CN108149130A - A kind of preparation method of high-pressure unit corrosion-and high-temp-resistant shell - Google Patents

A kind of preparation method of high-pressure unit corrosion-and high-temp-resistant shell Download PDF

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CN108149130A
CN108149130A CN201711234363.1A CN201711234363A CN108149130A CN 108149130 A CN108149130 A CN 108149130A CN 201711234363 A CN201711234363 A CN 201711234363A CN 108149130 A CN108149130 A CN 108149130A
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shell
temp
pressure unit
parts
corrosion
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李鹏飞
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Tianchang Rich Burt Electronics Co Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/04Making ferrous alloys by melting
    • C22C33/06Making ferrous alloys by melting using master alloys
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/005Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/52Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/20Recycling

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Abstract

The invention discloses a kind of high-pressure unit preparation methods of corrosion-and high-temp-resistant shell, include the following steps:S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirs, then add in magnesium alloy and rare earth ferroalloy, stirring adjusts component, obtains aluminium alloy;S2, by aluminium alloy moulding by casting, obtain shell idiosome, it is thermally treated to obtain shell A;S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through plasma cladding, obtain coated shell, it is subsequently heat-treated, obtain high-pressure unit corrosion-and high-temp-resistant shell.A kind of high-pressure unit corrosion-and high-temp-resistant shell and preparation method thereof proposed by the present invention has good heat-resisting quantity, corrosion resistance and mechanical performance, and performance is stablized, and service life is long, is effectively improved high voltage package overall performance.

Description

A kind of preparation method of high-pressure unit corrosion-and high-temp-resistant shell
Technical field
The present invention relates to the preparations of technical field of metal material more particularly to a kind of high-pressure unit corrosion-and high-temp-resistant shell Method.
Background technology
High voltage package, rectification of name are line output transformers, and also referred to as row packet or row become, the high voltage package of display and the work of television set It is basically identical to make principle, main function is to generate anode high voltage, in addition provides and focuses on, accelerates, grid Deng Ge roads voltage.Due to High voltage package work in high temperature, high-frequency, high voltage, high current state, in addition the factors such as external ambient humidity or more dirt influence, High voltage package casing overall performance is influenced very big.Therefore, a kind of high temperature resistant is developed, the high voltage package casing that corrosion-resistant, performance is stablized It is current urgent problem.
Invention content
Technical problems based on background technology, the present invention propose a kind of high-pressure unit corrosion-and high-temp-resistant shell Preparation method, obtained high-pressure unit shell have good heat-resisting quantity, corrosion resistance and mechanical performance, and performance is stablized, and use Long lifespan is effectively improved high voltage package overall performance.
The present invention proposes a kind of preparation method of high-pressure unit corrosion-and high-temp-resistant shell, includes the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirred, Ran Houjia Enter magnesium alloy and rare earth ferroalloy, stir, adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, it is thermally treated to obtain shell A;
S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through wait from Sub- cladding obtains coated shell, subsequently heat-treated, obtains high-pressure unit corrosion-and high-temp-resistant shell.
Preferably, in S1, aluminium alloy includes following components by weight percent:C:0.28-0.45%, Mg:0.06- 0.12%th, Al:0.1-0.2%, Si:0.52-0.8%, Ti:0.18-0.32%, Mn:0.15-0.42%, V:0.12- 0.24%th, Cr:6.8-8.2%, Co:0.05-0.12%, Ni:0.2-0.32%, W:0.15-0.25%, Zr:0.05-0.1%, Mo:0.08-0.15%, La:0.05-0.1%, Ce:0.04-0.1%, Sm:0.04-0.1%, Nd:0.04-0.1%, remaining is Fe and inevitable impurity.
Preferably, in S2, heat treatment process is as follows:Shell idiosome is warming up to 500-540 with the speed of 2-3.5 DEG C/min DEG C, keep the temperature 1.5-2h, be then warming up to 680-720 DEG C with the speed of 1.2-2 DEG C/min, keep the temperature 1-1.5h, then with 0.5-1 DEG C/ The speed of min is warming up to 820-850 DEG C, keeps the temperature 12-20min, is then cooled to 350-400 DEG C, keeps the temperature 35-50min, then air-cooled To room temperature, 2-3h is stood.
Preferably, in S3, the raw material of cladding powder includes by weight:60-80 parts of alloy powder, nano ceramic powder 5- 8 parts.
Preferably, alloy powder includes by weight percent:C:0.22-0.4%, Cr:12-14.5%, Al:0.4- 0.6%th, Ni:0.2-0.35%, Si:0.35-0.55%, Ti:0.15-0.3%, Zr:0.05-0.12%, Ce:0.1-0.2%, Nd:0.1-0.2%, surplus are Fe and inevitable impurity.
Preferably, the raw material of nano ceramic powder by including by weight:Al2O3:40-50 parts, TiO2:5-10 parts, SiC: 10-20 parts, TiC:8-15 parts, BN:5-10 parts, MgO:5-10 parts.
Preferably, in S3, plasma cladding parameter is as follows:Protective gas is argon gas and argon flow amount is 6.5-8L/min, Power is 2-2.2KW, and sweep speed 150-180mm/min, plasma arc spot diameter is 2.5-3.5mm.
Preferably, in S3, heat treatment process is as follows:Coated shell is warming up to 250-280 DEG C, keeps the temperature 1.5-2h, then Room temperature is air-cooled to, stands 2-3d.
By adjusting component every in aluminium alloy in the present invention, the content of C, Cr, Mn, Ti, V are controlled, is inventive article It lays a good foundation with good wearability, high temperature resistant and mechanical performance, is also easy to inventive article machine-shaping;By adjusting The content of Mg, Al, Si, Ti, Mn in aluminium alloy have good deoxidation, dehydrogenation, desulfurization, nitrogen fixation effect, effectively reduce aluminium alloy Middle harmful substance contents are effectively improved institutional framework of the present invention, and each component cooperates, and the strong carbide Dispersed precipitate of generation exists In inventive article, nucleation rate is effectively improved, notable crystal grain thinning reduces carbide and formed on crystal boundary and continuous net-shaped inclined To the dislocation density being effectively improved in inventive article improves inventive article intensity, toughness, high temperature resistant and corrosion resistance;Again Rare earth element is added in aluminium alloy, further purifies aluminium alloy, inventive article internal organizational structure is effectively optimized, is eliminated Dendrite disorder form in inventive article institutional framework further improves the dislocation density of inventive article interior tissue, enhancing Inventive article overall performance;By rationally setting the heat treatment parameter of shell idiosome, shell idiosome institutional framework is effectively improved, Thinning microstructure crystal grain improves inventive article stability, further improves inventive article overall performance;Coating material is adopted With alloy powder and nano ceramic powder, and the ratio of both alloy powder, nano ceramic powder is controlled, by a small amount of ceramics Powder is filled in alloy powder, then the proportioning by optimized alloy powder, nano ceramic powder, rationally sets plasma cladding And process of thermal treatment parameter after cladding, obtained coating and shell B compatibilities are good, are tightly combined, not easily to fall off with cracking, together When coating the good mechanical property of the alloy powder wearability excellent with nano ceramic powder, corrosion resistance, inoxidizability are had The combination of machine effectively improves the performances such as corrosion-resistant, the wear-resisting and high temperature resistant of inventive article, extends inventive article service life. A kind of preparation method of high-pressure unit corrosion-and high-temp-resistant shell proposed by the present invention, obtained high-pressure unit shell have good resistance to High temperatures, corrosion resistance and mechanical performance, performance are stablized, and service life is long, are effectively improved high voltage package overall performance.
Specific embodiment
In the following, technical scheme of the present invention is described in detail by specific embodiment.
Embodiment 1
A kind of high-pressure unit preparation method of corrosion-and high-temp-resistant shell proposed by the present invention, includes the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirred, Ran Houjia Enter magnesium alloy and rare earth ferroalloy, stir, adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, it is thermally treated to obtain shell A;
S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through wait from Sub- cladding obtains coated shell, subsequently heat-treated, obtains high-pressure unit corrosion-and high-temp-resistant shell.
Embodiment 2
A kind of high-pressure unit preparation method of corrosion-and high-temp-resistant shell proposed by the present invention, includes the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirred, Ran Houjia Enter magnesium alloy and rare earth ferroalloy, stir, adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, shell idiosome be warming up to 500 with the speed of 2 DEG C/min DEG C, 2h is kept the temperature, is then warming up to 680 DEG C with the speed of 1.2 DEG C/min, keeps the temperature 1.5h, then be warming up to the speed of 0.5 DEG C/min 820 DEG C, 20min is kept the temperature, is then cooled to 400 DEG C, keeps the temperature 35min, then be air-cooled to room temperature, 3h is stood, obtains shell A;
S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through wait from Sub- cladding obtains coated shell, and coated shell then is warming up to 250 DEG C, keeps the temperature 2h, is then air-cooled to room temperature, stands 3d, obtains To high-pressure unit corrosion-and high-temp-resistant shell.
Wherein, in S1, aluminium alloy includes following components by weight percent:C:0.28%th, Mg:0.06%th, Al:0.1%th, Si:0.8%th, Ti:0.18%th, Mn:0.42%th, V:0.24%th, Cr:6.8%th, Co:0.12%th, Ni:0.2%th, W:0.25%th, Zr:0.05%th, Mo:0.15%th, La:0.05%th, Ce:0.1%th, Sm:0.04%th, Nd:0.04%, remaining is for Fe and unavoidably Impurity;
In S3, the raw material of cladding powder includes by weight:80 parts of alloy powder, 8 parts of nano ceramic powder;Alloy powder Include by weight percent:C:0.35%th, Cr:14.2%th, Al:0.55%th, Ni:0.3%th, Si:0.48%th, Ti:0.25%th, Zr:0.1%th, Ce:0.18%th, Nd:0.12%, surplus is Fe and inevitable impurity;The raw material of nano ceramic powder is by pressing Parts by weight include:Al2O3:48 parts, TiO2:6 parts, SiC:12 parts, TiC:10 parts, BN:6 parts, MgO:6 parts.
Embodiment 3
A kind of high-pressure unit preparation method of corrosion-and high-temp-resistant shell proposed by the present invention, includes the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirred, Ran Houjia Enter magnesium alloy and rare earth ferroalloy, stir, adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, shell idiosome be warming up to 525 with the speed of 2.6 DEG C/min DEG C, 1.8h is kept the temperature, is then warming up to 700 DEG C with the speed of 1.5 DEG C/min, keeps the temperature 1.2h, then heat up with the speed of 0.8 DEG C/min To 836 DEG C, 16min is kept the temperature, is then cooled to 365 DEG C, keeps the temperature 42min, then be air-cooled to room temperature, 2.5h is stood, obtains shell A;
S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through wait from Sub- cladding obtains coated shell, and coated shell then is warming up to 270 DEG C, keeps the temperature 1.8h, is then air-cooled to room temperature, stands 2.5d obtains high-pressure unit corrosion-and high-temp-resistant shell.
Wherein, in S1, aluminium alloy includes following components by weight percent:C:0.34%th, Mg:0.1%th, Al:0.15%th, Si:0.65%th, Ti:0.25%th, Mn:0.32%th, V:0.18%th, Cr:7.5%th, Co:0.09%th, Ni:0.26%th, W:0.2%th, Zr:0.08%th, Mo:0.12%th, La:0.08%th, Ce:0.08%th, Sm:0.08%th, Nd:0.06%, remaining is Fe and can not keep away The impurity exempted from;
In S3, the raw material of cladding powder includes by weight:60 parts of alloy powder, 5 parts of nano ceramic powder;Alloy powder Include by weight percent:C:0.4%th, Cr:14.5%th, Al:0.6%th, Ni:0.35%th, Si:0.35%th, Ti:0.3%th, Zr: 0.05%th, Ce:0.2%th, Nd:0.1%, surplus is Fe and inevitable impurity;The raw material of nano ceramic powder is by by weight Part includes:Al2O3:50 parts, TiO2:5 parts, SiC:20 parts, TiC:8 parts, BN:10 parts, MgO:10 parts.
Embodiment 4
A kind of high-pressure unit preparation method of corrosion-and high-temp-resistant shell proposed by the present invention, includes the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirred, Ran Houjia Enter magnesium alloy and rare earth ferroalloy, stir, adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, shell idiosome be warming up to 540 with the speed of 3.5 DEG C/min DEG C, 1.5h is kept the temperature, is then warming up to 720 DEG C with the speed of 2 DEG C/min, keeps the temperature 1h, then 850 are warming up to the speed of 1 DEG C/min DEG C, 12min is kept the temperature, is then cooled to 350 DEG C, keeps the temperature 50min, then be air-cooled to room temperature, 2h is stood, obtains shell A;
S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through wait from Sub- cladding obtains coated shell, and coated shell then is warming up to 280 DEG C, keeps the temperature 1.5h, is then air-cooled to room temperature, stands 2d, Obtain high-pressure unit corrosion-and high-temp-resistant shell.
Wherein, in S1, aluminium alloy includes following components by weight percent:C:0.45%th, Mg:0.12%th, Al:0.2%th, Si:0.52%th, Ti:0.32%th, Mn:0.15%th, V:0.12%th, Cr:8.2%th, Co:0.05%th, Ni:0.32%th, W:0.15%th, Zr:0.1%th, Mo:0.08%th, La:0.1%th, Ce:0.04%th, Sm:0.1%th, Nd:0.1%, remaining is for Fe and inevitably Impurity;
In S3, the raw material of cladding powder includes by weight:70 parts of alloy powder, 6.5 parts of nano ceramic powder;Alloyed powder End includes by weight percent:C:0.32%th, Cr:13.2%th, Al:0.5%th, Ni:0.25%th, Si:0.42%th, Ti:0.22%th, Zr:0.1%th, Ce:0.15%th, Nd:0.15%, surplus is Fe and inevitable impurity;The raw material of nano ceramic powder is by pressing Parts by weight include:Al2O3:45 parts, TiO2:8 parts, SiC:15 parts, TiC:12 parts, BN:8 parts, MgO:8 parts.
Embodiment 5
A kind of high-pressure unit preparation method of corrosion-and high-temp-resistant shell proposed by the present invention, includes the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirred, Ran Houjia Enter magnesium alloy and rare earth ferroalloy, stir, adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, shell idiosome be warming up to 530 with the speed of 2.5 DEG C/min DEG C, 1.6h is kept the temperature, is then warming up to 710 DEG C with the speed of 1.5 DEG C/min, keeps the temperature 1.2h, then heat up with the speed of 0.6 DEG C/min To 840 DEG C, 15min is kept the temperature, is then cooled to 365 DEG C, keeps the temperature 45min, then be air-cooled to room temperature, 2.2h is stood, obtains shell A;
S3, shell A is cleaned, dry, sandblasting, obtains shell B, then cladding powder is coated in shell B outer surfaces, through wait from Sub- cladding obtains coated shell, and coated shell then is warming up to 260 DEG C, keeps the temperature 1.8h, is then air-cooled to room temperature, stands 3d, Obtain high-pressure unit corrosion-and high-temp-resistant shell.
Wherein, in S1, aluminium alloy includes following components by weight percent:C:0.42%th, Mg:0.1%th, Al:0.18%th, Si:0.68%th, Ti:0.28%th, Mn:0.36%th, V:0.22%th, Cr:7.8%th, Co:0.1%th, Ni:0.3%th, W:0.22%th, Zr:0.08%th, Mo:0.12%th, La:0.08%th, Ce:0.08%th, Sm:0.08%th, Nd:0.08%, remaining is Fe and can not keep away The impurity exempted from;
In S3, the raw material of cladding powder includes by weight:75 parts of alloy powder, 5.5 parts of nano ceramic powder;Alloyed powder End includes by weight percent:C:0.22%th, Cr:12%th, Al:0.4%th, Ni:0.2%th, Si:0.55%th, Ti:0.15%th, Zr: 0.12%th, Ce:0.1%th, Nd:0.2%, surplus is Fe and inevitable impurity;The raw material of nano ceramic powder is by by weight Part includes:Al2O3:40 parts, TiO2:10 parts, SiC:10 parts, TiC:15 parts, BN:5 parts, MgO:5 parts.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto, Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.

Claims (8)

1. a kind of high-pressure unit preparation method of corrosion-and high-temp-resistant shell, which is characterized in that include the following steps:
S1, melting will be carried out in scrap iron, steel scrap, ferrochrome, manganese ingot, nickel ingot and graphite powder input smelting furnace, stirs, then add in magnesium Aluminium alloy and rare earth ferroalloy, stirring adjust component, obtain aluminium alloy;
S2, by aluminium alloy moulding by casting, obtain shell idiosome, it is thermally treated to obtain shell A;
S3, shell A is cleaned, dry, sandblasting, shell B is obtained, then cladding powder is coated in shell B outer surfaces, through plasma melting It covers, obtains coated shell, it is subsequently heat-treated, obtain high-pressure unit corrosion-and high-temp-resistant shell.
2. the preparation method of high-pressure unit corrosion-and high-temp-resistant shell according to claim 1, which is characterized in that in S1, close Golden liquid includes following components by weight percent:C:0.28-0.45%, Mg:0.06-0.12%, Al:0.1-0.2%, Si: 0.52-0.8%, Ti:0.18-0.32%, Mn:0.15-0.42%, V:0.12-0.24%, Cr:6.8-8.2%, Co:0.05- 0.12%th, Ni:0.2-0.32%, W:0.15-0.25%, Zr:0.05-0.1%, Mo:0.08-0.15%, La:0.05- 0.1%th, Ce:0.04-0.1%, Sm:0.04-0.1%, Nd:0.04-0.1%, remaining is Fe and inevitable impurity.
3. the preparation method of high-pressure unit corrosion-and high-temp-resistant shell according to claim 1, which is characterized in that in S2, heat Processing procedure is as follows:Shell idiosome is warming up to 500-540 DEG C with the speed of 2-3.5 DEG C/min, keeps the temperature 1.5-2h, then with The speed of 1.2-2 DEG C/min is warming up to 680-720 DEG C, keeps the temperature 1-1.5h, then be warming up to 820- with the speed of 0.5-1 DEG C/min 850 DEG C, 12-20min is kept the temperature, is then cooled to 350-400 DEG C, keeps the temperature 35-50min, then be air-cooled to room temperature, stands 2-3h.
4. the preparation method of high-pressure unit corrosion-and high-temp-resistant shell according to claim 1, which is characterized in that in S3, melt The raw material at whiting end includes by weight:60-80 parts of alloy powder, 5-8 parts of nano ceramic powder.
5. the preparation method of the 4 high-pressure unit corrosion-and high-temp-resistant shells is wanted according to right, which is characterized in that alloy powder is pressed Mass percent includes:C:0.22-0.4%, Cr:12-14.5%, Al:0.4-0.6%, Ni:0.2-0.35%, Si:0.35- 0.55%th, Ti:0.15-0.3%, Zr:0.05-0.12%, Ce:0.1-0.2%, Nd:0.1-0.2%, surplus are Fe and can not The impurity avoided.
6. the preparation method of high-pressure unit corrosion-and high-temp-resistant shell according to claim 4, which is characterized in that nano ceramics The raw material of powder by including by weight:Al2O3:40-50 parts, TiO2:5-10 parts, SiC:10-20 parts, TiC:8-15 parts, BN: 5-10 parts, MgO:5-10 parts.
7. the preparation method of high-pressure unit corrosion-and high-temp-resistant shell according to claim 1, which is characterized in that in S3, etc. Ion cladding parameter is as follows:Protective gas is argon gas and argon flow amount is 6.5-8L/min, power 2-2.2KW, sweep speed For 150-180mm/min, plasma arc spot diameter is 2.5-3.5mm.
8. the preparation method of high-pressure unit corrosion-and high-temp-resistant shell according to claim 1, which is characterized in that in S3, heat Processing procedure is as follows:Coated shell is warming up to 250-280 DEG C, keeps the temperature 1.5-2h, is then air-cooled to room temperature, stands 2-3d.
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Application publication date: 20180612