USPatent applicationPatented

Heat treatment method for a vehicle component

Granted 25 Oct 2022 · 2 office actions

Assignee: Kia America, Inc.

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Inventors: Dong-Hwi Kim, Hyun-Ki Kim, Soon-Woo Kwon, Min-Woo Kang +2 · Examiner: Jessee R Roe · AU 1759 · TC 1700

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Abstract

A heat treatment method of a component for a vehicle includes: heating an inner space of a heat treatment furnace in which a component for a vehicle is disposed in the inner space; stabilizing hydrogen (H 2 ) by injecting the H 2 into the inner space; and performing nitrification heat treatment for the component by injecting only ammonia (NH 3 ) into the inner space after the stabilizing. The heat treatment method may adjust the degree of vacuum and the flow rate instead of a Kn without additionally injecting the H 2 gas into an NH 3 gas, thereby implementing the nitrification heat treatment of a quality similar to that of a conventional nitrification heat treatment for a short time.

Description

8 parts
›CROSS-REFERENCE TO RELATED APPLICATION

This application claims priority to Korean Patent Application No. 10-2020-0170205 filed on Dec. 8, 2020, which is incorporated herein by reference in its entirety.

BACKGROUND OF THE DISCLOSURE
›Field of the Disclosure

The present disclosure relates to a heat treatment method for securing the durability characteristics of a component for a vehicle.

›Description of Related Art

A component for a vehicle secures the durability characteristics through heat treatment processes of various methods according to each characteristic driving environment. Particularly, nitrification heat treatment is applied to a component in which the contact occurs together with tensile/twist/bending like a gear or a shaft to secure the abrasion resistance and the fatigue characteristics at the same time in many cases. Until now, nitrification heat treatment has been designed to impart the heat treatment condition through the combination of the temperature-nitrogen potential-time in the equipment at a normal pressure (1 atmospheric pressure) or more.

Particularly, in the related art, nitrogen or hydrogen is additionally injected into an ammonia gas upon the nitrification heat treatment for adjusting the nitrogen potential. Such a mixed gas is advantageous for the nitrogen potential control but reduces the partial pressure of the ammonia gas actually participating in the reaction, thereby becoming the basic cause reducing the reaction speed.

Further, some patented processes of the related art, which are related to the low-pressure nitrification process. are confirmed to also reduce the reaction speed using the ammonia/nitrogen/hydrogen mixed gas.

The contents described in the Description of Related Art section are to help understand the background of the present disclosure and may include what is not previously known to those having ordinary skill in the art to which the present disclosure pertains.

›SUMMARY OF THE DISCLOSURE

The present disclosure is devised to solve the above problem. An object of the present disclosure is to provide a heat treatment method of a component for a vehicle. The heat treatment method may adjust the degree of vacuum and a flow rate instead of a nitrogen potential without injecting an additional gas into an ammonia gas, thereby implementing the nitrification heat treatment of the quality similar to that of the conventional nitrification heat treatment for a short time.

A heat treatment method of a component for a vehicle according to one aspect of the present disclosure includes: heating an inner space of a heat treatment furnace in which a component for a vehicle is disposed in the inner space; stabilizing the inner space by injecting hydrogen (H 2 ) into the inner space; and performing nitrification heat treatment for the component by injecting only ammonia (NH 3 ) into the inner space after the stabilizing.

Further, the performing of the nitrification heat treatment injects the NH 3 at the speed of 0.5 to 6 m 3 /h.

Further, the performing of the nitrification heat treatment is performed by maintaining the pressure of the inner space at 230 to 400 torr.

Further, the performing of the nitrification heat treatment is performed in the state where the temperature of the inner space is 400 to 600° C. by the heating.

The performing of the nitrification heat treatment is performed for 6 to 15 hours.

Meanwhile, the stabilizing injects the H 2 at the speed of 0.5 to 15 m 3 /h.

Further, the stabilizing is performed by maintaining the pressure of the inner space at 230 to 400 torr.

Further, the stabilizing is performed in the state where the temperature of the inner space is 400 to 600° C. by the heating.

Further, the stabilizing is performed within 2 hours.

The thickness of a compound layer formed on the surface of the component subjected to the nitrification heat treatment is 8 to 20 μm.

Alternatively, the thickness of a pore layer formed on the surface of the component subjected to the nitrification heat treatment is 2 to 5 μm.

Further, the surface hardness of the component subjected to the nitrification heat treatment is 620 to 710 Hv.

Alternatively, the depth of a diffusion layer of the surface of the component subjected to the nitrification heat treatment is 0.5 mm or less.

Further, the gamma prime (γ′) phase of a microstructure of the surface of the component subjected to the nitrification heat treatment is 50 to 90%.

Next, a heat treatment method of a component for a vehicle according to another aspect of the present disclosure performs nitrification heat treatment for a component by injecting only NH 3 into the inner space at the speed of 0.5 to 6 m 3 /h in a state where an inner space of a heat treatment furnace, in which a component for a vehicle is disposed in the inner space, is maintained at 400 to 600° C.

Further, the nitrification heat treatment is performed by maintaining the pressure of the inner space at 230 to 400 torr.

The performing of the nitrification heat treatment is performed for 6 to 15 hours.

The heat treatment method of a component for the vehicle according to the present disclosure may secure the compound layer, the pore layer, the surface hardness, the diffusion layer, and the γ′ phase, which are equal to or more than those of the conventional nitrification heat treatment even with only the NH 3 gas.

Further, the physical property may be implemented for a shorter time than that of the conventional nitrification heat treatment.

›BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a diagram illustrating a comparison between the temperature, atmospheric pressure, and the like of a heat treatment method according to the present disclosure with those of patented processes of the related art.

FIG. 2 is a diagram for explaining a difference in principle between the heat treatment method according to the present disclosure and the conventional method.

FIG. 3 is a diagram illustrating a microstructure by the heat treatment of Comparative Example 1 of the present disclosure.

FIG. 4 is a diagram illustrating a microstructure by the heat treatment of Comparative Example 1 of the present disclosure.

FIG. 5 is a diagram illustrating a microstructure by the heat treatment of Example 2 of the present disclosure.

FIG. 6 is a diagram illustrating a microstructure by the heat treatment of Example 4 of the present disclosure.

›DESCRIPTION OF SPECIFIC EMBODIMENTS · 1 of 2

To fully understand the present disclosure, the operational advantages of the present disclosure, and the object achieved by the practice of the present disclosure, reference should made to the accompanying drawings illustrating an embodiment of the present disclosure and the contents described in the accompanying drawings.

In describing the disclosed embodiment of the present disclosure, the description of the known technology or the repetitive description capable of unnecessarily obscuring the gist of the present disclosure has been reduced or omitted.

FIG. 1 is a diagram illustrating a comparison between the temperature, atmospheric pressure, and the like of a heat treatment method according to the present disclosure with those of related art patented processes.

Hereinafter, a heat treatment method of a component for a vehicle according to an embodiment of the present disclosure is described with reference to FIG. 1 .

In the related art, heat treatment for the durability of a component for a vehicle performs the heat treatment by additionally injecting nitrogen (N 2 ) to ammonia (NH 3 ) by a low-pressure process to adjust an equilibrium condition based on the ammonia resolution (Kn) to control the quality of a compound layer.

An ammonia resolution reaction formula is as follows.

NH 3 →N+2/3H 2

Further, the reaction equilibrium constant (K) is as follows.

K=P NH3 /{[N]+PH 2 2/3 }

Therefore, the ammonia resolution (Kn) is as follows.

Kn=K×[N]=P NH 3 /P H 2 2/3

Therefore, if the Kn is high, the partial pressure of the NH 3 is high, such that an available nitrogen amount is increased.

Upon the real heat treatment, the Kn is controlled by injecting N 2 or hydrogen (H 2 ), and the Kn is increased when N 2 is injected and the Kn is decreased when H 2 is injected.

The heat treatment condition according to the related art is summarized in Table 1 below. The related art 1 is the low-pressure process but the process is configured in the form of adding N 2 to NH 3 to adjust the Kn and controlling the physical property of the compound.

Unlike the aforementioned related arts, the present disclosure injects only the ammonia gas to adjust the atmospheric pressure and the flow rate within a heat treatment furnace to control the quality (reaction speed) of the compound layer.

In other words, the reaction (decomposition) speed of the gas is inversely proportional to the density of the gas molecules (density ↑→ collision between the gas molecules ↑→ reaction speed ↓).

Further, the reaction (decomposition) speed of the gas is inversely proportional to the gas flow speed within the furnace (gas speed ↑→ collision between gas molecules-component ↑→ reaction speed ↓).

Using the above, the present disclosure adjusts the ammonia decomposition speed through the combination of the temperature upon the heat treatment, the pressure within the furnace, and the flow rate within the furnace to control the thickness and the phase fraction of the compound layer.

When describing a difference in principle between the heat treatment method according to the present disclosure and the conventional method with reference to FIG. 2 , since the gas is injected after the ammonia resolution (Kn) is adjusted by mixing the gas, the ammonia resolution is converged to an equilibrium phase fraction rate determined by the heat treatment temperature+Kn with the time.

However, the present disclosure has no concept of adjusting the Kn separately, and the partial pressure of H 2 is 0, such that the Kn is infinite (determined by Kn=partial pressure of NH 3 /partial pressure of H 2 ).

In other words, since the ammonia is unlimitedly decomposed immediately from the surface of the component, the present disclosure has the concept which may be close to the concept of stopping the decomposition in the appropriate condition in which the temperature/the atmospheric pressure/the flow rate should be adjusted to adjust the quality (reaction speed) of the compound layer, rather than being converged to the equilibrium state.

The present disclosure summarized to be compared with Table 1 is expressed in Table 2 below. The contents of describing the conditions such as the temperature, pressure, and the like of the present disclosure and the related art in the graph are the same as those of FIG. 1 .

The heat treatment method of a component for a vehicle according to the present disclosure, i.e., the vacuum nitrification heat treatment process, may be summarized as follows with reference to Table 2.

In the heat treatment of a component for a vehicle according to the present disclosure, the manufactured metal (may be an iron-based) component is disposed in the inner space of the furnace for the heat treatment, and then the heating and the H 2 purge are performed.

The heating in one example is 400 to 600° C., and H 2 is purged until the pressure becomes 230 to 780 torr.

Thereafter, the heated temperature is maintained for the primary stabilization, and H 2 is supplied at the speed of 0.5 to 15 m 3 /h, such that the inner pressure becomes 230 to 400 torr, and the stabilization time in one example is within 2 hours.

After the primary stabilization, the temperature is maintained at 400 to 600° C., and only NH 3 is supplied.

NH 3 is supplied at the speed of 0.5 to 6 m 3 /h such that the inner pressure becomes 230 to 400 torr, and a secondary nitrification time in one example is 6 to 15 hours.

It may be confirmed that it is possible to secure the compound layer and the surface hardness for a short time by the aforementioned heat treatment condition. The Examples and experimental examples according to the present disclosure are summarized in Tables 3 and 4 below.

As summarized in Tables 3 and 4, it may be seen that it is possible to secure the surface characteristics in which the thickness of the compound is 8 to 20 μm, the thickness of the pore layer is 2 to 5 μm, the surface hardness is 620 to 710 Hv, and the diffusion layer is 0.5 mm or less, upon the heat treatment within a range of the nitrification conditions (the temperature, the pressure, the flow rate, and the time) according to the present disclosure. It may also be seen that it is possible to secure the γ′ phase of 50 to 90%.

›DESCRIPTION OF SPECIFIC EMBODIMENTS · 2 of 2

Further, Comparative Examples out of the range of the Examples of the present disclosure are summarized in Table 5 below.

It may be seen that Comparative Example 1 is the case where N 2 is mixed with NH 3 , and Comparative Example 2 is the case of comparing the normal pressure/low pressure with those of Example 2 with only NH 3 and the compound is insufficient. It may be seen that Comparative Example 3 is the case of comparing the normal pressure/low pressure with those of Example 19 with only NH 3 and the pore layer side is excessive, and the hardness and the phase fraction rate are insufficient. It may be seen that in Comparative Example 4, the temperature is insufficient, and the compound is insufficient, and in Comparative Example 5, the temperature is insufficient, and the compound is insufficient in the time excess condition. It may be seen that in Comparative Example 6, the gamma prime (γ′) phase, Fe4N fraction rate is rapidly decreased by the temperature excess to form an austenite.

It may be seen that in Comparative Example 7, the compound is insufficient due to the insufficiency of the flow rate. It may be seen that in Comparative Examples 8 and 9, the compound is not formed or insufficient due to the insufficiency of the atmospheric pressure. It may also be seen in Comparative Examples 10 and 11, the compound is insufficient due to the insufficiency of the time or the compound fraction rate is insufficient.

As described above, unlike the Comparative Examples, it may be seen that the Examples of the present disclosure may secure the surface characteristics in which the thickness of the compound layer is 8 to 20 μm, the pore layer is 2 to 5 μm, the surface hardness is 620 to 710 Hv, and the thickness of the diffusion layer is 0.5 mm or less when the corresponding heat treatment is performed, and may secure the γ′ phase of 50 to 90%.

FIGS. 3-6 are pictures or photographs of the real microstructures. FIG. 3 illustrates the microstructure of Comparative Example 1 of the condition of 540° C., 1 atmospheric pressure, and 22 hours, and illustrates that the thickness is 13.9 μm, the thickness of the pore layer is 3.0 μm, the hardness is 677 Hv, and the γ′ fraction rate is 87.3%.

FIG. 4 illustrates the microstructure of Comparative Example 2 of the condition of 540° C., 1 atmospheric pressure, and 10 hours, and illustrates that the thickness is 5.5 μm, the thickness of the pore layer is 0.7 μm, the hardness is 708 Hv, and the γ′ fraction rate is 78.5%.

On the other hand, FIG. 5 illustrates the microstructure of Example 2 of the condition of 540° C., 0.5 atmospheric pressure, and 10 hours, and illustrates that the thickness is 11.6 μm, the thickness of the pore layer is 3.5 μm, the hardness is 691 Hv, and the γ′ fraction rate is 75.9%. It may be seen that the compound is sufficient compared to Comparative Example 2 and is equal to that of Comparative Example 1.

Further, FIG. 6 illustrates the microstructure of Example 4 of the condition of 540° C., 0.3 atmospheric pressure, and 6 hours, and illustrates that the thickness is 12.1 μm, the thickness of the pore layer is 3.6 μm, the hardness is 670 Hv, and the γ′ fraction rate is 72.8%.

As described above, while the present disclosure has been described with reference to the drawings, the present disclosure is not limited to the described embodiment. It should be apparent to those having ordinary skill in the art that the present disclosure may be variously modified and changed without departing from the spirit and scope of the present disclosure. Therefore, the modified examples or the changed examples should be included in the claims of the present disclosure, and the scope of the present disclosure should be interpreted based on the appended claims.

›Tables in the description — 5
TABLE 1
AtmosphericFlow
ItemsTemperatureGaspressurerateTimeRemark
RelatedHeating:Heating: N 2 orHeating: XxHeating: X
Primary400~600° C.inert gasPrimaryPrimary
art 1PrimaryPrimarynitrification:nitrification:
nitrification:nitrification:10~800 torr1~6 hours
400~600° C.NH 3 + N 2SecondarySecondary
SecondarySecondarynitrification:nitrification: 2
nitrification:nitrification: N 2400~800 torrhours or more
400~600° C.
RelatedHeating:Heating: NH 3Heating: XxHeating:Nitrified
art 2480~560° C.Nitrification:Nitrification40~80 minutesgas NH 3
nitrification:NH 3 + N 3 + N 2 O500~300 mbarNitrification:50~80%
480~560° C.Cooling: N 2(38.5~230.9 torr)60~120N 2
(final heatingOxidation:Cooling: xminutes10~30%
temperatureN 2 + H 2 OOxidation: xCooling:N 2 O
maintenance)10~30 minutes5~20%
Cooling: finalOxidation:
heating10~50 minutes
temperature-
10~30° C.
Oxidation: final
cooling
maintenance
RelatedPrimary heatingPrimary heatPrimary heatxPrimary:Secondary/
art 3treatment:treatment: N 2treatment: 0.5~1.215~25 minutestertiary
440~490° C.Secondary heatatmosphericSecondary:gases
Secondarytreatment:pressure8~13minutesN 2 50%
heatingN 2 + CO 2(390~936 torr)Tertiary:CO 2 50%
treatment:Tertiary heatSecondary heat15~25 minutesPrimary
500~580° C.treatment:treatment: 0.8~1.2Primarynitrification
Tertiary heatingN 2 + CO 2atmosphericnitrification:gases
treatment:Primarypressure45~120NH3
550~580° C.nitrification:Tertiary heatminutes55~90%
PrimaryNH 3 + CO 2 + N 2treatment: xSecondary:CO 2
nitrification:SecondaryPrimary15~25 minutes5~10%
tertiary heatingnitrification:nitrification:Tertiary: xN 2
treatmentx(discharge)1.2~3.5Fourth: 30~605~35%
temperatureTertiaryatmosphericminutes
maintenancenitrification:pressure
Secondaryx(maintenance)(936~2730 torr)
nitrification:Cooling: N 2Secondary
temperaturenitrification:
maintenancex(discharge)
TertiaryTertiary
nitrification:nitrification:
450~500° C.x(maintenance)
Cooling 0° C.Cooling: x
RelatedHeating:Heating: N 2 afterHeating: vacuumxHeating: XOxidizing
art 4180~350° C.vacuumdischargePre-oxidation:gases
Pre-oxidation: xPre-oxidation:Pre-oxidation: X30~60 minutesNOx
Secondaryoxidizing gasSecondarySecondaryCOx
heating: xSecondaryheating: vacuumheating: Xair
Nitrification:heating: NH 3exhaustNitrification:
450~600° C.Nutrification:Nitrification:X
Cooling andNH 3 + N 2 +50~1000 mbarCooling and
oxidation:oxidizingCooling andoxidation:
450~520° C.gasoxidation: 15~100 minutes
Cooling:Cooling andatmosphericCooling: x
oxidationoxidation: H 2 Opressure
Cooling: N 2Cooling: vacuum
exhaust
TABLE 2 — Atmospheric
ItemsTemperatureGaspressureFlow rateTime
PresentHeating:Heating:Heating:PrimaryHeating: X
disclosure400~600° C.H 2 purge230~780 torrstabilization:Primary
PrimaryPrimaryPrimary0.5~15 m 3 /hstabilization:
stabilization:stabilization:stabilization:Secondarywithin 2 hours
400~600° C.H 2 (vacuum)230~400 torrstabilization:secondary
SecondarySecondarySecondary0.5~6 m 3 /hnitrification:
nitrification:nitrification:nitrification:6~15 hours
400~600° C.NH 3 (vacuum)230~400 torr
TABLE 3
FlowThicknessDepth
Atmos-rateThicknessofofγ′
Temper-phericofofporediffusionfractionHard-
aturepressureTimeNH 3compoundlayerlayerrateness
(° C.)(atm)(h)(m 3 /h)(μm)(μm)(mm)(%)(Hv)
Example5400.5619.72.10.3168.7678
1
Example5400.510111.63.50.3975.9691
2
Example5400.515112.54.00.4385.3682
3
Example5400.36112.13.60.3072.8670
4
Example5400.310112.33.90.4065.4637
5
Example5400.315113.14.00.4162.1625
6
Example5400.3100.510.84.00.3872.4671
7
Example5400.310611.53.70.4069.7668
8
Example5800.56114.74.60.4251.4651
9
Example5800.515116.84.80.4958.7620
10
Example5800.36113.93.90.4062.1664
11
Example5800.315117.24.30.4754.2630
12
Example5100.5619.12.00.2379.1708
13
Example5100.51519.82.20.3188.4689
14
Example5100.3619.32.10.2280.4696
15
Example5100.315110.02.20.3085.7695
16
Example4500.360.58.02.10.2089.7707
17
Example4500.31519.12.20.2483.4699
18
Example5800.515619.84.30.4951.1624
19
TABLE 4 — Atmospheric
TemperaturepressureTimeFlow rate
Example 1—Upper limitLower limit—
Example 2—Upper limit——
Example 3—Upper limitUpper limit—
Example 4—Lower limitLower limit—
Example 5—Lower limit——
Example 6—Lower limitUpper limit—
Example 7—Lower limit—Lower limit
Example 8—Lower limit—Upper limit
Example 9Upper limitUpper limitLower limit—
Example 10Upper limitUpper limitUpper limit—
Example 11Upper limitLower limitLower limit—
Example 12Upper limitLower limitUpper limit—
Example 13—Upper limitLower limit—
Example 14—Upper limitUpper limit—
Example 15—Lower limitLower limit—
Example 16—Lower limitUpper limit—
Example 17Lower limitLower limitLower limitLower limit
Example 18Lower limitLower limitUpper limit—
Example 19Upper limitUpper limitUpper limitUpper limit
TABLE 5
FlowThicknessDepth
Atmos-rateThicknessofofγ′
Temper-phericofofporediffusionfractionHard-
aturepressureTimeNH 3compoundlayerlayerrateness
(° C.)(atm)(h)(m 3 /h)(μm)(μm)(mm)(%)(Hv)
Compar-5401.0221013.93.00.4187.3677
ative
Example
1
Compar-5401.01015.50.70.3778.5708
ative
Example
2
Compar-5801.015622.44.80.4225.8626
ative
Example
3
Compar-4300.51513.80.70.1992.1716
ative
Example
4
Compar-4300.52015.10.70.2090.4706
ative
Example
5
Compar-6000.56125.75.70.3727.1594
ative
Example
6
Compar-5400.5100.36.92.40.3477.2661
ative
Example
7
Compar-5100.2151——0.08——
ative
Example
8
Compar-5400.21014.20.80.3477.2661
ative
Example
9
Compar-5400.5517.11.80.2660.2659
ative
Example
10
Compar-5800.55111.33.90.3737.4609
ative
Example
11

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IPC · International Patent Classification
Section C — Chemistry; metallurgy
  • C23C8/26

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