U.S. patent application number 16/240930 was filed with the patent office on 2020-07-09 for methods to avoid over-developed aluminized coatings during hot stamping line stoppages.
This patent application is currently assigned to Ford Motor Company. The applicant listed for this patent is Ford Motor Company. Invention is credited to Maik Broda, Elizabeth Bullard, Constantin Chiriac, Kyle Fleeger, Jagbir Guron, Torsten Hallfeldt.
Application Number | 20200216922 16/240930 |
Document ID | / |
Family ID | 71104240 |
Filed Date | 2020-07-09 |
United States Patent
Application |
20200216922 |
Kind Code |
A1 |
Chiriac; Constantin ; et
al. |
July 9, 2020 |
METHODS TO AVOID OVER-DEVELOPED ALUMINIZED COATINGS DURING HOT
STAMPING LINE STOPPAGES
Abstract
A method of treating a blank is provided. The method includes
moving a blank through a first section of a furnace at an
inter-critical temperature and through a second section of the
furnace at a critical temperature greater than the inter-critical
temperature before hot stamping the blank. Movement of the blank
from the first section to the second section of the furnace is
delayed during a hot stamping line stoppage. The blank is in the
first section of the furnace for a first time period and in the
second section of the furnace a second time period less than the
first time period. Also, the first section of the furnace may have
a first length and in the second section of the furnace may have a
second length that is less than the first length.
Inventors: |
Chiriac; Constantin;
(Windsor, CA) ; Broda; Maik; (Wuerselen, DE)
; Fleeger; Kyle; (Westland, MI) ; Guron;
Jagbir; (Dearborn, MI) ; Hallfeldt; Torsten;
(Eschweiler, DE) ; Bullard; Elizabeth; (Royal Oak,
MI) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Ford Motor Company |
Dearborn |
MI |
US |
|
|
Assignee: |
Ford Motor Company
Dearborn
MI
|
Family ID: |
71104240 |
Appl. No.: |
16/240930 |
Filed: |
January 7, 2019 |
Current U.S.
Class: |
1/1 |
Current CPC
Class: |
C21D 1/18 20130101; C23C
2/28 20130101; C21D 1/673 20130101; C23C 2/12 20130101; C23C 2/40
20130101; C21D 2221/00 20130101 |
International
Class: |
C21D 1/673 20060101
C21D001/673; C21D 1/18 20060101 C21D001/18; C23C 2/12 20060101
C23C002/12; C23C 2/28 20060101 C23C002/28; C23C 2/40 20060101
C23C002/40 |
Claims
1. A method of treating a blank comprising: moving a blank through
a first section of a furnace at an inter-critical temperature and
through a second section of the furnace at a critical temperature
greater than the inter-critical temperature; and hot stamping the
blank, wherein movement of the blank from the first section to the
second section of the furnace is delayed during a hot stamping line
stoppage.
2. The method according to claim 1, wherein the blank is in the
first section of the furnace for a first time period and in the
second section of the furnace a second time period less than the
first time period.
3. The method according to claim 2, wherein the first time period
is at least 1.2 times greater than the second time period.
4. The method according to claim 1, wherein the first section of
the furnace has a first length and the second section of the
furnace has a second length less than the first length.
5. The method according to claim 1, wherein the first length is at
least 1.2 times greater than and the second length.
6. The method according to claim 1, wherein the blank is formed
from coated press hardenable steel.
7. The method according to claim 1, wherein the blank is formed
from aluminized press hardenable steel, the inter-critical
temperature is between 725.degree. C. and 825.degree. C., and the
critical temperature is above 910.degree. C.
8. The method according to claim 1, wherein the blank is formed
from aluminized press hardenable steel, the inter-critical
temperature is between 750.degree. C. and 800.degree. C., and the
critical temperature is above 920.degree. C.
9. The method according to claim 8, wherein the blank is positioned
in the first section of the furnace at the inter-critical
temperature for a time period up to 1200 seconds before moving to
the second section of the furnace and being hot stamped.
10. The method according to claim 9, wherein the hot stamped blank
comprises an inter-diffusion layer with a thickness less than 16
.mu.m.
11. The method according to claim 8, wherein the blank is
positioned in the first section of the furnace at the
inter-critical temperature for a time period up to 1800 seconds
before moving to the second section of the furnace and being hot
stamped, and the hot stamped blank comprises an inter-diffusion
layer with a thickness less than 16 .mu.m.
12. The method according to claim 8, wherein the blank is
positioned in the first section of the furnace at the
inter-critical temperature for a time period up to 2400 seconds
before moving to the second section of the furnace and being hot
stamped, and the hot stamped blank comprises an inter-diffusion
layer with a thickness less than 16 .mu.m.
13. The method according to claim 1, wherein: the blank is formed
from aluminized press hardenable steel; the blank is in the first
section of the furnace during the hot stamping line stoppage for a
time period up to 1800 seconds; the blank moves from the first
section to the second section and is hot stamped after the hot
stamping line stoppage is over; and the hot stamped blank comprises
an inter-diffusion layer with a thickness less than 16 .mu.m.
14. The method according to claim 13, wherein the inter-critical
temperature is between 725.degree. C. and 825.degree. C., and the
critical temperature is between 910.degree. C. and 950.degree.
C.
15. The method according to claim 1, wherein: the blank is formed
from aluminized press hardenable steel; the inter-critical
temperature is between 750.degree. C. and 800.degree. C., and the
critical temperature is between 920.degree. C. and 940.degree. C.
the blank is in the first section of the furnace during the hot
stamping line stoppage for a time period up to 2400 seconds; the
blank moves from the first section to the second section and is hot
stamped after the hot stamping line stoppage is over; and the hot
stamped blank comprises an inter-diffusion layer with a thickness
less than 16 .mu.m.
16. A method of treating a plurality of blanks during stoppage of a
hot stamping line, the method comprising: heating a first section
of a furnace to an inter-critical temperature between 725.degree.
C. and 825.degree. C.; heating a second section of the furnace to a
critical temperature between 910.degree. C. and 950.degree. C.; and
moving a plurality of blanks on a conveyer line through the first
section and the second section of the furnace to a hot stamping
press and hot stamping the plurality of blanks; wherein: the
conveyer line stops moving during stoppage of the hot stamping line
such that a subset of blanks in the first section of the furnace do
not move into the second section of the furnace; and the conveyer
line starts moving after the stoppage of the hot stamping line is
over such that the subset of blanks in the first section of the
furnace move into and through the second section of the furnace and
to the hot stamping press.
17. The method according to claim 16, wherein the plurality of
blanks is formed from aluminized press hardenable steel and the
subset of blanks hot stamped by the hot stamping press after the
stoppage of the hot stamping line is over comprise an
inter-diffusion layer thickness less than 16 .mu.m.
18. The method according to claim 17, wherein the stoppage of the
hot stamping line is for a time up to 1800 seconds.
19. A method of hot stamping a blank after stoppage of a hot
stamping line comprising: heating a blank formed from a coated
press hardenable steel in a first section of a roller hearth
furnace to an inter-critical temperature for a first time period;
heating the blank in a second section of the roller hearth furnace
to a critical temperature greater than the inter-critical
temperature for a second time period less than the first time
period; stopping the blank from moving from the first section to
the second section of the roller hearth furnace during stoppage of
the hot stamping line; moving the blank from the first section to
the second section of the roller hearth furnace after the stoppage
of the hot stamping line is over; and hot stamping the blank after
it moves through the second section of the furnace, wherein the
blank is positioned in the first section of the roller hearth
furnace for up to 2400 seconds and the hot stamped blank has an
inter-diffusion layer less than 16 .mu.m.
20. The method according to claim 19, wherein the inter-critical
temperature is between 725.degree. C. and 825.degree. C., and the
critical temperature is above 910.degree. C.
Description
FIELD
[0001] The present disclosure relates to hot forming steels, and
particularly, to hot stamping of coated press hardenable steel.
BACKGROUND
[0002] The statements in this section merely provide background
information related to the present disclosure and may not
constitute prior art.
[0003] Hot stamping and forming parts out of a press hardenable
steel (PHS) generally requires heating a PHS blank into the
intercritically (e.g., between 750.degree. C. and 850.degree. C.)
or austenitic phase region (e.g., above 900.degree. C.) of the
steel, hot stamping the PHS blank, and cooling the hot stamped PHS
blank such that a hot stamped PHS part with a martensitic
microstructure is provided. However, heating the PHS blank into the
austenitic phase region results in undesirable oxidation of the
PHS. Accordingly, PHS material is typically provided by steel
suppliers with an oxidation resistant coating, for example, an
aluminum-silicon alloy coating formed by dipping or passing the PHS
through a liquid aluminum-silicon alloy bath. Such coated PHS is
often referred to as aluminized PHS. Upon heating an aluminized PHS
blank, diffusion between the aluminum-silicon alloy coating and the
PHS results in at least two layers, one of which is an
interdiffusion layer (IDL) between the PHS and an outer aluminized
alloy layer. Unfortunately, the IDL affects welding, particularly
resistance welding, of a hot stamped part. Also, studies have shown
that an IDL with a thickness equal to or greater than 16
micrometers (.mu.m) prevents resistance welding of hot stamped
aluminized PHS parts.
[0004] The present disclosure addresses the issues of IDL thickness
among other issues related to hot stamping of steels that have an
aluminized coating.
SUMMARY
[0005] This section provides a general summary of the disclosure
and is not a comprehensive disclosure of its full scope or all of
its features.
[0006] In one form of the present disclosure, a method of treating
a blank is provided. The method comprises moving a blank through a
first section of a furnace at an inter-critical temperature and
through a second section of the furnace at a critical temperature
greater than the inter-critical temperature; and hot stamping the
blank, wherein movement of the blank from the first section to the
second section of the furnace is delayed during a hot stamping line
stoppage.
[0007] In some aspects of the present disclosure, the blank is in
the first section of the furnace for a first time period and in the
second section of the furnace a second time period less than the
first time period. In such aspects, the first time period is at
least 1.2 times greater than the second time period, for example,
at least 1.5 times greater or at least 2.0 times greater than the
second time period. In the alternative, or in addition to, the
first section of the furnace has a first length and the second
section of the furnace has a second length less than the first
length. For example, in some aspects of the present disclosure, the
first length is at least 1.2 times greater than the second length,
for example, at least 1.5 times greater or at least 2.0 times
greater than the second length.
[0008] In some aspects of the present disclosure, the blank is a
coated press hardenable steel and the inter-critical temperature is
between 725.degree. C. and 825.degree. C., and the critical
temperature is above 910.degree. C. In such aspects, the
inter-critical temperature may be between 750.degree. C. and
800.degree. C., and the critical temperature may be above
920.degree. C.
[0009] In some aspects of the present disclosure, the blank is
positioned in the first section of the furnace at the
inter-critical temperature for a time period up to 1200 seconds
before moving to the second section of the furnace and being hot
stamped. Also, the hot stamped blank comprises an inter-diffusion
layer with a thickness less than 16 .mu.m.
[0010] In other aspects of the present disclosure, the blank is
positioned in the first section of the furnace at the
inter-critical temperature for a time period up to 1800 seconds
before moving to the second section of the furnace and being hot
stamped, and the hot stamped blank comprises an inter-diffusion
layer with a thickness less than 16 .mu.m.
[0011] In still other aspects of the present disclosure, the blank
is positioned in the first section of the furnace at the
inter-critical temperature for a time period up to 2400 seconds
before moving to the second section of the furnace and being hot
stamped, and the hot stamped blank comprises an inter-diffusion
layer with a thickness less than 16 .mu.m.
[0012] In some aspects of the present disclosure, the blank is
formed from aluminized press hardenable steel, it is in the first
section of the furnace during the hot stamping line stoppage for a
time period up to 1800 seconds. The blank moves from the first
section to the second section and is hot stamped after the hot
stamping line stoppage is over and the hot stamped blank comprises
an inter-diffusion layer with a thickness less than 16 .mu.m.
[0013] In another form of the present disclosure, a method of
treating a plurality of blanks during stoppage of a hot stamping
line is provided. The method comprises heating a first section of a
furnace to an inter-critical temperature between 725.degree. C. and
825.degree. C., heating a second section of the furnace to a
critical temperature between 910.degree. C. and 950.degree. C.,
moving a plurality of blanks on rollers (e.g. rollers of a roller
hearth furnace) through the first section and the second section of
the furnace to a hot stamping press, and hot stamping the plurality
of blanks. When the rollers stop moving during stoppage of the hot
stamping line, a subset of blanks in the first section of the
furnace do not move into the second section of the furnace. When
the rollers start moving after the stoppage of the hot stamping
line is over, the subset of blanks in the first section of the
furnace move into and through the second section of the furnace and
to the hot stamping press.
[0014] In some aspects of the present disclosure, the plurality of
blanks is formed from aluminized press hardenable steel and the
subset of blanks hot stamped by the hot stamping press after the
stoppage of the hot stamping line is over comprise an
inter-diffusion layer thickness less than 16 .mu.m. Also, the
stoppage of the hot stamping line is for a time up to 1800
seconds.
[0015] In yet another form of the present disclosure, a method of
hot stamping a blank after stoppage of a hot stamping line is
provided. The method comprises heating a blank formed from a coated
press hardenable steel in a first section of a roller hearth
furnace to an inter-critical temperature for a first time period
and heating the blank in a second section of the roller hearth
furnace to a critical temperature greater than the inter-critical
temperature for a second time period less than the first time
period. The blank stops moving from the first section to the second
section of the roller hearth furnace during stoppage of the hot
stamping line. Also, the blank moves from the first section to the
second section of the roller hearth furnace after the stoppage of
the hot stamping line is over. The blank is hot stamped after it
moves through the second section of the furnace. In some aspects of
the present disclosure, the blank is positioned in the first
section of the roller hearth furnace for up to 2400 seconds and the
hot stamped blank has an inter-diffusion layer less than 16 .mu.m.
Also, the inter-critical temperature is between 725.degree. C. and
825.degree. C., and the critical temperature is above 910.degree.
C.
[0016] Further areas of applicability will become apparent from the
description provided herein. It should be understood that the
description and specific examples are intended for purposes of
illustration only and are not intended to limit the scope of the
present disclosure.
DRAWINGS
[0017] In order that the disclosure may be well understood, there
will now be described various forms thereof, given by way of
example, reference being made to the accompanying drawings, in
which:
[0018] FIG. 1 schematically depicts a baseline hot stamping line
for producing parts from aluminized press hardenable steel
(PHS);
[0019] FIG. 2 graphically depicts a baseline heating schedule
(profile) for the hot stamping line in FIG. 1;
[0020] FIG. 3 schematically depicts a hot stamping line for
producing parts from aluminized press hardenable steel (PHS)
according to the teachings of the present disclosure;
[0021] FIG. 4 graphically depicts a heating profile for the hot
stamping line in FIG. 3 according to the teachings of the present
disclosure;
[0022] FIG. 5 is a flow chart of a method of treating a blank
according to the teachings of the present disclosure;
[0023] FIG. 6 is a flow chart of a method of treating a plurality
of blanks during stoppage of a hot stamping line according to the
teachings of the present disclosure;
[0024] FIG. 7 is a micrograph of a press hardenable steel (PHS)
with an aluminized coating following a baseline heat treatment
graphically depicted in FIG. 2;
[0025] FIG. 8A is a micrograph of a PHS with an aluminized coating
following 10 minutes of heat treatment at an inter-critical
temperature T.sub.IC graphically depicted in FIG. 4 according to
the teachings of the present disclosure;
[0026] FIG. 8B is a micrograph of a boron steel with an aluminized
coating following 20 minutes of heat treatment at an inter-critical
temperature T.sub.IC graphically depicted in FIG. 4 according to
the teachings of the present disclosure;
[0027] FIG. 8C is a micrograph of a boron steel with an aluminized
coating following 30 minutes of heat treatment at an inter-critical
temperature T.sub.IC graphically depicted in FIG. 4 according to
the teachings of the present disclosure;
[0028] FIG. 8D is a micrograph of a boron steel with an aluminized
coating following 40 minutes of heat treatment at an inter-critical
temperature T.sub.IC graphically depicted in FIG. 4 according to
the teachings of the present disclosure;
[0029] The drawings described herein are for illustration purposes
only and are not intended to limit the scope of the present
disclosure in any way.
DETAILED DESCRIPTION
[0030] The following description is merely exemplary in nature and
is not intended to limit the present disclosure, application, or
uses. It should be understood that throughout the drawings,
corresponding reference numerals indicate like or corresponding
parts and features. Examples are provided to fully convey the scope
of the disclosure to those who are skilled in the art. Numerous
specific details are set forth such as types of specific
components, devices, and methods, to provide a thorough
understanding of variations of the present disclosure. It will be
apparent to those skilled in the art that specific details need not
be employed and that the examples provided herein, may include
alternative embodiments and are not intended to limit the scope of
the disclosure. In some examples, well-known processes, well-known
device structures, and well-known technologies are not described in
detail.
[0031] The present disclosure addresses the issues of
interdiffusion layer (IDL) thickness and coating thickness
increases due to total furnace time and other issues related to hot
stamping steels that have an aluminized coating.
[0032] Referring now to FIG. 1, a baseline hot stamping line 10 for
producing parts from aluminized press hardenable steel (PHS) is
schematically depicted. In one form of the present disclosure, the
baseline hot stamping line 10 generally includes a furnace transfer
station 100, a furnace 110, a hot stamping transfer station 120, a
hot stamping station 130, and a post-hot stamping transfer station
140. The furnace transfer station 100 transfers aluminized press
hardenable steel (PHS) blanks 52 from a stack of aluminized PHS
blanks 50 to a conveyer line 112 of the furnace 110. One
non-limiting example of the furnace 110 is a roller hearth furnace
and the conveyer line 112 is a plurality of rollers. The conveyer
line 112 moves the aluminized PHS blanks 52 from a first end 114 to
a second end 116 of the furnace 110 where the hot stamping transfer
station 120 moves the aluminized PHS blanks 52 to the hot stamping
station 130. The aluminized PHS blanks 52 are hot stamped at the
hot stamping station 130 to form a hot stamped part 54 and then
removed therefrom and moved to a subsequent station (not shown) by
the post-hot stamping transfer station 140.
[0033] It should be understood that the thickness of an IDL of an
aluminized PHS blank 52 prior to being hot stamped at the hot
stamping station 130 is a function of its distance-temperature
history (also referred to herein as "distance-temperature
profile"). One example of distance-temperature profile for a
plurality of aluminized PHS blanks 52 moving along the baseline hot
stamping line 10 is graphically depicted in FIG. 2. In such an
example, the thickness of the IDL is a function of the temperature
T.sub.F of the furnace 110 (also referred to herein as the "furnace
temperature"), residence (dwell) time 22 of the aluminized PHS
blank 52 in the furnace temperature 110 (also referred to herein as
the "dwell time"), and total time 24 of the aluminized PHS blank 52
in the furnace 110 also referred to herein as the "total furnace
time"). As used herein, "total furnace time" refers to the time 20
to heat an aluminized PHS blank 52 from room temperature T.sub.R to
furnace temperature T.sub.F plus the dwell time 22. It should also
be understood that the temperature of the aluminized PHS blank 52
decreases after removal from the furnace 110, during hot stamping
at the hot stamping station 130 and during cooling after being hot
stamped as graphically depicted by section 26 in FIG. 2.
[0034] Unfortunately, there are issues which cause stoppage of the
baseline hot stamping line 10 and thereby result in aluminized PHS
blanks 52 exceeding 10 minutes of dwell time 22 at the critical
temperature T.sub.C. Also, these delays turn the affected
aluminized PHS blanks 52 into production waste because they are
rendered unsuitable for further processing as the weldability of
the blanks is greatly reduced due to the excessive IDL thickness
and porous coating.
[0035] As noted above, an IDL thickness equal to or greater than 16
.mu.m reduces the weldability of the aluminized PHS blank 52 to
about zero. As such, current production specifications limit the
total furnace time 24 such that the IDL thickness is less than 16
.mu.m. For example, depending on the thickness of the PHS blank 52
and the type of oxidation resistant coating thereon, total furnace
time 24 is limited to between 3 to 10 minutes. That is, if
aluminized PHS blanks 52 are held in the furnace for a time longer
than the prescribed dwell time 22, e.g., due a stoppage of the hot
stamping line 10, such aluminized PHS blanks 52 have an IDL
thickness greater than 16 .mu.m and are typically scrapped. This
time at temperature dependent scrapping of blanks increases the
expense of the hot stamping process due to lower material yields,
wasted energy, wasted labor, etc.
[0036] Referring now to FIGS. 3 and 4, a hot stamping line 10' and
a distance-temperature profile according to the teachings of the
present disclosure are shown. Particularly, the furnace transfer
station 100 transfers aluminized press hardenable steel (PHS)
blanks 52 from a stack of aluminized PHS blanks 50 to the conveyer
line 112 of the furnace 110. The conveyer line 112 moves the
aluminized PHS blanks 52 from the first end 114 and through a first
section 111 of the furnace 110 at an inter-critical temperature
T.sub.IC, through a second section 113 of the furnace 110 at a
critical temperature T.sub.C, and to the second end 116 of the
furnace 110. In some aspects of the present disclosure the first
section of the furnace 110 extends from the first end 114 to a
divider 115 and the second section of the furnace 113 extends from
the divider 115 to the second end 116. In such aspects, the divider
115 may be a baffle, an insulated panel, and the like. In the
alternative, the divider 115 may simply represent a change in the
power settings of heater element or burners (not shown) positioned
in the first section 111 versus the heater elements or burners
positioned in the second section 113.
[0037] During movement of the aluminized PHS blank 52 through the
first section 111 of the furnace 110, the aluminized PHS steel
blank is heated to the inter-critical temperature T.sub.IC during a
first transient time period 30 and held at the inter-critical
temperature T.sub.IC for a first time period 32. Upon reaching the
second section 113 of the furnace 110, the aluminized PHS blank 52
is heated to the critical temperature TC during a second transient
time period 34 and held at the critical temperature TC for a second
time period 36. When the aluminized PHS blank 52 reaches the second
end 116 of the furnace 110 the hot stamping transfer station 120
moves the aluminized PHS blanks 52 to the hot stamping station 130
where it is hot stamped and quenched to form a hot stamped PHS part
54. Thereafter, post-hot stamping transfer station 140 transfers
the hot stamped PHS part 54 to a subsequent station (not
shown).
[0038] The inter-critical temperature T.sub.IC corresponds to a
ferrite plus austenite microstructure in the aluminized PHS blank
52 and the T.sub.C corresponds to a fully austenite microstructure
in the aluminized PHS blank 52. The T.sub.C and T.sub.IC are
dependent upon the composition of the boron steel. The
inter-critical temperature T.sub.IC is sufficiently high such that
iron diffuses from the PHS steel into the aluminum-silicon alloy
coating to form the eutectic AlSi.sub.10Fe.sub.3 alloy layer in a
short time frame (e.g., seconds). The solidification temperature of
the eutectic AlSi.sub.10Fe.sub.3 alloy layer is greater than the
melting temperature of the aluminum-silicon alloy layer thereby
providing a solid (i.e., not liquid) aluminized coating on the
aluminized PHS blank 52 as it moves through the furnace 110. Also,
the solid eutectic AlSi.sub.10Fe.sub.3 alloy layer is not removed
from the aluminized PHS blank 52 and transferred to the conveyer
line 112 (e.g., rollers). Heating the aluminized PHS blank 52 to
the critical temperature T.sub.C, i.e., heating the aluminized PHS
blank 52 into the fully austenitic phase region, followed by
cooling and quenching in the region 26 graphically depicted in FIG.
4, transforms the austenite into martensite, martensite plus
retained austenite and/or martensite and bainite. Accordingly, the
distance-temperature profile graphically depicted in FIG. 4 allows
for hot stamping of aluminized PHS blanks 52 such that high
strength parts are formed. However, and unlike the
distance-temperature profile in FIG. 2, the distance-temperature
profile graphically depicted in FIG. 4 allows for the aluminized
PHS blanks 52 to remain in the furnace 110 for times greater than
10 minutes without developing an IDL greater than 16 .mu.m. That
is, in the event of a stoppage of the hot stamping line 10,
diffusion between the PHS steel blank and the eutectic
AlSi.sub.10Fe.sub.3 alloy layer at the inter-critical temperature
T.sub.IC is such that more than 10 minutes, e.g., more than 30
minutes, is needed before the IDL is equal to or greater than 16
.mu.m as described in greater detail below.
[0039] Referring now referring to FIG. 5, a method 60 of treating a
coated PHS blank is provided. At step 62, the method 60 comprises
moving a coated PHS blank through a first section of a furnace at
an inter-critical temperature and through a second section of the
furnace at a critical temperature greater than the inter-critical
temperature. The coated PHS blank is hot stamped at step 64 and
movement of the blank from the first section to the second section
of the furnace is delayed during a hot stamping line stoppage.
[0040] Referring now to FIG. 6, a method 70 of treating a plurality
of aluminized PHS blanks during stoppage of a hot stamping line is
provided. The method 70 includes heating a first section of a
furnace to an inter-critical temperature between 725.degree. C. and
825.degree. C. at step 71 and heating a second section of the
furnace to a critical temperature between 910.degree. C. and
950.degree. C. at step 72. A plurality of aluminized PHS blanks are
moved through the first section and the second section of the
furnace on a conveyor belt to a hot stamping press at step 73. At
step 74, the conveyor belt is stopped for a time period up to 40
minutes during a hot stamping line stoppage such that aluminized
PHS blanks in the first section of the furnace do not move into the
second section of the furnace. The conveyor belt is re-started
after the hot stamping line stoppage is over (i.e., the hot
stamping line is moving again) at step 75 and the aluminized PHS
blanks held in the first section are moved to the second section of
the furnace and to a hot stamping station. At step 76, the
aluminized PHS blanks held in the first section of the furnace for
the time period up to 40 minutes are hot stamped such that hot
stamped aluminized PHS parts are provided. It should be understood
that the hot stamped aluminized PHS parts formed from the
aluminized PHS blanks held in the first section for up to 40
minutes have an IDL thickness of less than 16 .mu.m and thereby can
be successfully resistance welded. It should also be understood
that the aluminized PHS blanks held in the first section for up to
40 minutes exhibited desired mechanical properties that meet or
exceed predefined strength, ductility and/or impact resistance
levels.
EXAMPLES
[0041] Samples of aluminized PHS were subjected to
distance-temperature profiles as graphically depicted in FIG. 4 for
first time periods 32 ranging from 10 to 40 minutes and a second
time period 36 equal to 3 minutes. The aluminized PHS material was
obtained from the company ARCELORMITTAL.TM. with the coating and
PHS compositional ranges shown in Table 1 below. It should be
understood that other alloys, for example other PHSs currently
available, PHSs currently being developed but not yet commercially
available, and PHSs yet to be developed, can be used with the
methods disclosed herein and thereby fall within the scope of the
teachings of the present disclosure.
TABLE-US-00001 TABLE 1 Element Min. wt. % Max. wt. % Aluminized
coating Iron (Fe) 0 .ltoreq.3 Silicon (Si) >0 .ltoreq.10
Aluminum (Al) Balance Boron Steel Aluminum (Al) 0.02 0.06 Boron (B)
0 0.005 Carbon (C) 0.2 0.25 Chromium (Cr) 0 0.35 Copper (Cu) 0 0.2
Manganese (Mn) 1.1 1.4 Molybdenum (Mo) 0 0.35 Nitrogen (N) 0 0.009
Phosphorus (P) 0 0.025 Silicon (Si) 0 0.5 Sulfur (S) 0 0.008
Titanium (Ti) 0.02 0.05 Iron (Fe) Balance plus impurities
[0042] The inter-critical temperature was between 750.degree. C.
and 800.degree. C. and the critical temperature was 930.degree. C.
The samples were metallographically prepared and examined using
optical microscopy and compared to a baseline PHS sample subjected
to the distance-temperature profile graphically depicted in FIG. 2
with a dwell time 22 of less than 10 minutes and a critical
temperature T.sub.C of 930.degree. C.
[0043] Referring now to FIG. 7, an optical microscopy image (also
referred to herein as a "micrograph") of the baseline aluminized
coating on the PHS sample subjected to the distance-temperature
profile graphically depicted in FIG. 2 with a dwell time 22 of less
than 5 minutes is shown. As shown in FIG. 7, the average IDL
thickness was about 5 .mu.m and the outer eutectic
AlSi.sub.10Fe.sub.3 alloy layer was about 26.6 .mu.m. Given that
the IDL thickness is less than 16 .mu.m, such an aluminized PHS
sample is suitable for hot stamping and subsequent resistance
welding.
[0044] Referring now to FIGS. 8A-8D, micrographs of the PHS samples
subjected to the distance-temperature profiles graphically depicted
in FIG. 4 are shown. Particularly, FIG. 8A-8D are micrographs of
aluminized PHS samples subjected to the inter-critical temperature
T.sub.IC for a first time period 32 equal to 10 minutes, 20
minutes, 30 minutes, and 40 minutes, respectively, and the critical
temperature T.sub.C for a second time period equal to 3 minutes.
The average total coating thickness, average IDL thickness, and
average eutectic AlSi.sub.10Fe.sub.3 alloy layer thickness (labeled
as "Ave. Coating Thickness") for all of the aluminized PHS samples
are provided below in Table 2. As shown in Table 2, all of the
aluminized PHS samples subjected to distance-temperature profiles
graphically depicted in FIG. 4 had an IDL thickness less than 16
.mu.m, even the aluminized PHS sample subjected to the
inter-critical temperature T.sub.IC for 40 minutes. Accordingly, in
the event of a stoppage of the hot stamping line 10' (FIG. 3)
greater than 10 minutes, aluminized PHS blanks 52 held in the first
section 111 of the furnace 110 can be used to produce hot stamped
PHS parts 54 and thereby not scrapped.
TABLE-US-00002 TABLE 2 Time in Average Total Ave. IDL Ave. Coating
furnace Coating Thickness Thickness (minutes) Thickness (.mu.m)
(.mu.m) (.mu.m) FIG. 7 5 31.6 5 26.6 FIG. 8A 10 38.5 6.7 31.8 FIG.
8B 20 36.5 8.1 28.4 FIG. 8C 30 37.7 7.9 29.8 FIG. 8D 40 35.7 9.4
26.3
[0045] In some aspects of the present disclosure, a longer roller
hearth furnace compared to traditional roller hearth furnaces used
in hot stamping lines is used in the methods disclosed herein. It
should be understood that the increase in length of the roller
hearth furnace may increase the cost of the roller hearth furnace.
However, the additional length of travel at temperature in the
longer roller hearth furnace provides an increase in the number of
blanks per unit area, feed rate of the blanks through the furnace,
the number of temperature zones, and/or the temperature per zone.
The inventors have modelled the process in non-roller hearth
furnaces which are also within the scope of the present disclosure.
The present disclosure is also applicable to zinc-coated press
hardened steels.
[0046] The present disclosure reduces the scrap rate, blanks will
still experience quality control following an unplanned line
stoppage, however the scrap rate has a potential of being 80% with
some models placing the scrap rate below 50%, 30%, or 10%. However,
even an 80% scrap rate is a marked improvement over the current
100% scrap rate.
[0047] Although the terms first, second, third, etc. may be used to
describe various elements, components, regions, layers and/or
sections, these elements, components, regions, layers and/or
sections, should not be limited by these terms. These terms may be
only used to distinguish one element, component, region, layer
and/or section, from another element, component, region, layer
and/or section. Terms such as "first," "second," and other
numerical terms when used herein do not imply a sequence or order
unless clearly indicated by the context. Thus, a first element,
component, region, layer or section, could be termed a second
element, component, region, layer or section without departing from
the teachings of the example forms. Furthermore, an element,
component, region, layer or section may be termed a "second"
element, component, region, layer or section, without the need for
an element, component, region, layer or section termed a "first"
element, component, region, layer or section.
[0048] As used herein, the phrase at least one of A, B, and C
should be construed to mean a logical (A OR B OR C), using a
non-exclusive logical OR, and should not be construed to mean "at
least one of A, at least one of B, and at least one of C.
[0049] Unless otherwise expressly indicated, all numerical values
indicating mechanical/thermal properties, compositional
percentages, dimensions and/or tolerances, or other characteristics
are to be understood as modified by the word "about" or
"approximately" in describing the scope of the present disclosure.
This modification is desired for various reasons including
industrial practice, manufacturing technology, and testing
capability.
[0050] The terminology used herein is for the purpose of describing
particular example forms only and is not intended to be limiting.
The singular forms "a," "an," and "the" may be intended to include
the plural forms as well, unless the context clearly indicates
otherwise. The terms "including," and "having," are inclusive and
therefore specify the presence of stated features, integers, steps,
operations, elements, and/or components, but do not preclude the
presence or addition of one or more other features, integers,
steps, operations, elements, components, and/or groups thereof. The
method steps, processes, and operations described herein are not to
be construed as necessarily requiring their performance in the
particular order discussed or illustrated, unless specifically
identified as an order of performance. It is also to be understood
that additional or alternative steps may be employed.
[0051] The description of the disclosure is merely exemplary in
nature and, thus, examples that do not depart from the substance of
the disclosure are intended to be within the scope of the
disclosure. Such examples are not to be regarded as a departure
from the spirit and scope of the disclosure. The broad teachings of
the disclosure can be implemented in a variety of forms. Therefore,
while this disclosure includes particular examples, the true scope
of the disclosure should not be so limited since other
modifications will become apparent upon a study of the drawings,
the specification, and the following claims.
* * * * *