如图4所示,实施例3制备的材料的氧化表面在氧化过程中形成相对致密的氧化层,同时,没有明显的凸起和优先氧化区域产生。As shown in FIG. 4 , the oxidized surface of the material prepared in Example 3 forms a relatively dense oxide layer during the oxidation process, and at the same time, no obvious protrusions and preferential oxidation regions are generated.
如图5所示,实施例4制备的材料的氧化层与基体层结合良好,未发现明显的开裂。从能谱结果可以看出,各元素的质量百分比为Fe:Cu:Al:Ti=42.6:20.3:7.8:1.6,基本满足合金原料的配比。As shown in FIG. 5 , the oxide layer of the material prepared in Example 4 is well bonded to the base layer, and no obvious cracks are found. It can be seen from the results of the energy spectrum that the mass percentage of each element is Fe: Cu: Al: Ti = 42.6: 20.3: 7.8: 1.6, which basically meets the ratio of the alloy raw materials.
如图6所示,实施例5制备的材料氧化后出现明显的氧化层,且氧化层与基体层之间结合良好,并未发现明显的开裂,基体层相对致密。As shown in Figure 6, the material prepared in Example 5 had an obvious oxide layer after oxidation, and the oxide layer was well bonded to the base layer, no obvious cracks were found, and the base layer was relatively dense.
如图7、图8所示,实施例6制备的材料氧化后合金表面出现较多孤岛状区域,说明合金在氧化过程中存在优先氧化;同时,氧化后的氧化截面中,氧化外层出现裂纹,氧化外层与基体层之间结合处也存在裂纹和剥落坑。与实施例2-5制备材料的试样相比,实施例6制备的未添加Al和Ti的材料试样,氧化更明显,其抗氧化性明显低于添加合金元素后的合金。As shown in Figure 7 and Figure 8, after oxidation of the material prepared in Example 6, there are many isolated island-like areas on the surface of the alloy, indicating that the alloy has preferential oxidation during the oxidation process; at the same time, in the oxidized cross-section after oxidation, cracks appear in the outer layer of oxidation , There are also cracks and spalling pits at the junction between the oxide outer layer and the base layer. Compared with the material samples prepared in Examples 2-5, the material samples prepared in Example 6 without adding Al and Ti had more obvious oxidation, and their oxidation resistance was significantly lower than that of the alloys added with alloying elements.
需要说明的是,根据本发明实施例制备的具有良好的抗氧化性能的含Al和Ti的Fe-Cu-C基合金材料方法,显著改善铁基合金氧化过程中氧化层与基体层之间热膨胀系数差异较大的问题,改善形成的氧化膜易剥落的问题,提高氧化层与基体层的附着力,从而提高合金的抗氧化性。It should be noted that the Fe-Cu-C-based alloy material containing Al and Ti with good oxidation resistance prepared according to the embodiment of the present invention can significantly improve the thermal expansion between the oxide layer and the base layer during the oxidation process of the iron-based alloy. The problem of large differences in coefficients can improve the problem that the formed oxide film is easy to peel off, and improve the adhesion between the oxide layer and the base layer, thereby improving the oxidation resistance of the alloy.
以上所述,仅为本发明的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本发明的保护范围之内。因此,本发明的保护范围应以权利要求的保护范围为准。The above is only a specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Anyone skilled in the art can easily think of changes or substitutions within the technical scope disclosed in the present invention. All should be covered within the protection scope of the present invention. Therefore, the protection scope of the present invention should be based on the protection scope of the claims.
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