CN107164718B - A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss - Google Patents

A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss Download PDF

Info

Publication number
CN107164718B
CN107164718B CN201710336611.7A CN201710336611A CN107164718B CN 107164718 B CN107164718 B CN 107164718B CN 201710336611 A CN201710336611 A CN 201710336611A CN 107164718 B CN107164718 B CN 107164718B
Authority
CN
China
Prior art keywords
product
abrasion loss
rare earth
surface treatment
gasoline engine
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.)
Active
Application number
CN201710336611.7A
Other languages
Chinese (zh)
Other versions
CN107164718A (en
Inventor
周承志
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.)
Hefei Dingxin Mould Co Ltd
Original Assignee
Hefei Dingxin Mould Co Ltd
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 Hefei Dingxin Mould Co Ltd filed Critical Hefei Dingxin Mould Co Ltd
Priority to CN201710336611.7A priority Critical patent/CN107164718B/en
Publication of CN107164718A publication Critical patent/CN107164718A/en
Application granted granted Critical
Publication of CN107164718B publication Critical patent/CN107164718B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/28Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases more than one element being applied in one step
    • C23C8/30Carbo-nitriding
    • C23C8/32Carbo-nitriding of ferrous surfaces
    • 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
    • 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/008Heat treatment of ferrous alloys containing Si
    • 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
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • 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
    • C23C24/02Coating starting from inorganic powder by application of pressure only
    • 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

The invention proposes a kind of process of surface treatment for reducing gasoline engine crank watt abrasion loss, quenching, temper processing, nitrocarburizing and surface rare earth/aluminium oxide plating intensive treatment including double fragmentation, engine crankshaft bush finished product obtained has excellent Wear-resistant, high-temperature resistant, comprehensive mechanical performance is compared to improving 50% or more before untreated, hardness is less than 0.01mm up to 63HRC, abrasion loss.

Description

A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss
Technical field
The present invention relates to automobile parts processing technology fields, and in particular to a kind of table for reducing gasoline engine crank watt abrasion loss Surface treatment technique.
Background technique
Engine crankshaft bush is exactly crankshaft bearing liner, is mounted in the mounting bracket of crankshaft and cylinder body, and the tile for playing the role of bearing is logical Often it is called crankshaft bearing liner.General crankshaft of diesel engine watt gap: 0.12-0.207MM, gasoline engine crank main bearing shell gap, limit mill Damage amount is no more than 0.17mm.Currently, the processing method of engine crankshaft bush is generally turning molding, intensity is often difficult to ensure, is existed sometimes It produces fracture, the dangerous phenomenon such as serious wear, heat-resisting quantity difference, industrial production is endangered very big in use.Therefore, it develops A kind of technique that engine crankshaft bush is effectively treated is most important to improve its obdurability, high temperature resistant, wear-resistant etc., to the prior art and warp Ji development all has significant propulsion effect.
Summary of the invention
In view of the above problems, the invention proposes a kind of surface treatment works for reducing gasoline engine crank watt abrasion loss Skill, quenching, temper processing, nitrocarburizing and surface rare earth/aluminium oxide plating intensive treatment including double fragmentation, is made Engine crankshaft bush finished product there is excellent Wear-resistant, high-temperature resistant, comprehensive mechanical performance compared to improve before untreated 50% with On, hardness is less than 0.01mm up to 63HRC, abrasion loss.
In order to achieve the above purpose, the following technical solution is employed by the present invention:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first at 1000-1020 DEG C Under the conditions of quenching, 540-550 DEG C of high tempering, then again under the conditions of 980-1000 DEG C quenching, 300-320 average tempering, obtain Product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 630-640Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and helps infiltration steam Permeation processing is carried out to product one, 5-6h is kept, obtains product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 20-30min, and filtering is freeze-dried to obtain powder, then spread plating work using cold spraying Skill will be sprayed on two surface of product, then 380-400 DEG C of heat preservation 3h under nitrogen atmosphere, then be cooled to room with 30-50 DEG C/h Temperature is to get finished product.
Preferably, engine crankshaft bush uses alloy steel material, including following percentage composition component: C0.45- in step 1) 0.56%, Si0.9-1.2%, Mn0.5-0.6%, Ti0.7-1.1%, Mo0.8-1.3%, Cu0-0.5%, B0-0.1%, remaining Amount is Fe and inevitable impurity.
Preferably, the engine crankshaft bush further includes Cr, Ni, and percentage composition is 10.8%≤Cr+Ni≤13.6%.
Preferably, in step 2) gaseous mixture be nitriding medium and carburizer mixture, C, N atomic ratio are in the gaseous mixture 2:3。
Preferably, it is the alcohol vapour that volume fraction is 6% and the ammonia that volume fraction is 2.5% that infiltration steam is helped in step 2) The mixed vapour of base methyl formate steam.
Preferably, rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size For 5-10nm.
Preferably, rare earth and the addition mass ratio of mesoporous aluminas are 1:3 in step 3), and the two gross mass is two matter of product The 3-6% of amount.
Due to using above-mentioned technical solution, the beneficial effects of the present invention are: process of surface treatment of the present invention includes twice Quenching, temper processing, nitrocarburizing and the surface rare earth/aluminium oxide plating intensive treatment of segmentation, engine crankshaft bush end obtained Product has excellent Wear-resistant, high-temperature resistant, and for comprehensive mechanical performance compared to improving 50% or more before untreated, hardness is reachable 63HRC, abrasion loss are less than 0.01mm.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention, Technical scheme in the embodiment of the invention is clearly and completely described.Based on the embodiment of the present invention, the common skill in this field Art personnel every other embodiment obtained without creative efforts belongs to the model that the present invention protects It encloses.
Embodiment 1:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first under the conditions of 1010 DEG C Quenching, 540 DEG C of high temperings, then quenching, 300 DEG C of average temperings under the conditions of 980 DEG C again, obtains product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 630Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 5h, obtain product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 20min, and filtering is freeze-dried to obtain powder, then spread plating technique using cold spraying, will It is sprayed on two surface of product, then 400 DEG C of heat preservation 3h under nitrogen atmosphere, then room temperature is cooled to get finished product with 30 DEG C/h.
Engine crankshaft bush is using alloy steel material, including following percentage composition component in step 1): C0.45%, Si1.1%, Mn0.55%, Ti0.7%, Mo1.2%, Cu0.5%, B0.05%, surplus be Fe and inevitable impurity, further include Cr, Ni, percentage composition are (Cr+Ni) 10.8%.
Gaseous mixture is the mixture of nitriding medium and carburizer in step 2), and C, N atomic ratio are 2:3 in the gaseous mixture, is helped Seep the mixed vapour that steam is the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5%.
Rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size 5- The addition mass ratio of 10nm, rare earth and mesoporous aluminas is 1:3, and the two gross mass is the 4% of two mass of product.
Embodiment 2:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first under the conditions of 1020 DEG C Quenching, 550 DEG C of high temperings, then quenching, 310 DEG C of average temperings under the conditions of 990 DEG C again, obtains product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 640Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 6h, obtain product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 30min, and filtering is freeze-dried to obtain powder, then spread plating technique using cold spraying, will It is sprayed on two surface of product, then 390 DEG C of heat preservation 3h under nitrogen atmosphere, then room temperature is cooled to get finished product with 40 DEG C/h.
Engine crankshaft bush is using alloy steel material, including following percentage composition component in step 1): C0.5%, Si1%, Mn0.6%, Ti1%, Mo1.8%, Cu0.1%, B0.1%, surplus are Fe and inevitable impurity, further include Cr, Ni, hundred Dividing content is (Cr+Ni) 13.6%.
Gaseous mixture is the mixture of nitriding medium and carburizer in step 2), and C, N atomic ratio are 2:3 in the gaseous mixture, is helped Seep the mixed vapour that steam is the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5%.
Rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size 5- The addition mass ratio of 10nm, rare earth and mesoporous aluminas is 1:3, and the two gross mass is the 6% of two mass of product.
Embodiment 3:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first under the conditions of 1000 DEG C Quenching, 550 DEG C of high temperings, then quenching, 310 DEG C of average temperings under the conditions of 1000 DEG C again, obtains product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 640Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 6h, obtain product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 30min, and filtering is freeze-dried to obtain powder, then spread plating technique using cold spraying, will It is sprayed on two surface of product, then 380 DEG C of heat preservation 3h under nitrogen atmosphere, then room temperature is cooled to get finished product with 40 DEG C/h.
Engine crankshaft bush is using alloy steel material, including following percentage composition component in step 1): C0.56%, Si1.2%, Mn0.58%, Ti1.1%, Mo0%, Cu0.3%, B0.08%, surplus are Fe and inevitable impurity, further include Cr, Ni, Percentage composition is (Cr+Ni) 11.2%.
Gaseous mixture is the mixture of nitriding medium and carburizer in step 2), and C, N atomic ratio are 2:3 in the gaseous mixture, is helped Seep the mixed vapour that steam is the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5%.
Rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size 5- The addition mass ratio of 10nm, rare earth and mesoporous aluminas is 1:3, and the two gross mass is the 5% of two mass of product.
Embodiment 4:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first under the conditions of 1000 DEG C Quenching, 545 DEG C of high temperings, then quenching, 320 DEG C of average temperings under the conditions of 1000 DEG C again, obtains product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 630Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 6h, obtain product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 30min, and filtering is freeze-dried to obtain powder, then spread plating technique using cold spraying, will It is sprayed on two surface of product, then 390 DEG C of heat preservation 3h under nitrogen atmosphere, then room temperature is cooled to get finished product with 50 DEG C/h.
Engine crankshaft bush is using alloy steel material, including following percentage composition component in step 1): C0.48%, Si0.9%, Mn0.5%, Ti0.8%, Mo1.3%, Cu0%, B0%, surplus are Fe and inevitable impurity, further include Cr, Ni, percentage Content is (Cr+Ni) 12.4%.
Gaseous mixture is the mixture of nitriding medium and carburizer in step 2), and C, N atomic ratio are 2:3 in the gaseous mixture, is helped Seep the mixed vapour that steam is the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5%.
Rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size 5- The addition mass ratio of 10nm, rare earth and mesoporous aluminas is 1:3, and the two gross mass is the 3% of two mass of product.
Embodiment 5:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first under the conditions of 1020 DEG C Quenching, 550 DEG C of high temperings, then quenching, 300 DEG C of average temperings under the conditions of 990 DEG C again, obtains product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 630Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 5h, obtain product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 30min, and filtering is freeze-dried to obtain powder, then spread plating technique using cold spraying, will It is sprayed on two surface of product, then 400 DEG C of heat preservation 3h under nitrogen atmosphere, then room temperature is cooled to get finished product with 50 DEG C/h.
Engine crankshaft bush is using alloy steel material, including following percentage composition component in step 1): C0.53%, Si1.1%, Mn0.55%, Ti0.9%, Mo1%, Cu0%, B0.06%, surplus are Fe and inevitable impurity.
Gaseous mixture is the mixture of nitriding medium and carburizer in step 2), and C, N atomic ratio are 2:3 in the gaseous mixture, is helped Seep the mixed vapour that steam is the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5%.
Rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size 5- The addition mass ratio of 10nm, rare earth and mesoporous aluminas is 1:3, and the two gross mass is the 4% of two mass of product.
Embodiment 6:
A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss, comprising the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first under the conditions of 1010 DEG C Quenching, 540 DEG C of high temperings, then quenching, 320 DEG C of average temperings under the conditions of 980 DEG C again, obtains product one;
2) nitrocarburizing is handled: adjusting furnace pressure is 630Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 6h, obtain product two;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the poly- second of the two gross mass 10% is added Enol and 2 times of water are ultrasonically treated 20min, and filtering is freeze-dried to obtain powder, then spread plating technique using cold spraying, will It is sprayed on two surface of product, then 380 DEG C of heat preservation 3h under nitrogen atmosphere, then room temperature is cooled to get finished product with 30 DEG C/h.
Engine crankshaft bush is using alloy steel material, including following percentage composition component in step 1): C0.55%, Si1.2%, Mn0.56%, Ti1.1%, Mo1.2%, Cu0.2%, B0%, surplus are Fe and inevitable impurity.
Gaseous mixture is the mixture of nitriding medium and carburizer in step 2), and C, N atomic ratio are 2:3 in the gaseous mixture, is helped Seep the mixed vapour that steam is the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5%.
Rare earth is the composition of La, Ce, Sc in step 3), and aluminium oxide is specially mesoporous aluminas, average pore size 5- The addition mass ratio of 10nm, rare earth and mesoporous aluminas is 1:3, and the two gross mass is the 5% of two mass of product.
The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations;Although with reference to the foregoing embodiments Invention is explained in detail, those skilled in the art should understand that: it still can be to aforementioned each implementation Technical solution documented by example is modified or equivalent replacement of some of the technical features;And these modification or Replacement, the spirit and scope for technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution.

Claims (5)

1. a kind of process of surface treatment for reducing gasoline engine crank watt abrasion loss, which comprises the following steps:
1) modifier treatment: the segmentation of molding engine crankshaft bush is quenched twice, is tempered, specially first in 1000-1020 DEG C of condition Lower quenching, 540-550 DEG C of high tempering, then quenching, 300-320 average tempering under the conditions of 980-1000 DEG C again, obtains product One;
Wherein, engine crankshaft bush uses alloy steel material, including following percentage composition component: C 0.45-0.56%, Si 0.9- 1.2%, Mn 0.5-0.6%, Ti 0.7-1.1%, Mo 0.8-1.3%, Cu 0-0.5%, B 0-0.1%, surplus be Fe and Inevitable impurity;
2) nitrocarburizing is handled: adjusting furnace pressure is 630-640Pa, and gaseous mixture is passed through under the conditions of 510 DEG C and is helped and seeps steam to production Product one carry out permeation processing, keep 5-6h, obtain product two;
Wherein, gaseous mixture is the mixture of nitriding medium and carburizer, and C, N atomic ratio are 2:3 in the gaseous mixture;
3) rare earth/aluminium oxide plating processing: appropriate rare earth, aluminium oxide are blended, the polyvinyl alcohol of the two gross mass 10% is added With 2 times of water of the two gross mass, it is ultrasonically treated 20-30min, filtering is freeze-dried to obtain powder, then seeps using cold spraying diffusion Obtained material is sprayed on two surface of product by depositing process, then 380-400 DEG C of heat preservation 3h under nitrogen atmosphere, then with 30-50 DEG C/h is cooled to room temperature to get finished product.
2. the process of surface treatment according to claim 1 for reducing gasoline engine crank watt abrasion loss, it is characterised in that: described Engine crankshaft bush further includes Cr, Ni, and percentage composition is 10.8%≤Cr+Ni≤13.6%.
3. the process of surface treatment according to claim 1 for reducing gasoline engine crank watt abrasion loss, it is characterised in that: step 2) help that seep steam be the mixed of the alcohol vapour that volume fraction is 6% and the methyl carbamate steam that volume fraction is 2.5% in Close steam.
4. the process of surface treatment according to claim 1 for reducing gasoline engine crank watt abrasion loss, it is characterised in that: step 3) rare earth is the composition of La, Ce, Sc in, and aluminium oxide is specially mesoporous aluminas, average pore size 5-10nm.
5. the process of surface treatment according to claim 1 for reducing gasoline engine crank watt abrasion loss, it is characterised in that: step 3) rare earth and the addition mass ratio of mesoporous aluminas are 1:3 in, and the two gross mass is the 3-6% of two mass of product.
CN201710336611.7A 2017-05-13 2017-05-13 A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss Active CN107164718B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710336611.7A CN107164718B (en) 2017-05-13 2017-05-13 A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710336611.7A CN107164718B (en) 2017-05-13 2017-05-13 A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss

Publications (2)

Publication Number Publication Date
CN107164718A CN107164718A (en) 2017-09-15
CN107164718B true CN107164718B (en) 2018-12-04

Family

ID=59816407

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710336611.7A Active CN107164718B (en) 2017-05-13 2017-05-13 A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss

Country Status (1)

Country Link
CN (1) CN107164718B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110042339B (en) * 2019-06-05 2021-07-06 哈尔滨工程大学 Vacuum carburization method for reducing temperature and increasing speed
CN113122683B (en) * 2021-04-19 2022-09-30 江阴大手印精密材料科技发展有限公司 High-wear-resistance alloy steel for linear guide rail and preparation method thereof
CN113245794A (en) * 2021-05-30 2021-08-13 东风汽车车轮随州有限公司 Gapless elastic bearing bush of rolling die and machining method thereof
CN114000095B (en) * 2022-01-04 2022-04-29 潍坊谷合传动技术有限公司 Surface carbonitriding treatment method for planet shaft for tractor axle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1192121C (en) * 1999-02-19 2005-03-09 大众汽车有限公司 Method and device for treating a component surface
CN100516299C (en) * 2007-06-04 2009-07-22 西安交通大学 Method for preparing compound coat between metals
CN104087889A (en) * 2014-07-01 2014-10-08 江苏科技大学 Treatment method of successively aluminizing and oxidizing surface of die-casting die and oxidizing device
CN105296850A (en) * 2015-11-03 2016-02-03 合肥海源机械有限公司 Preparation method of high-temperature-resistant engine crankshaft bearing bush

Also Published As

Publication number Publication date
CN107164718A (en) 2017-09-15

Similar Documents

Publication Publication Date Title
CN107164718B (en) A kind of process of surface treatment reducing gasoline engine crank watt abrasion loss
US4243414A (en) Slidable members for prime movers
CN100590208C (en) 42CrMoE heat treatment technique
US4388114A (en) Anti-wear sintered alloy
US20120091663A1 (en) Nitriding Grade Steel Material Composition for Manufacturing Piston Rings and Cylinder Liners
CN101078071A (en) Wide temperature zone self-lubricating nickel-chromium alloy base composite material and preparation method thereof
WO2015141331A1 (en) Valve seat constituted of iron-based sintered alloy
JP6929313B2 (en) Iron-based sintered alloy for high-temperature wear resistance
CN102994907A (en) Casting method of check valve body
CN112077300B (en) High-strength wear-resistant corrosion-resistant steel powder for additive manufacturing and additive manufacturing method
CN114318168A (en) High-strength high-toughness carbonitriding steel and preparation method thereof
CN108580889A (en) A kind of manufacturing method of iron-based powder metallurgy parts
CN1058650C (en) Manufacture method of powder metallurgy valve seat
JPWO2016152967A1 (en) Sliding parts and sliding structures
CN108838388B (en) Powder metallurgy austenitic stainless steel and preparation method thereof
CN111593296A (en) Martensitic stainless steel surface hardening agent and preparation method and application method thereof
CN102808187A (en) Surface subzero treatment method for corrugated roller
KR101464197B1 (en) Sintered Alloy for Diesel engines and Valve Seat and Guide of Diesel engines Using Thereof
CN1570192A (en) Valve finisher surface modified processing method
WO2015111642A1 (en) Piston ring and production method therefor
JPS6365056A (en) Wear resistant sintered iron alloy
JPH0116297B2 (en)
KR102205475B1 (en) Thin layer tappet including WC-Ni based hard metals and manufacturing thereof
CN111996454A (en) Stainless steel for mechanical seal, mechanical seal casting made of stainless steel and preparation method of mechanical seal casting
JPS6033343A (en) Wear resistance sintered alloy

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
GR01 Patent grant
GR01 Patent grant