Technical Field
[0001] The present invention relates to a precipitation hardening martensite stainless steel
exhibiting high strength and ductility after aging heat treatment.
Background Art
[0002] A precipitation hardening type stainless steel is used for a steel belt, press plate,
or the like, because strength thereof can be increased by performing aging heat treatment.
As an example, SUS630, SUS631, or the like, may be mentioned.
[0003] The above SUS631 is a semi-austenitic stainless steel, and it is a metastable austenitic
stainless steel under a solid solution condition.
[0004] After a deformation-induced martensite structure is formed by performing cold rolling
on this steel, NiAl is precipitated by aging heat treatment so as to strengthen it;
however, there is a problem in that productivity is not satisfactory. Furthermore,
there is also a problem in that a δ ferrite phase is easily precipitated under high
temperatures because Al is contained, and hot processing workability is not satisfactory.
[0005] The above SUS630 is a martensitic stainless steel, and has a martensite structure
after solution heat treatment. It is strengthened by precipitation of ε-Cu phase by
aging heat treatment; however, achievable strength is about 1500 MPa (Vickers hardness
about 400).
Summary of Invention
[0007] Precipitation hardening martensite stainless steels, stronger than those disclosed
in the techniques of the above Patent documents, are widely used. However, as purposes
of use for the precipitation hardening martensite stainless steels increased, demands
associated with the purpose of use increased, and there may be a case in which properties
are not sufficient, depending on conditions for use.
[0008] Therefore, an object of the present invention is to provide a precipitation hardening
martensite stainless steel in which even greater strength and toughness can be maintained
by performing aging heat treatment.
[0009] In order to solve the above problem, the inventors have researched focusing on a
strengthened phase which is precipitated by alloy elements and aging heat treatment.
In order to study effects by each of the elements, various components were solved
by an experimental laboratory level, hot forged, and cold rolled so as to prepare
a cold rolled material having a plate thickness of 2 mm. With respect to this material,
solution heat treatment and aging heat treatment were performed, and then, mechanical
properties were evaluated by tension test, Vickers hardness test, and the like, and
a nanoscale precipitation hardening phase was evaluated by observing by a transmission
electron microscope (TEM) and a scanning transmission electron microscope (STEM).
[0010] In particular, the observation was performed carefully and in detail by STEM having
high resolution, and the precipitation phase was measured by EDS, and the following
information was obtained. It became obvious that X in the G phase (Ni
16X
6Si
7) precipitated by aging heat treatment can be substituted by Fe, Mn, or Nb, in addition
to Ti.
[0011] In particular, it was obvious that Ti was confirmed to be an element forming a skeleton
of a G phase, and Mn was solid-solved at an X-site in a case in which Nb was not added.
However, in this case, particle diameter of a G phase was large, being 4 to 20 nm,
and at the same time, a Cu phase was also large, being 4 to 50 nm, and there was a
tendency for the G phase and Cu phase to be distributed unevenly at a grain boundary,
and as a result, precipitation hardening was not improved.
[0012] On the other hand, in a material in which Nb was added, it was obvious that Nb, instead
of Mn, was solid-solved at the X-site. In addition, it was clear that precipitation
of a precipitation hardening phase such as a G phase and a Cu phase was promoted,
high strength could be obtained by shorter aging heat treatment time compared to the
case in which Nb was not added, and the precipitation hardening phase such as a G
phase and a Cu phase was fined, having a particle diameter of 1 to 20 nm. Furthermore,
it was obvious that these G phase and Cu phase were not distributed unevenly at grain
boundaries, and were dispersed finely in crystalline grains and grain boundaries.
It was clear that precipitation hardening was extremely improved by these fine precipitation
effects.
[0013] That is, the present invention is as follows:
An aspect of the present invention is a precipitation hardening martensite stainless
steel including: in mass%, indicated by "%", C: 0.01 to 0.05%, Si: 1.0 to 2.0%, Mn:
0.70 to 1.50%, P: not more than 0.04%, S: not more than 0.01%, Ni: 6.0 to 8.0%, Cr:
12.0 to 15.0%, Mo: 0.50 to 1.50%, Cu: 0.40 to 1.20%, Ti: 0.20 to 0.50%, Nb: 0.05 to
0.40%, N: 0.001 to 0.005%, Al: 0.001 to 0.2%, O: 0.0001 to 0.01%, with the remainder
being inevitable impurities and Fe, in which Cu phase and Ni
16(Ti, Nb)
6Si
7 type intermetallic compounds phase are distributed, and Nb in the intermetallic compounds
phase is 0.2 to 3.0 (at%).
[0014] In addition, in precipitation hardening, distribution condition and size of precipitation
hardening phase may greatly affect strength. Therefore, another aspect of the precipitation
hardening martensite stainless steel of the present invention is that not less than
50 number% of the Cu phase and the Ni
16(Ti, Nb)
6Si
7type intermetallic compounds phase is distributed in crystal grains, when a thin layer
sample is prepared using a focused ion beam, an element mapping image is obtained
by EDS by using an energy dispersive X-ray analyzer installed in a scanning transmission
electron microscope (STEM), and the image is image-analyzed by observing and evaluating
precipitation hardening phase at the nanoscale so as to obtain the distribution.
[0015] Another aspect of the precipitation hardening martensite stainless steel of the present
invention is that average diameter of the Cu phase and the Ni
16(Ti, Nb)
6Si
7 type intermetallic compounds phase is 1 to 20 nm.
[0016] Furthermore, another aspect of the present invention is that elongation is 2 to 15%
and hardness is 400 to 600 Hv as a mechanical property.
Brief Description of Drawings
[0017] Fig. 1 is a conceptual diagram showing precipitation conditions of a Cu phase and
a G phase in the stainless steel of the present invention, and showing neighbors at
the grain boundary of three crystal grains.
Embodiments of the Invention
[0018] Reasons for limitations on chemical composition of the stainless steel of the present
invention are explained. It should be noted that hereinafter "%" means "mass%" unless
particularly noted.
C: 0.01 to 0.10%
[0019] C is austenite forming element, and reduces generation of δ ferrite phase at high
temperatures. Furthermore, it solid-solves in a martensite phase so as to increase
strength; however, a residual austenite phase may easily be increased after solution
heat treatment, and sufficient strength may not be obtained after aging heat treatment.
Furthermore, in a case in which C amount is large, Ti and Nb, which are constituent
components of the G phase contributing to precipitation hardening, may be easily consumed
by formation of TiC and NbC. Therefore, in order to reduce precipitation hardening
ability by aging heat treatment, the content of C is set to be 0.01 to 0.10%. Furthermore,
it is desirably set to be 0.03 to 0.05%.
Si: 1.0 to 2.0%
[0020] Since a G phase is generated by aging heat treatment and strength is greatly increased
by precipitation hardening, Si is set to be not less than 1.0%. On the other hand,
content amount of Si is set to be not more than 2.0% since Si is a ferrite generating
element, δ ferrite phase may be easily generated by a large content amount of Si,
and hot workability and strength around a welded portion may be decreased. Furthermore,
it is desirably set to be 1.30 to 1.90%.
Mn: 0.50 to 1.50%
[0021] Since Mn is an austenite forming element, generation of δ ferrite phase at high temperatures
is restrained. Furthermore, residual austenite phase may be easily increased after
solution heat treatment, and toughness may be increased; but on the other hand, strength
may be decreased after aging heat treatment. Furthermore, MnO and MnS are formed so
that corrosion resistance is decreased. Therefore, the range of Mn is set to be 0.50
to 1.50%. Furthermore, it is desirably set to be 0.70 to 1.20%.
P: Not more than 0.04%
[0022] P is segregated at a crystal grain boundary so that solidification crack susceptibility
is increased and hot workability is decreased. Therefore, content amount of P is desirably
as small as possible, and it is set to be not more than 0.04%.
S: Not more than 0.01%
[0023] S is a harmful component since MnS is formed so that corrosion resistance is decreased
and since S segregates at a grain boundary so that hot workability is decreased. Therefore,
content amount of S is desirably as small as possible, and it is set to be not more
than 0.01%.
Ni: 6.0 to 8.0%
[0024] Ni is set to be not less than 6.0% since it is an austenite forming element, a constituent
element of the G phase, and an important element for precipitation hardening. However,
it is set to be not more than 8.0% since a residual austenite phase after solution
heat treatment may be easily increased, and strength may be decreased if content amount
of Ni is too high.
Cr: 12.0 to 15.0%
[0025] Content amount of Cr is set to be not less than 12.0% in order to maintain corrosion
resistance of the stainless steel. However, it is set to be not more than 15.0% since
it is a ferrite forming element, δ ferrite phase may be easily generated at high temperatures,
and hot workability may be decreased.
Mo: 0.50 to 1.50%
[0026] Mo is an element effective for increasing corrosion resistance; however, it may promote
generation of δ ferrite phase. Therefore, content amount of Mo is set to be 0.50 to
1.50%. Furthermore, it is desirably set to be 0.50 to 1.00%.
Cu: 0.40 to 1.20%
[0027] Cu is an element effective for precipitation hardening since a Cu phase is generated
by aging heat treatment. However, excess addition may cause deterioration of strength
by increasing residual austenite phase and cause generation of cracks by decrease
of hot workability. Therefore, content amount of Cu is set to be 0.40 to 1.20%. Furthermore,
it is desirably set to be 0.50 to 1.00%.
Ti: 0.20 to 0.50%
[0028] Ti is a necessary element for formation of a G phase and is an element effective
for increasing strength by precipitation hardening. However, since it may easily form
oxides and nitrides and may cause defects, the range of Ti content is set to be 0.20
to 0.50%.
Nb: 0.05 to 0.40%
[0029] Nb is a constituent element for a G phase, and it is a very important element. Nb
is an effective element since it has actions for controlling the G phase to be Ni
16(Ti, Nb)
6Si
7 type and for promoting generation of nucleus. Furthermore, it also has an effect
of dispersing Cu phase finely, and ability for precipitation hardening by a Cu phase
and a G phase is extremely improved. Furthermore, although it is not limited in particular,
it is also effective for fining crystal grains since it has an effect of inhibiting
coarsening of crystal grains by forming Nb carbides having sizes of about 0.3 to 1
µm. Therefore, the content amount of Nb is set to be not less than 0.05%. However,
it is set to be not more than 0.40% since excessive addition of Nb causes formation
of excess NbC, decreasing solid-solved C amount, and decreasing elongation. Furthermore,
it is desirably set to be 0.10 to 0.30%.
N: 0.001 to 0.005%
[0030] N is an austenite generating element similar to C, and it solid-solves in a martensite
phase so as to increase strength. However, Ti and Nb, which are constituent elements
of a G phase, contributing to precipitation hardening, may be easily consumed by forming
TiN and NbN, and precipitation hardening ability by aging heat treatment is decreased.
Therefore, the range of N is set to be 0.001 to 0.02%.
Al: 0.001 to 0.2%
[0031] Al is an effective deoxidizing agent element for decreasing amount of O. Furthermore,
since Nb is an element which is relatively easily oxidized, by decreasing oxygen concentration
by deoxidizing by Al, Nb can be reliably controlled in a range of the present invention.
However, in a case in which an excessive amount is contained, generation of δ ferrite
phase is promoted and hot workability and toughness are decreased. Therefore, the
range of Al is set to be 0.001 to 0.2%.
O: 0.0001 to 0.01%
[0032] Since O forms non-metallic inclusions by combining with Si and Ti, which are constituent
elements of a G phase, contributing to precipitation hardening, strength after aging
heat treatment is decreased. Furthermore, the oxide type inclusions may decrease cleanliness
level of steel and cause defects. However, since excess deoxidizing may increase cost,
the range of O is set to be from 0.0001 to 0.01%.
[0033] The steel of the present invention is a precipitation hardening type martensite stainless
steel having superior strength, which is realized by precipitating simultaneously
a Cu phase and G phase Ni
16X
6Si
7. Distribution conditions of these precipitation hardening phases and size of the
precipitation hardening phase itself have a large effect on mechanical properties
such as hardness and elongation.
[0034] For example, in a case in which precipitations exist more at a crystal grain boundary
and less inside a crystal grain, the precipitations may easily grow to be coarse and
brittle. On the other hand, strength is increased in a case in which precipitations
are distributed uniformly regardless of whether it is inside a crystal grain or at
a crystal grain boundary. Therefore, precipitations are uniformly dispersed by solution
heat treatment and aging heat treatment under appropriate conditions. The appropriate
heating treatment conditions here means, although not limited thereto in particular,
performing solution heat treatment at 1000 to 1150 °C for 1 to 5 minutes, and then
performing aging heat treatment at 400 to 600 °C for 30 minutes to 10 hours.
[0035] It should be noted that there is an optimal value of ratio of Nb in the G phase.
That is, in a case in which Nb content is too low, distribution of the G phase becomes
uneven and the G phase is distributed more at crystal grain boundaries, so that hardness
required in the present invention is not satisfied. On the other hand, in a case in
which Nb content is too high, elongation may be less than 2%, which is the lower limit
value of the range of the present invention, and the alloy does not elongate sufficiently,
so that the alloy cannot be processed. In a case in which content of Nb is set to
be x in Ni
16(Ti, Nb)
6Si
7, the G phase is described as Ni
16(Ti(
1-x), Nb
x)
6Si
7. Therefore, ratio of Nb atom (at%) in the G phase can be described as x/(16+6+7).
Although not limited in particular, hardness, and elongation can be controlled within
the present invention by setting Nb (at%) in the G phase 0.2 to 3.0. To realize this
range, content amount of Nb is set to be 0.05 to 0.40%.
[0036] In addition, in the steel of the present invention, by adding Nb, generation of nucleus
of the precipitation phase can be promoted, and precipitations can be dispersed uniformly.
Therefore, by setting Nb within the range of the present invention, it is possible
that not less than 50% of Cu phase and Ni
16(Ti, Nb)
6Si
7 type intermetallic compound phase are distributed inside crystal grains.
[0037] Furthermore, since sizes of these precipitation hardening phases themselves have
great effect on strength, the value is very important in the present invention. Even
if rearrangement progresses, strength can be maintained high as long as precipitations
can stop the rearrangement.
[0038] This action of precipitations as a blockade varies depending on size of precipitation
phase, and there is an optimal size of the precipitation phase. In the steel of the
present invention, since precipitation phase of a size of 1 nm to 20 nm has maximal
action of precipitation phase as a blockade against rearrangement, it is necessary
to optimize the size of the precipitation phase. Therefore, by performing solution
heat treatment and aging heat treatment under appropriate conditions, and by setting
Nb within the range of the present invention, it is possible for the average particle
diameter of a Cu phase and Ni
16(Ti, Nb)
6Si
7 type intermetallic compound phase to be 1 to 20 nm.
[0039] Since strength of precipitation hardening type stainless steel can be increased by
performing aging heat treatment, it is used for a steel belt or a press plate. These
require strength and fatigue properties, and hardness of HV 400 or more is necessary
to increase these properties. On the other hand, since elongation is reduced if it
has very high hardness, hardness is set to be not more than HV 600. In addition, since
toughness is required, elongation is set to be 2 to 15 % in view of balance with hardness.
Examples
[0040] Next, structure, action, and effect of the present invention are explained with reference
to Examples; however, the present invention is not limited only to the following Examples.
[0041] Table 1 shows chemical compositions, existence of precipitation hardening phase,
Nb amount in G phase, ratio of precipitations inside of a grain, Vickers hardness,
and elongation of each of sample materials. A bracketed value of a chemical composition
is outside the range of the present invention. In addition, Examples 2 and 5 are Reference
Examples.
Table 1
Section |
Steel No. |
Chemical composition mass% |
Exis tence of Cu phase |
Exis tence of G phase |
Evalua tion |
Nb in G phase (at%) |
Evalua tion |
Ratio of precipita tion inside of grain (%) |
Evalua tion |
Average particle diameter of precipita tion phase (nm) |
Evalua tion |
Hard ness Hv (10kg Load) |
Evalua tion |
Elonga tion (%) |
Evalua tion |
Overall Evalua tion |
C |
Si |
Mn |
P |
S |
| Ni |
Cr |
Mo |
Cu |
Ti |
Nb |
N |
Al |
O |
Examples |
1 |
0.042 |
1.45 |
0.72 |
0.003 |
0.0009 |
6.14 |
12.8 |
1.32 |
0.62 |
0.22 |
0.14 |
0.005 |
0.022 |
0,0044 |
Y |
Y |
Superior |
0.2 |
Superior |
77 |
Superior |
10.8 |
Superior |
488 |
Superior |
9.6 |
Superior |
A |
 2 |
0.042 |
1.78 |
(0.51) |
0.003 |
0.0006 |
6.92 |
14.6 |
0.65 |
0.83 |
0.30 |
0.18 |
0.003 |
0.017 |
0,0052 |
Y |
Y |
Superior |
0.3 |
Superior |
86 |
Superior |
3.6 |
Superior |
502 |
Superior |
8.6 |
Superior |
A |
3 |
0.042 |
1.28 |
0.99 |
0.003 |
0.0008 |
7.86 |
12.5 |
0.74 |
0.76 |
0,27 |
0.06 |
0.003 |
0.032 |
0.0005 |
Y |
Y |
Superior |
0.2 |
Superior |
66 |
Superior |
9.8 |
Superior |
399 |
Inferior |
10.1 |
Superior |
B |
4 |
0.043 |
1.97 |
1.42 |
0.007 |
0.0008 |
7.52 |
13.7 |
1.33 |
0.44 |
0,49 |
0.26 |
0.005 |
0.020 |
0,0050 |
Y |
Y |
Superior |
0.5 |
Superior |
52 |
Superior |
24.2 |
Inferior |
443 |
Superior |
3.8 |
Superior |
B |
 5 |
0.043 |
1,83 |
(0.63) |
0.004 |
0.0008 |
6.91 |
14.2 |
0.92 |
0.83 |
0,29 |
0.39 |
0.002 |
0.019 |
0,0049 |
Y |
Y |
Superior |
2.8 |
Superior |
49 |
Inferior |
3.3 |
Superior |
537 |
Superior |
1.9 |
Inferior |
B |
Compara tve Examples |
6 |
0.044 |
1.11 |
1.29 |
0.003 |
0.0008 |
(9.51) |
13.8 |
0.75 |
(1.62) |
0.21 |
(0.01) |
0.003 |
0.023 |
0.0047 |
Y |
Y |
Superior |
0.1 |
Inferior |
20 |
Inferior |
23.2 |
Inferior |
323 |
Inferior |
14.8 |
Superior |
C |
7 |
0.043 |
1.92 |
(0.27) |
0.004 |
0.0008 |
6.93 |
13.2 |
0.85 |
0.66 |
(0.03) |
0.26 |
0.002 |
0.019 |
0.0041 |
Y |
N |
Inferior |
- |
Inferior |
62 |
Superior |
25.6 |
Inferior |
378 |
Inferior |
11.2 |
Superior |
C |
8 |
0.041 |
1.73 |
1.23 |
0.004 |
0.0008 |
6.91 |
13.8 |
0.74 |
(0.05) |
0.48 |
0.39 |
0.005 |
0.018 |
0,0053 |
N |
Y |
Inferior |
2.1 |
Superior |
78 |
Superior |
15.8 |
Superior |
383 |
Inferior |
17.5 |
Inferior |
C |
9 |
0.042 |
1.79 |
(0.38) |
0.004 |
0.0008 |
7.98 |
13.7 |
0.51 |
0.82 |
(0,96) |
(0.83) |
(0.006) |
0.019 |
0,0043 |
Y |
Y |
Superior |
8.5 |
Inferior |
40 |
Inferior |
24.5 |
Superior |
620 |
Inferior |
1.6 |
Inferior |
C |
10 |
0.042 |
(0.23) |
(2.31) |
0.004 |
0.0008 |
6.94 |
12.3 |
0.83 |
0.75 |
0.26 |
(0.03) |
(0.006) |
0.012 |
0.0062 |
Y |
Y |
Superior |
0.1 |
Inferior |
35 |
Inferior |
4.6 |
Superior |
280 |
Inferior |
32.2 |
Inferior |
C |
[0042] To prepare each of the steels, raw materials were melted in a high-frequency induction
furnace, and the melt was casted in a cast-iron mold so as to prepare an ingot of
about 20 kg. The ingot was hot-forged at 1000 to 1200 °C so as to obtain a forged
plate having a thickness of 12 mm. Then, the forged plate was cold-rolled to obtain
cold rolled material having a thickness of 2 mm, and solution heat treatment and aging
heat treatment were performed with respect to this. The solution heat treatment was
performed to solid-solve precipitations existing in a steel, and martensite transformation
may occur by rapid cooling after the heat treatment. With respect to the cold-rolled
material above, solution heat treatment was performed at 1050 °C for 2 minutes.
[0043] The aging heat treatment is a treatment in which precipitation hardening phase, that
is a Cu phase and a G phase in the steel of the present invention, is finely dispersed
and precipitated after the solution heat treatment. With respect to the cold-rolled
material above, aging heat treatment was performed at 480 °C for 1 hour.
[0044] Evaluation of mechanical properties such as a tensile test and a Vickers hardness
test, evaluation of structure by an optical microscope and an SEM, and evaluation
of nanoscale precipitation hardening phase by TEM and STEM observation of these sample
materials were performed.
[0045] Existence, distribution, and size of Cu phase and G phase, which are the precipitation
hardening phases, were measured by preparing a thin film sample using a focused ion
beam (FIB), obtaining an element mapping image by energy dispersive X-ray spectroscopy
(EDS) installed in a STEM, and analyzing the image.
[0046] Hereinafter, bases for evaluation of each evaluation item shown in Table 1 are explained.
Existence of Cu phase and G phase
[0047] In a case in which both a Cu phase and a G phase exist (both "Yes" in Table 1), evaluation
was "Superior". In a case in which one of the phases does not exist (one "No" in Table
1), evaluation was "Inferior". As a basis for deciding whether each phase exists or
not, observing a freely selected view, a case in which precipitations are not less
than 0.001 (pieces/nm
2) was regarded as the phase of "existing".
Nb (at%) in G phase
[0048] Nb (at%) in the G phase Ni
16(Ti, Nb)
6Si
7 can be described as x/(16+6+7), in a case of Ni
16(Ti(
1-x), Nb
x)
6Si
7. This Nb amount in a G phase during aging heat treatment was calculated by using
a thermodynamic calculating software (trade name: Thermo-Calc). Furthermore, Nb amount
in a G phase obtained by this thermodynamic calculation matches well with the result
of STEM-EDS analysis. In view of mechanical properties such as hardness and elongation,
Nb (at%) in G phase being 0.2 to 3.0 was evaluated as "Superior".
Ratio of precipitations inside of grains (%)
[0049] Ratio of precipitations inside of grains being not less than 50% was evaluated as
"Superior".
Average particle diameter of precipitation phase (nm)
[0050] Average particle diameter of a precipitation phase being 1 to 20 nm was evaluated
as "Superior".
Hardness Hv (10 kg load)
[0051] In the Vickers hardness test, heat treatment was performed on the above cold-rolled
material with thickness of 2 mm, the rolled surface was polished by #800, five points
were measured with a 10 kg load with respect to the surface, and average value thereof
was calculated. Hardness being 400 to 600 Hv was evaluated as "Superior".
Elongation (%)
[0052] In the tensile test, heat treatment was performed on the above cold-rolled material
of thickness of 2 mm, a flat type tensile test piece, defined by JIS (Japanese Industrial
Standards) No. 13B, in which tensile direction matches rolled direction, is cut out,
and measurement was performed. From the measurement results, elongation being 2 to
15% was evaluated as "Superior".
Overall evaluation
[0053] In view of the above results, overall evaluation was "A" in a case in which all of
the evaluations were "Superior", overall evaluation was "B" in a case in which one
or two instances of "Inferior" were included, and overall evaluation was "C" in a
case in which not less than three instances of "Inferior" were included. The overall
evaluation was "A" or "B" in Examples; in contrast, the overall evaluation was "C"
in Comparative Examples.
[0054] In Comparative Example 6, the Nb amount was low, and the ratio of precipitations
inside of grains was low. Furthermore, residual γ amount could easily be greater since
Ni amount and Cu amount were high, and hardness was low.
[0055] Comparative Example 7 is out of the range of the present invention and hardness was
low since Ti amount was low and no G phase existed.
[0056] In Comparative Example 8, although a G phase existed, no Cu phase existed, and hardness
and elongation were low since the Cu amount was low.
[0057] In Comparative Example 9, although a Cu phase and a G phase existed, elongation was
low since Ti and Nb amounts were high.
[0058] In Comparative Example 10, residual γ amount was extremely high, similar to the case
of Comparative Example 6, since the Mn amount was high. Furthermore, Nb in the G phase
was low since Nb amount was low, and hardness was low and elongation was high since
ratio of precipitations inside of grains was low.
[0059] As explained so far, mechanical properties of both of, or of one of, hardness and
elongation, were inferior in Comparative Examples compared to in Examples.