CN109355617A - A kind of 30Cr2Ni2WVA nitriding method - Google Patents

A kind of 30Cr2Ni2WVA nitriding method Download PDF

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Publication number
CN109355617A
CN109355617A CN201811428105.1A CN201811428105A CN109355617A CN 109355617 A CN109355617 A CN 109355617A CN 201811428105 A CN201811428105 A CN 201811428105A CN 109355617 A CN109355617 A CN 109355617A
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CN
China
Prior art keywords
nitriding
treatment
temperature
cooling
requirement
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
CN201811428105.1A
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Chinese (zh)
Inventor
桂培培
赵浩川
杨善波
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.)
AECC Guizhou Liyang Aviation Power Co Ltd
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AECC Guizhou Liyang Aviation Power 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 AECC Guizhou Liyang Aviation Power Co Ltd filed Critical AECC Guizhou Liyang Aviation Power Co Ltd
Priority to CN201811428105.1A priority Critical patent/CN109355617A/en
Publication of CN109355617A publication Critical patent/CN109355617A/en
Pending legal-status Critical Current

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    • 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
    • C23C8/08Solid 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 only one element being applied
    • C23C8/24Nitriding
    • C23C8/26Nitriding 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
    • C21D1/25Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
    • 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
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)

Abstract

The invention discloses a kind of 30Cr2Ni2WVA nitriding methods, according to the material property of 30Cr2Ni2WVA and nitriding quality requirement, meet the core rigidities requirement of part by part modifier treatment before nitriding, Finishing Parts Machining meets size requirement before nitriding, nitrided surface carries out phosphorating treatment, is then heated up in well formula nitriding furnace, keeps the temperature (nitriding), is cooling.It finally tests to nitriding quality, reaches part nitrided case depth, nitriding surface hardness is met the requirements.

Description

A kind of 30Cr2Ni2WVA nitriding method
Technical field
The invention belongs to technical field of heat treatment, are related to the nitriding method of 30Cr2Ni2WVA material.
Background technique
30Cr2Ni2WVA belongs to aviation steel forgings material, is a kind of high-quality structural steel.In " the aeronautic structure grade of steel of HB/Z 79 Stainless steel nitriding specification " in do not provide the nitriding of 30Cr2Ni2WVA material with reference to technological parameter.There is this on certain type machine Material parts need to carry out surface carburization processing, and require nitrided case depth 0.5mm~0.7mm, nitriding surface hardness HR15N >=87, Core rigidities HRC=35.5~41.5.
Summary of the invention
The present invention is intended to provide a kind of 30Cr2Ni2WVA nitriding method, meets nitrided case depth 0.5mm~0.7mm, nitriding Surface hardness HR15N >=87, the nitriding quality requirement of core rigidities HRC=35.5~41.5.
According to the material property of 30Cr2Ni2WVA and nitriding quality requirement, reasonable arrangement of the present invention handles route, passes through Part modifier treatment meets the core rigidities requirement of part before nitriding, and Finishing Parts Machining meets size requirement before nitriding, nitriding table Face carries out phosphorating treatment, is then heated up in well formula nitriding furnace, keeps the temperature (nitriding), is cooling.Finally nitriding quality is carried out It examines, reaches part nitrided case depth, nitriding surface hardness is met the requirements.
The present invention is achieved by following technical solution:
A kind of 30Cr2Ni2WVA nitriding method, modifier treatment and Nitrizing Treatment including part material;
Hardening heat in the modifier treatment is 900 ± 10 DEG C, and tempering temperature is 610 ± 20 DEG C;
The Nitrizing Treatment includes heating, heat preservation and cooling;
The heating is heated up under ammonia flow, and temperature is finally promoted to 540 ± 10 DEG C by 3~5h of heating-up time;
The heat preservation is to keep the temperature 40~50h under conditions of guaranteeing ammonia dissociation rate control 35%~50%;
The cooling is air-cooled after being cooled to≤150 DEG C under ammonia flow.
Part woollen is machined to predetermined size after the modifier treatment.
The part woollen is machined to predetermined size, nitrided surface phosphorating treatment, the non-tin plating protection in nitriding face.
The present invention provides a kind of 30Cr2Ni2WVA nitriding methods, without the existing parameter that can refer in navigation mark, propose The nitriding method that can be used for 30Cr2Ni2WVA material nitriding, meets the needs of certain type machine production task, and provides The reference method of 30Cr2Ni2WVA material nitriding, and this method is safe and reliable, reproducible, energy conservation and environmental protection, pollution-free, efficiency It is high.
Detailed description of the invention
Fig. 1 is 30Cr2Ni2WVA material nitridation process route map.
Specific embodiment
Technical solution of the present invention is described further below in conjunction with attached drawing, but required protection scope does not limit to In described;
By taking the part of 30Cr2Ni2WVA material processing as an example, in order to obtain (0.5~0.7) mm depth, surface hardness HR15N >=87, and core rigidities HRC=35.5~41.5, as shown in Figure 1, this method includes successively carrying out using following methods Woollen blanking, modifier treatment, machining, phosphorating treatment, nitriding and inspection, detailed process be as follows:
1, woollen modifier treatment: quenching: (900 ± 10) DEG C, tempering: (610 ± 20) DEG C, hardening media presses HB/Z when quenched 136 require to be oily, and tempering time is calculated by 136 prescriptive procedure of HB/Z when quenched, and tempering time is true according to part effective thickness It is fixed.
2, guarantee part size by machine overstriking processing, finishing.
3, part nitrided surface phosphorating treatment, the non-tin plating protection in nitriding face.
4, part shove charge.
5, nitriding:
(1) heat up: (3~5) h is warming up to (540 ± 10) DEG C under ammonia flow.
(2) it keeps the temperature: adjusting ammonia flow (ammonia flow requires ammonia dissociation rate during guaranteeing to meet the requirements), guarantee ammonia point The control of solution rate keeps the temperature 40h~50h 35%~50%.
(3) cooling: outlet is air-cooled after being cooled to≤150 DEG C under ammonia flow, and ammonia purity is to meet the requirement of GB 536, pure Degree >=99.99%.
6, nitrided case depth, nitriding surface hardness, core rigidities, nitriding covering weave is carried out to part to examine.

Claims (3)

1. a kind of 30Cr2Ni2WVA nitriding method, it is characterised in that: modifier treatment and Nitrizing Treatment including part material;
Hardening heat in the modifier treatment is 900 ± 10 DEG C, and tempering temperature is 610 ± 20 DEG C;
The Nitrizing Treatment includes heating, heat preservation and cooling;
The heating is heated up under ammonia flow, and temperature is finally promoted to 540 ± 10 DEG C by 3~5h of heating-up time;
The heat preservation is to keep the temperature 40~50h under conditions of guaranteeing ammonia dissociation rate control 35%~50%;
The cooling is air-cooled after being cooled to≤150 DEG C under ammonia flow.
2. a kind of 30Cr2Ni2WVA nitriding method according to claim 1, it is characterised in that: will after the modifier treatment Part woollen is machined to predetermined size.
3. a kind of 30Cr2Ni2WVA nitriding method according to claim 2, it is characterised in that: the part woollen machine adds After work to predetermined size, nitrided surface phosphorating treatment, the non-tin plating protection in nitriding face.
CN201811428105.1A 2018-11-27 2018-11-27 A kind of 30Cr2Ni2WVA nitriding method Pending CN109355617A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811428105.1A CN109355617A (en) 2018-11-27 2018-11-27 A kind of 30Cr2Ni2WVA nitriding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811428105.1A CN109355617A (en) 2018-11-27 2018-11-27 A kind of 30Cr2Ni2WVA nitriding method

Publications (1)

Publication Number Publication Date
CN109355617A true CN109355617A (en) 2019-02-19

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CN201811428105.1A Pending CN109355617A (en) 2018-11-27 2018-11-27 A kind of 30Cr2Ni2WVA nitriding method

Country Status (1)

Country Link
CN (1) CN109355617A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112442650A (en) * 2020-11-11 2021-03-05 中国航发中传机械有限公司 Method for accurately controlling surface hardness, roughness and white layer depth of nitrided gear of engine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1858287A (en) * 2006-02-17 2006-11-08 沪东重机股份有限公司 Moving part pin of diesel engine and its producing method
CN102534392A (en) * 2012-02-16 2012-07-04 无锡市万邦机械制造厂 Processing, formation and manufacturing method of piston rod using 38CrMoAlA steel as materials
JP2013007065A (en) * 2011-06-22 2013-01-10 Toyota Motor Corp Nitriding-quenching method
CN106342097B (en) * 2011-01-04 2014-02-12 哈尔滨东安发动机(集团)有限公司 32Cr3MoVE material deep layer nitriding method
CN107779810A (en) * 2017-12-24 2018-03-09 中国航发贵州红林航空动力控制科技有限公司 A kind of 4Cr14Ni14W2The technique of Mo heat resisting steel rapid ion nitridings

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1858287A (en) * 2006-02-17 2006-11-08 沪东重机股份有限公司 Moving part pin of diesel engine and its producing method
CN106342097B (en) * 2011-01-04 2014-02-12 哈尔滨东安发动机(集团)有限公司 32Cr3MoVE material deep layer nitriding method
JP2013007065A (en) * 2011-06-22 2013-01-10 Toyota Motor Corp Nitriding-quenching method
CN102534392A (en) * 2012-02-16 2012-07-04 无锡市万邦机械制造厂 Processing, formation and manufacturing method of piston rod using 38CrMoAlA steel as materials
CN107779810A (en) * 2017-12-24 2018-03-09 中国航发贵州红林航空动力控制科技有限公司 A kind of 4Cr14Ni14W2The technique of Mo heat resisting steel rapid ion nitridings

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
国营彤辉机械厂: "《检验手册 内部资料》", 31 March 1976 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112442650A (en) * 2020-11-11 2021-03-05 中国航发中传机械有限公司 Method for accurately controlling surface hardness, roughness and white layer depth of nitrided gear of engine

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Application publication date: 20190219

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