Aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability

Abstract

An aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability and a method of fabricating the same. The aluminum alloy piping material comprises an aluminum alloy which comprises 0.3-1.5% of Mn, 0.01-0.20% of Fe, and 0.01-0.20% of Si, wherein the content of Cu as impurities is limited to 0.05% or less, with the balance consisting of Al and impurities, wherein, among Si compounds, Fe compounds, and Mn compounds present in the alloy matrix, the number of compounds with a particle diameter (equivalent circle diameter, hereinafter the same) of 0.5 μm or more is 3×104 or less per mm2. The aluminum alloy piping material has a tensile strength of 70-130 MPa (temper: O material). An ingot of an aluminum alloy having the composition is hot extruded. The resulting extruded pipe is cold drawn at a working ratio of 30% or more and annealed.

Description

BACKGROUND OF THE INVENTION

[0001] 1. Field of the Invention

[0002] The present invention relates to an aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, which is used for pipes connecting automotive radiators and heaters or pipes connecting automotive evaporators, condensers, and compressors, and to a method of fabricating the same.

[0003] 2. Description of Background Art

[0004] As a piping material used for passages connecting automotive heaters, evaporators, condensers, or compressors, a single pipe consisting of an Al-Mn alloy such as a JIS 3003 alloy (Japanese Patent Application Laid-open No. 63-24133), and a two-layered or three-layered clad pipe consisting of 3003 alloy as a core material and an Al-Zn alloy sacrificial anode material such as a 7072 alloy clad on either the inner side or outer side of the core material (Japanese Patent Application Laid-open No. 56-127767) have been used. The sacrificial anode material exhibits an sacrificial anode effect on pitting corrosion occurring in the core material under a severe environment or crevice corrosion occurring when connected to a rubber hose.

[0005] However, when the Al-Mn alloy single pipe is used under severe corrosive environment, pitting corrosion tends to occur. Occurrence of pitting corrosion can be prevented by using the clad pipe. However, this significantly increases costs. When these piping materials are connected to radiators, heaters, evaporators, condensers, compressors, and the like, the pipe ends of the piping materials are caused to bulge. However, the Al-Mn alloy single pipe exhibits inferior workability, whereby working may become difficult.

SUMMARY OF THE INVENTION

[0006] The present invention has been achieved as a result of examination of the relation between the structural properties of the Al-Mn alloy single pipe, such as the alloy components and the compound distribution in the alloy matrix, and properties required for automotive piping materials. Accordingly, an object of the present invention is to provide an aluminum alloy piping material for automotive piping made of an Al-Mn alloy single pipe which excels in corrosion resistance and workability and is produced at low cost.

[0007] (1) In order to achieve the above object, the present invention provides an aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, comprising an aluminum alloy which comprises 0.3-1.5% of Mn, 0.01-0.20% of Fe, and 0.01-0.20% of Si, wherein the content of Cu as impurities is limited to 0.05% or less, with the balance consisting of Al and impurities, wherein, among Si compounds, Fe compounds, and Mn compounds present in the alloy matrix, the number of compounds with a particle diameter (equivalent circle diameter, hereinafter the same) of 0.5 μm or more is 3×104 or less per mm2.

[0008] (2) In this aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, the aluminum alloy may further comprise 0.4% or less of Mg.

[0009] (3) In the above aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, the aluminum alloy may further comprise 0.01-0.2% of Zr.

[0010] (4) In the above aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, the aluminum alloy piping material refined into an O material has a tensile strength of 70-130 MPa.

[0011] (5) A method of fabricating an aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, comprising hot extruding an ingot of an aluminum alloy having a composition according to any one the above (1) to (3), cold drawing the resulting extruded pipe at a working ratio of 30% or more, and annealing the cold drawn pipe, wherein the aluminum alloy piping material after being refined into an O material has a tensile strength of 70-130 MPa.

[0012] (6) In this method of fabricating an aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, the cooling rate when casting the ingot is 10° C./second or more.

DETAILED DESCRIPTION OF THE INVENTION AND PREFERRED EMBODIMENTS

[0013] (1) The effects of alloy components and reasons for the limitations thereof, (2) the effects of compounds in the matrix and reasons for the limitations thereof, and (3) the effects of fabrication steps and reasons for the limitations thereof in the present invention are described below.

[0014] (1) Effects of Alloy Components and Reasons for Limitations

[0015] Mn increases the strength and improves corrosion resistance (pitting corrosion resistance). The Mn content is preferably 0.3-1.5%. If the Mn content is less than 0.3%, the effect may be insufficient. If the Mn content exceeds 1.5%, a large number of Mn compound particles may be formed, whereby the corrosion resistance may decrease.

[0016] Fe decreases the grain size after drawing and annealing. If the grain size is large, surface roughening or cracks tend to occur during bending or bulge formation of the piping material. The Fe content is preferably 0.01-0.20%. If the Fe content is less than 0.01%, the effect may be insufficient. If the Fe content exceeds 0.20%, a large number of Fe compound particles may be formed, whereby the corrosion resistance may decrease. The Fe content is still more preferably 0.01-0.10%.

[0017] Si decreases the grain size after drawing and annealing, thereby preventing the occurrence of surface roughening or cracks during bending or bulge formation. Moreover, Si forms Al-Mn-Si compounds and Al-Mn-Fe-Si compounds, thereby preventing the occurrence of penetration between tools and the material during bending or bulge formation. The Si content is preferably 0.01-0.20%. If the Si content is less than 0.01%, the effect maybe insufficient. If the Si content exceeds 0.20%, a large number of Si compound particles may be formed, whereby the corrosion resistance may decrease. The Si content is still more preferably 0.01-0.10%.

[0018] Cu is dissolved under corrosive environment and decreases the corrosion resistance by readhering to the surface by reduction. If the Cu content exceeds 0.05%, corrosion resistance significantly decreases due to readhesion under repeated humidity-salt spray conditions. The Cu content is still more preferably 0.02% or less.

[0019] Mg increases the strength of the piping material and decreases the grain size. The Mg content is preferably 0.4% or less. If the Mg content exceeds 0.4%, extrusion capability and corrosion resistance may decrease. The Mg content is still more preferably 0.2% or less.

[0020] Zr is separately distributed in a high-concentration area and a low-concentration area along the extrusion direction. These areas are alternately layered in the direction of the thickness. The low-concentration area is preferentially corroded rather than the high-concentration area, thereby forming corrosion layers. This prevents the corrosion from proceeding in the direction of the thickness, thereby improving pitting corrosion resistance and crevice corrosion resistance of the material. The Zr content is preferably 0.01-0.2%. If the Zr content is less than 0.01%, the effect may be insufficient. If the Zr content exceeds 0.2%, giant compounds are produced during casting, whereby a sound piping material cannot be obtained.

[0021] (2) Effects of Compounds in Matrix and Reasons for Limitations

[0022] The aluminum alloy piping material of the present invention comprises an aluminum alloy which comprises the above components, wherein, among Si compounds, Fe compounds, and Mn compounds present in the alloy matrix, the number of compounds with a particle diameter (equivalent circle diameter) of 0.5 μm or more is 3×104 or less per mm2. Such a compound distribution prevents the occurrence of microgalvanic corrosion between the compound particles and the matrix, thereby improving the corrosion resistance. Moreover, workability is improved due to increased elongation. The distribution of compounds with a particle diameter of 0.5 μm or more is still more preferably 1×104 or less per mm2.

[0023] The aluminum alloy piping material of the present invention is refined into an O material having a tensile strength of 70-130 MPa, which is a strength suitable as an automotive piping material. Moreover, the aluminum alloy piping material is provided with improved elongation and workability, thereby enabling easy bulge formation at the pipe ends.

[0024] (3) Effects of Production Steps and Reasons for Limitations

[0025] The aluminum alloy piping material of the present invention is produced as follows. A billet of the aluminum alloy having the above composition is cast by continuous casting at a cooling rate of preferably 10° C./sec. or more. The billet is hot extruded after homogenization or without performing homogenization to prepare an aluminum alloy extruded pipe. The resulting extruded pipe is cold drawn at a working ratio ({(cross section before working—cross section after working)/(cross section before working)}×100%) of 30% or more, and then annealed. The aluminum alloy is refined into an O material by this step to obtain an aluminum alloy piping material having a tensile strength of 70-130 MPa. If the drawing working ratio is less than 30%, the grain size after annealing is increased, whereby surface roughening or cracks tend to occur during bending or bulge formation.

EXAMPLES

[0026] The present invention is described below by examples and comparative examples to demonstrate the effects of the present invention. These examples illustrate only one of the embodiments of the present invention, which should not be construed as limiting the present invention.

Example 1

[0027] Billets (diameter: 90 mm) of aluminum alloys (alloys A-O) having a composition shown in Table 1 were cast by continuous casting. The casting temperature was 700-740° C. and the cooling rate was 10° C./sec. or 20° C./sec. as shown in Table 2.

[0028] The resulting billets were homogenized at a temperature of 600° C. or more and hot extruded to form extruded pipes with an outer diameter of 25 mm and an inner diameter of 20 mm. The extruded pipes were cold drawn into the dimensions shown in Table 2, and then annealed at a temperature of 500° C. for one hour to obtain test materials. The drawing working ratio is shown in Table 2.

[0029] The resulting test materials were subjected to a tensile test to measure the tensile strength and elongation. The average grain diameter at the outer surface of the test materials was measured. A test material of which the average grain diameter of less than 200 μm was judged as “Good”. The diameter and the number of compound particles in the matrix, bulge formation capability, and corrosion resistance were evaluated according to the following methods. The measurement and evaluation results are shown in Table 3.

[0030] Measurement of Diameter and Number of Compounds:

[0031] The total number of compounds with a particle diameter (equivalent circle diameter) of 0.5 μm or more within five fields of optical microstructure images (magnification: ×800, total area: 0.2 mm2) was measured using an image analyzer.

[0032] Bulge Formation Capability:

[0033] After forming bulges in the test materials, the presence or absence of surface roughening was observed. In the case where no surface roughening was observed, bulge formation capability of the test material was judged as “Good”. In the case where surface roughening was observed, bulge formation capability of the test material was judged “Bad”.

[0034] Corrosion Resistance:

[0035] The outer surface of the test material was subjected to a repeated salt spray-humidity test (SWAAT: ASTMG85-A3) for six weeks. The maximum depth of pitting corrosion occurring at the outer surface of the test material was measured. A test material with a maximum corrosion depth of less than 0.8 mm was judged as having good corrosion resistance.

TABLE 1
	Composition (mass %)
Alloy	Si	Fe	Mn	Cu	Mg	Zr
A	0.10	0.10	0.80	0.01	0.00	—
B	0.05	0.10	1.00	0.00	0.00	—
C	0.05	0.10	0.30	0.00	0.00	—
D	0.05	0.10	1.50	0.01	0.00	—
E	0.05	0.10	1.00	0.05	0.00	—
F	0.05	0.02	1.00	0.01	0.00	—
G	0.05	0.18	1.00	0.01	0.00	—
H	0.02	0.10	1.00	0.01	0.00	—
I	0.18	0.10	1.00	0.01	0.00	—
J	0.05	0.10	1.00	0.01	0.38	—
K	0.05	0.10	1.00	0.02	0.00	—
L	0.05	0.10	1.00	0.01	0.19	—
M	0.05	0.10	1.00	0.01	0.00	0.03
N	0.05	0.10	1.00	0.01	0.00	0.18
O	0.05	0.10	1.00	0.01	0.00	—

[0036]

TABLE 2
		Extrusion dimension	Drawing dimension
Test		(outer diameter ×)	(outer diameter ×	Drawing working	Casting cooling rate
Material	Alloy	inner diameter (mm))	inner diameter (mm))	ratio (%)	(° C./s)
1	A	25 × 20	17 × 15	71.6	10
2	B	25 × 20	17 × 15	71.6	10
3	C	25 × 20	17 × 15	71.6	10
4	D	25 × 20	17 × 15	71.6	10
5	E	25 × 20	17 × 15	71.6	10
6	F	25 × 20	17 × 15	71.6	10
7	G	25 × 20	17 × 15	71.6	10
8	H	25 × 20	17 × 15	71.6	10
9	I	25 × 20	17 × 15	71.6	10
10	J	25 × 20	17 × 15	71.6	10
11	K	25 × 20	17 × 15	71.6	10
12	L	25 × 20	17 × 15	71.6	10
13	M	25 × 20	17 × 15	71.6	10
14	N	25 × 20	17 × 15	71.6	10
15	O	25 × 20	20 × 16	36	10
16	O	25 × 20	8 × 6	87.6	10
17	O	25 × 20	17 × 15	71.6	20

[0037]

TABLE 3
					Number of
					compounds
					with		Corrosion
				Average	particle		resistance
				crystal	diameter of		(maximum
		Tensile		particle	0.5 μm or	Bulge	corrosion
Test		strength	Elongation	size	more	formation	depth)
Material	Alloy	(MPa)	(%)	(μm)	(per mm2)	capability	(mm)
1	A	100	40	80	13000	Good	0.42
2	B	105	40	80	10000	Good	0.33
3	C	78	48	80	9000	Good	0.30
4	D	115	38	80	20000	Good	0.40
5	E	107	40	80	9000	Good	0.69
6	F	95	42	130	6000	Good	0.35
7	G	105	40	60	23000	Good	0.65
8	H	95	42	85	9000	Good	0.34
9	I	105	40	75	18000	Good	0.51
10	J	125	40	80	10000	Good	0.38
11	K	100	40	75	10000	Good	0.49
12	L	113	41	80	10000	Good	0.40
13	M	100	40	90	10000	Good	0.40
14	N	105	40	100	12000	Good	0.53
15	O	105	40	90	10000	Good	0.39
16	O	105	40	80	11000	Good	0.42
17	O	95	42	90	8000	Good	0.30

[0038] As shown in Table 3, the test materials according to the present invention showed a tensile strength of 70-130 MPa and produced no surface roughening during bulge formation or bending due to the grain size of less than 200 μm. The number of compounds with a particle diameter of 0.5 μm or more distributed in the matrix was 30,000/mm2. These test materials exhibited good corrosion resistance with a maximum corrosion depth of less than 0.8 mm. It was confirmed that no cracks or surface roughening occurs during bulge formation or bending of the piping material for automobiles if the grain size is less than 200 μm. It was also confirmed that a piping material with a maximum corrosion depth of less than 0.8 mm does not cause problems in corrosion resistance to occur when used as a piping material for automobiles.

Comparative Example 1

[0039] Billets (diameter: 90 mm) of aluminum alloys (alloys a-k) having a composition shown in Table 4 were cast by continuous casting. The casting temperature was 700-740° C. and the cooling rate was 10° C./sec. or 0.5° C./sec. as shown in Table 5.

[0040] The resulting billets were homogenized at a temperature of 600° C. or more in the same manner as in Example 1 and hot extruded to form extruded pipes with a diameter shown in Table 5. The extruded pipes were cold drawn into an outer diameter of 17 mm and an inner diameter of 15 mm, and then annealed at a temperature of 500° C. for one hour to obtain test materials. The drawing working ratio is shown in Table 5.

[0041] The resulting test materials were subjected to a tensile test in the same manner as in Example 1 to measure the tensile strength and elongation. The average grain diameter at the outer surface of the test materials was measured. A test material of which the average grain diameter is less than 200 μm was judged as “Good”. The diameter and the number of compound particles in the matrix, bulge formation capability, and corrosion resistance were evaluated according to the same methods as in Example 1. The measurement and evaluation results are shown in Table 6.

TABLE 4
	Composition (mass %)
Alloy	Si	Fe	Mn	Cu	Mg	Zr
a	0.05	0.10	0.20	0.00	0.00	—
b	0.05	0.10	1.60	0.00	0.00	—
c	0.05	0.10	1.00	0.08	0.00	—
d	0.05	0.00	1.00	0.01	0.00	—
e	0.05	0.40	1.00	0.00	0.00	—
f	0.00	0.10	1.00	0.00	0.00	—
g	0.40	0.10	1.00	0.00	0.00	—
h	0.05	0.10	1.00	0.00	0.60	—
i	0.05	0.10	1.00	0.00	0.00	0.40
j	0.25	0.45	1.20	0.15	0.00	—
k	0.05	0.10	1.00	0.00	0.00	—

[0042]

TABLE 5
		Extrusion dimension	Drawing dimension
Test		(outer diameter ×)	(outer diameter ×	Drawing working	Casting cooling rate
Material	Alloy	inner diameter (mm))	inner diameter (mm))	ratio (%)	(° C./s)
18	a	25 × 20	17 × 15	71.6	10
19	b	25 × 20	17 × 15	71.6	10
20	c	25 × 20	17 × 15	71.6	10
21	d	25 × 20	17 × 15	71.6	10
22	e	25 × 20	17 × 15	71.6	10
22	f	25 × 20	17 × 15	71.6	10
24	g	25 × 20	17 × 15	71.6	10
25	h	25 × 20	17 × 15	71.6	10
26	i	25 × 20	17 × 15	71.6	10
27	j	25 × 20	17 × 15	71.6	10
28	k	18 × 16	17 × 15	5.9	10
29	k	25 × 20	17 × 15	71.6	0.5

[0043]

TABLE 6
					Number of
					compounds
					with		Corrosion
				Average	particle		resistance
				crystal	diameter of		(maximum
		Tensile		grain	0.5 μm or	Bulge	corrosion
Test		strength	Elongation	size	more	formation	depth)
Material	Alloy	(MPa)	(%)	(μm)	(per mm2)	capability	(mm)
18	a	68	50	80	9000	Good	0.33
19	b	120	35	80	33000	Good	0.90
20	c	110	38	80	10000	Good	Perforation
21	d	90	42	300	5000	Bad	0.33
22	e	105	40	50	40000	Good	0.93
23	f	90	45	230	7000	Bad	0.35
24	g	110	38	60	31000	Good	0.86
25	h	—	—	—	—	—	—
26	i	—	—	—	—	—	—
27	j	115	35	50	40000	Good	Perforation
28	k	105	40	400	10000	Bad	0.30
29	k	110	38	60	60000	Good	Perforation

[0044] As shown in Table 6, test material No. 18 exhibited insufficient strength due to low Mn content. Test material No. 19 exhibited inferior corrosion resistance since a large number of Mn compounds was formed due to high Mn content. Test material No. 20 exhibited inferior corrosion resistance due to high Cu content of more than 0.05%, in which perforation (maximum corrosion depth >0.1 mm) occurred. In test material No. 21, the average grain diameter was increased due to low Fe content, thereby resulting in inferior bulge formation capability. In test material No. 22, a large number of Fe compounds was formed due to high Fe content, thereby resulting in inferior corrosion resistance.

[0045] In test material No. 23, the average grain diameter was increased due to low Si content, thereby resulting in inferior bulge formation capability. In test material No. 24, a large number of Al-Mn-Si compounds and Al-Mn-Fe-Si compounds was formed due to high Si content, thereby resulting in inferior corrosion resistance. Test materials Nos. 25 and 26 exhibited insufficient extrusion capability due to high Mg content and high Zr content, respectively, whereby a sound test material could not be obtained.

[0046] Test material No. 27 consisting of a conventional 3003 alloy exhibited inferior corrosion resistance due to a large number of compound particles present therein, in which perforation occurred. Test material No. 28 exhibited inferior bulge formation capability because the average grain diameter was increased after annealing due to a small drawing working ratio. Test material No. 29 exhibited inferior corrosion resistance because of a large number of compound particles present therein due to a low cooling rate during casting, in which perforation were formed.

[0047] As described above, the present invention provides an aluminum alloy piping material for automotive piping made of an Al-Mn alloy single pipe which excels in corrosion resistance and workability and is produced at low cost. This piping material is suitably used as a piping material connecting automotive radiators and heaters or as a piping material connecting evaporators, condensers, and compressors.

[0048] Obviously, numerous modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described herein.

Claims

1. An aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, comprising an aluminum alloy which comprises 0.3-1.5% (mass %, hereinafter the same) of Mn, 0.01-0.20% of Fe, and 0.01-0.20% of Si, wherein the content of Cu as impurities is limited to 0.05% or less, with the balance consisting of Al and impurities, wherein, among Si compounds, Fe compounds, and Mn compounds present in the alloy matrix, the number of compounds with a particle diameter (equivalent circle diameter, hereinafter the same) of 0.5 μm or more is 3×104 or less per mm2.

2. The aluminum alloy piping material for automotive piping excelling in corrosion resistance and formability according to claim 1, wherein the aluminum alloy further comprises 0.4% or less of Mg.

3. The aluminum alloy piping material for automotive piping excelling in corrosion resistance and formability according to claim 1 or 2, wherein the aluminum alloy further comprises 0.01-0.2% of Zr.

4. The aluminum alloy piping material for automotive piping excelling in corrosion resistance and formability according to any one of claims 1 to 3, wherein the aluminum alloy piping material refined into an O material has a tensile strength of 70-130 MPa.

5. A method of fabricating an aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability, comprising hot extruding an ingot of an aluminum alloy having the composition according to any one the above (1) to (3), cold drawing the resulting extruded pipe at a working ratio of 30% or more, and annealing the cold drawn pipe, wherein the aluminum alloy piping material refined into an O material has a tensile strength of 70-130 MPa.

6. The method of fabricating an aluminum alloy piping material for automotive piping excelling in corrosion resistance and workability according to claim 5, wherein the cooling rate when casting the ingot is 10° C./sec. or more.