CN107365995A - A kind of diesel engine spiracle plating process - Google Patents

A kind of diesel engine spiracle plating process Download PDF

Info

Publication number
CN107365995A
CN107365995A CN201710641061.XA CN201710641061A CN107365995A CN 107365995 A CN107365995 A CN 107365995A CN 201710641061 A CN201710641061 A CN 201710641061A CN 107365995 A CN107365995 A CN 107365995A
Authority
CN
China
Prior art keywords
diesel engine
engine spiracle
plating process
spiracle
process according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201710641061.XA
Other languages
Chinese (zh)
Inventor
林青锋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WARD VALVE MANUFACTURING Co Ltd ANHUI PROVINCE
Original Assignee
WARD VALVE MANUFACTURING Co Ltd ANHUI PROVINCE
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by WARD VALVE MANUFACTURING Co Ltd ANHUI PROVINCE filed Critical WARD VALVE MANUFACTURING Co Ltd ANHUI PROVINCE
Priority to CN201710641061.XA priority Critical patent/CN107365995A/en
Publication of CN107365995A publication Critical patent/CN107365995A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • CCHEMISTRY; METALLURGY
    • 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
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • 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
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • 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
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • 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
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

The invention discloses a kind of diesel engine spiracle plating process, including Pre-treatment before plating and plasma cladding to be handled, and detailed process is as follows:Need coating position to be placed in activating solution diesel engine spiracle to soak, clean, dry;Mixed-powder is coated uniformly on the diesel engine spiracle surface for needing coating through Pre-treatment before plating, plasma cladding processing is carried out, cooling, obtains material A, be then heat-treated.A kind of diesel engine spiracle plating process proposed by the present invention, by optimize technique, coating material is tightly combined with matrix, is evenly distributed, and effectively increases the high temperature resistant, corrosion resistance and fatigue resistance of diesel engine spiracle, effectively extends the service life of diesel engine spiracle.

Description

A kind of diesel engine spiracle plating process
Technical field
The present invention relates to coating technology field, more particularly to a kind of diesel engine spiracle plating process.
Background technology
Valve can be divided into inlet valve and exhaust valve from engine structure, the effect of inlet valve is to draw air into start In machine, with fuel mixed combustion, the effect of exhaust valve is that the waste gas after burning is discharged and radiated.Existing diesel engine Valve is made of metal or alloy material more, needs to bear higher mechanical load and thermic load at work, while also The static load that impact load and gaseous-pressure are given of taking a seat is born, causes valve wear and seriously corroded, influences its valve Service life.Coating, which refers to be attached on a certain matrix material, plays certain special role, and has certain combine with matrix material The layer material of intensity, it can overcome certain defect of matrix material, improve its surface characteristic.At present, diesel engine spiracle Plating process need to be improved, and the valve after coating have impact on the service life of valve in high temperature resistant and corrosion-resistant.
The content of the invention
Based on technical problem existing for background technology, the present invention proposes a kind of diesel engine spiracle plating process, by excellent Chemical industry skill, coating material are tightly combined with matrix, are evenly distributed, and effectively increase high temperature resistant, the corrosion resistance of diesel engine spiracle And fatigue resistance, effectively extend the service life of diesel engine spiracle.
A kind of diesel engine spiracle plating process proposed by the present invention, including Pre-treatment before plating and plasma cladding processing.
Preferably, Pre-treatment before plating detailed process is as follows:Need coating position to be placed in activating solution diesel engine spiracle to soak Bubble, clean, dry.
Preferably, activating solution is by one or both of sulfuric acid, acetic acid, citric acid composition described above.
Preferably, plasma cladding processing detailed process is as follows:Mixed-powder is coated uniformly on through Pre-treatment before plating The diesel engine spiracle surface of coating is needed, plasma cladding processing is carried out, cooling, obtains material A, be then heat-treated.
Preferably, plasma cladding technological parameter is specific as follows:Ionized gas flow is 2-4L/min, and protective gas is argon Gas and argon flow amount are 5-8L/min, and transfer arc voltage is 36-40V, transfer current 80-100A, are sprayed away from for 1.5-3cm, work( Rate is 2-2.5KW, and sweep speed 5-8mm/s, plasma arc spot diameter is 1.2-2.2mm, and plasma melting coating thickness is 0.5-0.8mm。
Preferably, Technology for Heating Processing is as follows:Material A is warming up to 240-280 DEG C through 15-20min, is incubated 1-2h, then 320-350 DEG C is warming up to through 6-10min, 3-4h is incubated, is then air-cooled to room temperature.
Preferably, mixed-powder is by weight 100-120 by alloy powder and ceramic powders:1.5-3 is formed, and is mixed The granularity of powder is 180-220 mesh.
Preferably, alloy powder includes following components by mass fraction:Cr:20-25%, C:0.5-0.7%, B:0.2- 0.5%th, Si:0.8-1%, Mn:0.8-1.2%, Cu:0.5-0.8%, Ni:1.5-3%, W:0.2-0.5%, V:0.3- 0.8%th, Nb:0.1-0.3%, Sr:0.1-0.16%, La:0.2-0.5%, Ce:0.65-1%, Nd:0.5-0.8%, Y:0.1- 0.3%, surplus is Fe and inevitable impurity.
In specific embodiment, Cr mass fraction can also be 21%, 21.5%, 22%, 22.5%, 23%, 23.5%, 24%, C mass fraction can also be 0.54%, 0.58%, 0.6%, 0.62%, 0.65%, 0.68%, B mass fraction Can also be 0.25%, 0.3%, 0.35%, 0.4%, 0.45%, Si mass fraction can also be 0.82%, 0.85%, 0.9%th, 0.92%, 0.95%, 0.98%, Mn mass fraction can also be 0.85%, 0.9%, 0.95%, 0.1%, 0.11%, Cu mass fraction can also may be used also for 0.55%, 0.6%, 0.65%, 0.7%, 0.75%, Ni mass fraction Think 1.8%, 2%, 2.2%, 2.4%, 2.6%, 2.8%, W mass fraction can also be 0.25%, 0.3%, 0.35%, 0.4%th, 0.45%, V mass fraction can also be 0.4%, 0.5%, 0.55%, 0.6%, 0.7%, Nb mass fraction also Can be 0.14%, 0.18%, 0.2%, 0.22%, 0.25%, 0.28%, Sr mass fraction can also be 0.11%, 0.12%th, 0.13%, 0.14%, 0.15%, La mass fraction can also be 0.25%, 0.3%, 0.35%, 0.4%, 0.45%, Ce mass fraction can also be 0.7%, 0.75%, 0.8%, 0.85%, 0.9%, Nd mass fraction can be with For 0.55%, 0.6%, 0.65%, 0.7%, 0.75%, Y mass fraction can also be 0.14%, 0.16%, 0.2%, 0.22%th, 0.25%, 0.28%, surplus is Fe and inevitable impurity.
Preferably, ceramic powders are by SiC, TiC and B2O3It is by weight 2-4:1-2:1-1.5 composition.
By optimizing Pre-treatment before plating technique in the present invention, reasonable selection activating solution immersion diesel engine spiracle, effectively remove Diesel engine spiracle needs the metal oxide film at coating position, it is exposed fresh metallographic structure, forms one layer of activating surface, polishing Being advantageous to raising valve needs the roughness at coating position, effectively improves plasma cladding effect;By optimizing plasma cladding Handling process, coordinated from alloy powder with ceramic powders during plasma cladding and be used as coating material, it is logical in alloy powder Control Cr, Si, Ni, Mn, Cu content is crossed, is that valve after coating has good corrosion resistance, heat-resisting quantity, hardness, strong Degree is laid a good foundation with wearability, and V, Nb, B, Sr coordinate, and is made the dense internal organization of coating, crystallization of refinement, is avoided intergranular rotten Erosion, further improve coating overall performance, and by increasing the content of rare element La, Ce, Nd, Y in alloy powder, effectively carry Nucleation rate in high coating, effectively refine and improve the size of hardening constituent and distribution in coating, improve the globality of coating Energy;SiC, TiC and B in ceramic powders2O3Coordinate, dispersion-strengthened effect is played in coating, further improve the resistance to height of coating Temperature, corrosion resistance and anti-fatigue performance;Again by optimizing Technology for Heating Processing, further improve the institutional framework of coating, it is effectively thin Change diesel engine spiracle coating interior tissue, reduce the porosity, the bond strength of coating and valve matrix material is big, effectively improves bavin The performance such as hardness, intensity, impact resistance and the high temperature resistant of oil machine valve, corrosion-resistant.A kind of diesel engine spiracle proposed by the present invention Plating process, by optimize technique, coating material is tightly combined with matrix, is evenly distributed, and effectively increases diesel engine spiracle High temperature resistant, corrosion resistance and fatigue resistance, effectively extend the service life of diesel engine spiracle.
It is found through experiments that, the decay resistance and fatigue resistance of the diesel engine spiracle obtained using plating process of the present invention 5-7% and 4-5% are improved respectively, and its service life adds 3-4 times compared with before.
Embodiment
Below, technical scheme is described in detail by specific embodiment.
Embodiment 1
A kind of diesel engine spiracle plating process proposed by the present invention, including Pre-treatment before plating and plasma cladding processing.
Embodiment 2
A kind of diesel engine spiracle plating process proposed by the present invention, is comprised the following steps that:
S1, Pre-treatment before plating:Need coating position to be placed in activating solution diesel engine spiracle to soak, clean, dry;Its In, activating solution is sulfuric acid;
S2, plasma cladding processing:Mixed-powder is coated uniformly on to the diesel engine for needing coating through Pre-treatment before plating Valve surfaces, plasma cladding processing is carried out, cooling, obtains material A, it is subsequently heat-treated.
Wherein, plasma cladding technological parameter is specific as follows:Ionized gas flow is 3L/min, protective gas be argon gas and Argon flow amount is 6.5L/min, and transfer arc voltage is 38V, transfer current 90A, is sprayed away from for 2.2cm, power 2.2KW, scanning Speed is 6.5mm/s, and plasma arc spot diameter is 1.8mm, and plasma melting coating thickness is 0.5-0.8mm;
Mixed-powder is 110 by weight by alloy powder and ceramic powders:2.2 compositions, and the granularity of mixed-powder is 200 mesh;
Alloy powder includes following components by mass fraction:Cr:22.5%th, C:0.6%th, B:0.35%th, Si:0.9%th, Mn:1%th, Cu:0.65%th, Ni:2.2%th, W:0.35%th, V:0.5%th, Nb:0.2%th, Sr:0.12%th, La:0.35%th, Ce: 0.8%th, Nd:0.65%th, Y:0.2%, surplus is Fe and inevitable impurity;
Ceramic powders are by SiC, TiC and B2O3It is 3 by weight:1.5:1.2 composition.
Embodiment 3
A kind of diesel engine spiracle plating process proposed by the present invention, is comprised the following steps that:
S1, Pre-treatment before plating:Need coating position to be placed in activating solution diesel engine spiracle to soak, clean, dry;Its In, activating solution is 1 by volume by sulfuric acid, acetic acid:1 composition;
S2, plasma cladding processing:Mixed-powder is coated uniformly on to the diesel engine for needing coating through Pre-treatment before plating Valve surfaces, plasma cladding processing is carried out, cooling, obtains material A, material A is then warming up to 260 DEG C through 18min, insulation 1.5h, 335 DEG C then are warming up to through 8min, are incubated 3.4h, are then air-cooled to room temperature.
Wherein, plasma cladding technological parameter is specific as follows:Ionized gas flow is 2L/min, protective gas be argon gas and Argon flow amount is 5L/min, and transfer arc voltage is 36V, transfer current 80A, is sprayed away from for 1.5cm, power 2KW, sweep speed For 5mm/s, plasma arc spot diameter is 1.2mm, and plasma melting coating thickness is 0.5mm;
Mixed-powder is 100 by weight by alloy powder and ceramic powders:1.5 compositions, and the granularity of mixed-powder is 180 mesh;
Alloy powder includes following components by mass fraction:Cr:20%th, C:0.5%th, B:0.2%th, Si:0.8%th, Mn: 0.8%th, Cu:0.8%th, Ni:1.5、W:0.2%th, V:0.8%th, Nb:0.1%th, Sr:0.1%th, La:0.5%th, Ce:0.65%th, Nd:0.5%th, Y:0.3%, surplus is Fe and inevitable impurity;
Ceramic powders are by SiC, TiC and B2O3It is 2 by weight:1:1 composition.
Embodiment 4
A kind of diesel engine spiracle plating process proposed by the present invention, is comprised the following steps that:
S1, Pre-treatment before plating:Need coating position to be placed in activating solution diesel engine spiracle to soak, clean, dry;Its In, activating solution is 1 by volume by sulfuric acid, acetic acid, citric acid:1:1:Composition;
S2, plasma cladding processing:Mixed-powder is coated uniformly on to the diesel engine for needing coating through Pre-treatment before plating Valve surfaces, plasma cladding processing is carried out, cooling, obtains material A, material A is then warming up to 240 DEG C through 15min, insulation 2h, 320 DEG C then are warming up to through 6min, are incubated 4h, are then air-cooled to room temperature.
Wherein, plasma cladding technological parameter is specific as follows:Ionized gas flow is 4L/min, protective gas be argon gas and Argon flow amount is 8L/min, and transfer arc voltage is 40V, transfer current 100A, is sprayed away from for 3cm, power 2.5KW, scanning speed It is 2.2mm to spend for 8mm/s, plasma arc spot diameter, and plasma melting coating thickness is 0.8mm;
Mixed-powder is 120 by weight by alloy powder and ceramic powders:3 compositions, and the granularity of mixed-powder is 220 Mesh;
Alloy powder includes following components by mass fraction:Cr:25%th, C:0.7%th, B:0.2%th, Si:1%th, Mn: 1.2%th, Cu:0.5%th, Ni:3%th, W:0.5%th, V:0.8%th, Nb:0.3%th, Sr:0.16%th, La:0.2%th, Ce:1%th, Nd: 0.8%th, Y:0.1%, surplus is Fe and inevitable impurity;
Ceramic powders are by SiC, TiC and B2O3It is 4 by weight:2:1.5 composition.
Embodiment 5
A kind of diesel engine spiracle plating process proposed by the present invention, is comprised the following steps that:
S1, Pre-treatment before plating:Need coating position to be placed in activating solution diesel engine spiracle to soak, clean, dry;Its In, activating solution is 1 by volume by acetic acid, citric acid:1 composition;
S2, plasma cladding processing:Mixed-powder is coated uniformly on to the diesel engine for needing coating through Pre-treatment before plating Valve surfaces, plasma cladding processing is carried out, cooling, obtains material A, material A is then warming up to 250 DEG C through 16min, insulation 1.8h, 330 DEG C then are warming up to through 7min, are incubated 3.8h, are then air-cooled to room temperature.
Wherein, plasma cladding technological parameter is specific as follows:Ionized gas flow is 2.4L/min, and protective gas is argon gas And argon flow amount is 6L/min, transfer arc voltage is 38V, transfer current 85A, is sprayed away from for 2cm, power 2.2KW, scanning speed It is 1.5mm to spend for 6.5mm/s, plasma arc spot diameter, and plasma melting coating thickness is 0.6mm;
Mixed-powder is 120 by weight by alloy powder and ceramic powders:1.5 compositions, and the granularity of mixed-powder is 210 mesh;
Alloy powder includes following components by mass fraction:Cr:22.5%th, C:0.65%th, B:0.25%th, Si:0.9%th, Mn:0.85%th, Cu:0.65%th, Ni:1.8%th, W:0.25%th, V:0.4%th, Nb:0.15%th, Sr:0.12%th, La:0.25%th, Ce:0.7%th, Nd:0.65%th, Y:0.15%, surplus is Fe and inevitable impurity;
Ceramic powders are by SiC, TiC and B2O3It is 4 by weight:1:1 composition.
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 the invention discloses technical scope in, technique according to the invention scheme and its Inventive concept is subject to equivalent substitution or change, should all be included within the scope of the present invention.

Claims (9)

1. a kind of diesel engine spiracle plating process, it is characterised in that handled including Pre-treatment before plating and plasma cladding.
2. diesel engine spiracle plating process according to claim 1, it is characterised in that Pre-treatment before plating detailed process is as follows: Need coating position to be placed in activating solution diesel engine spiracle to soak, clean, dry.
3. diesel engine spiracle plating process according to claim 2, it is characterised in that activating solution is by sulfuric acid, acetic acid, citric acid One or both of composition described above.
4. diesel engine spiracle plating process according to claim 1, it is characterised in that plasma cladding processing detailed process is such as Under:Mixed-powder is coated uniformly on the diesel engine spiracle surface for needing coating through Pre-treatment before plating, carries out plasma cladding Processing, cooling, obtains material A, is then heat-treated.
5. diesel engine spiracle plating process according to claim 4, it is characterised in that plasma cladding technological parameter is specific such as Under:Ionized gas flow is 2-4L/min, and protective gas is argon gas and argon flow amount is 5-8L/min, and transfer arc voltage is 36- 40V, transfer current 80-100A, spray away from for 1.5-3cm, power 2-2.5KW, sweep speed 5-8mm/s, plasma arc Spot diameter is 1.2-2.2mm, and plasma melting coating thickness is 0.5-0.8mm.
6. diesel engine spiracle plating process according to claim 4, it is characterised in that Technology for Heating Processing is as follows:Material A is passed through 15-20min is warming up to 240-280 DEG C, is incubated 1-2h, is then warming up to 320-350 DEG C through 6-10min, is incubated 3-4h, Ran Houkong It is cooled to room temperature.
7. diesel engine spiracle plating process according to claim 4, it is characterised in that mixed-powder is by alloy powder and ceramics Powder is by weight 100-120:1.5-3 is formed, and the granularity of mixed-powder is 180-220 mesh.
8. diesel engine spiracle plating process according to claim 7, it is characterised in that alloy powder by mass fraction include with Lower component:Cr:20-25%, C:0.5-0.7%, B:0.2-0.5%, Si:0.8-1%, Mn:0.8-1.2%, Cu:0.5- 0.8%th, Ni:1.5-3%, W:0.2-0.5%, V:0.3-0.8%, Nb:0.1-0.3%, Sr:0.1-0.16%, La:0.2- 0.5%th, Ce:0.65-1%, Nd:0.5-0.8%, Y:0.1-0.3%, surplus are Fe and inevitable impurity.
9. diesel engine spiracle plating process according to claim 7, it is characterised in that ceramic powders are by SiC, TiC and B2O3Press Weight ratio is 2-4:1-2:1-1.5 composition.
CN201710641061.XA 2017-07-31 2017-07-31 A kind of diesel engine spiracle plating process Pending CN107365995A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710641061.XA CN107365995A (en) 2017-07-31 2017-07-31 A kind of diesel engine spiracle plating process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710641061.XA CN107365995A (en) 2017-07-31 2017-07-31 A kind of diesel engine spiracle plating process

Publications (1)

Publication Number Publication Date
CN107365995A true CN107365995A (en) 2017-11-21

Family

ID=60308850

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710641061.XA Pending CN107365995A (en) 2017-07-31 2017-07-31 A kind of diesel engine spiracle plating process

Country Status (1)

Country Link
CN (1) CN107365995A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101838807A (en) * 2010-04-19 2010-09-22 浙江吉利汽车研究院有限公司 Laser cladding coating material for inlet valve and exhaust valve of engine and coating thereof
CN102218857A (en) * 2011-05-27 2011-10-19 合肥金四达科技有限公司 Composite material coated with SiC-Fe based alloy layer and preparation method of composite material
CN102392241A (en) * 2011-11-10 2012-03-28 湖北汽车工业学院 Method for preparing Fe-based WC-Ni gradient coating by using plasma cladding method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101838807A (en) * 2010-04-19 2010-09-22 浙江吉利汽车研究院有限公司 Laser cladding coating material for inlet valve and exhaust valve of engine and coating thereof
CN102218857A (en) * 2011-05-27 2011-10-19 合肥金四达科技有限公司 Composite material coated with SiC-Fe based alloy layer and preparation method of composite material
CN102392241A (en) * 2011-11-10 2012-03-28 湖北汽车工业学院 Method for preparing Fe-based WC-Ni gradient coating by using plasma cladding method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
胡永俊 等: "热处理对等离子熔覆层析出物与残余应力的影响", 《热加工工艺》 *

Similar Documents

Publication Publication Date Title
CN104004972B (en) A kind of deep-sea high strength valve of Low temperature-resistancorrosion-resistant corrosion-resistant and manufacture method thereof
CN103465549A (en) Thermal barrier coating including anti-thermal corrosion transition bottom layer and preparation method thereof
CN106521400B (en) A kind of plasma transferred arc spraying method for strengthening heavy truck cylinder liner internal wall
CN106893965B (en) The bis- ceramic layer structure heat resistant coatings of YAG/8YSZ and plasma preparation method
CN104404430A (en) Iron-based non-crystalline composite coating for protecting heat exchange pipes in flue gas waste heat recovery system of power station boiler and laser re-melting and moulding technology thereof
CN1662666A (en) Heat-resistant ferritic stainless steel and method for production thereof
CN111826650B (en) Laser cladding composite powder and cladding method
CN107385433A (en) A kind of processing method for improving valve wear resistant corrosion resistant
CN107794459A (en) A kind of cylinder cover of automobile engine
WO2014069180A1 (en) Ni-Cr-Co-BASED ALLOY HAVING HIGH-TEMPERATURE CORROSION RESISTANCE PROPERTIES, AND POPPET VALVE HAVING SURFACE MODIFIED WITH SAME
CN103752818A (en) Iron-based composite powder high in chromium content for laser cladding
CN101104911A (en) Multicomponent alloy coating material for high corrosion resistance coating steel products and manufacturing method thereof
CN113564587A (en) High-temperature oxidation-resistant and press-in nodule-resistant functional layer alloy material for laser composite manufacturing furnace roller and process method
UA81021C2 (en) Iron-chromium-aluminium alloy
CN107699849A (en) A kind of high-frequency induction hot dipping alumetizing process
CN107365995A (en) A kind of diesel engine spiracle plating process
CN101492799A (en) Wear-resistant cast iron coating and production method
WO2021103426A1 (en) Powder-cored wire, preparation method therefor and use thereof, and porous coating and preparation method therefor
CN107858561A (en) A kind of handling process of engine turning rack
CN108203825B (en) Thermal fatigue resistant nickel-based composite coating for monitoring surface damage process of diesel engine cylinder cover and application thereof
CN104233281B (en) A kind of Co-based alloy powder that repairs for supercharger nozzle ring of internal-combustion engine
CN101487104A (en) Carbon steel / stainless steel composite material and preparation
CN107881438A (en) A kind of ball mill low abrasion wear-resistant ball and preparation method thereof
CN114737083A (en) GH3536 raw material powder for laser additive manufacturing, preparation method of GH3536 raw material powder and preparation method of GH3536 alloy
CN110777321B (en) Manufacturing method of wear-resistant cylinder sleeve based on surface treatment

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20171121