Hoffman D.M., Singh B., Thomas J.H. (Eds). Handbook of Vacuum Science and Technology
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522
Chapter 4.8: Aluminum-Based Vacuum Systems
Table 2
Comparative Characteristics and Applications of Selected Aluminum Alloys
ALLOY AND TEMPER
1060-0
H2
H14
K16
H18
1100-0
H12
H4
H16
H18
1350-0
H12.
Hill
HI4.
H24
HI6,
H26
H18
2011-T3
T4.
T451
T8
2014-0
T3.
T4.
T451
T6.T651,T6510.T6511
2017-T4. T451
2018-T61
2024-0
T4.
T3. T351.T3510. T3511
T361
T6
T861.
T81.
T851.
T8510. T8511
T72
2025-T6
2036-14
2117-T4
2124-T851
2218-T61
T72
2219-0
T31.T351,T3510. T3511
T37
T81.T851.T8510.T8511
T87
2618-T61
3003-0
H12
H14
H16
H18
H2S
3004-0
H32
H34
H36
H38
3105-0
H12
H14
H16
H18
H25
4032-T6
5005-0
H12
H14
H16
Hie
RESISTANCE
ro
CORROSION
0
S
1
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
00)
D®
D
DO)
0
DO)
bb
DO)
D
D
D
C
C
D
0
D
DO)
D(D
D
D
0
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
0
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
D
D
B
C
C
C
C
C
B
B
C
A
B
0
C
0
C
B
B
C
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
B
A
A
A
A
A
1®
It
A
A
A
B
B
A
A
A
B
0
A
A
A
B
B
C
B
D
0
D
C
C
D
C
D
B
B
D
C
D
D
D
A
A
B
C
C
B
A
B
B
C
0
A
B
B
0
0
B
A
A
B
C
C
1
t
E
E
D
D
D
E
E
0
D
0
E
E
0
D
D
A
A
A
D
B
B
B
B
D
B
B
B
B
B
B
C
C
B
B
B
B
B
B
B
E
E
D
D
D
D
D
D
C
0
C
E
E
D
D
D
D
B
E
E
D
D
D
@
1
1
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
D
D
D
0
D
D
D
D
D
D
D
0
D
D
D
0
0
D
D
0
D
D
D
0
0
D
A
A
A
A
A
A
B
B
B
B
B
A
A
A
A
A
A
0
B
B
B
B
B
WELOABIUTYCD
3
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
D
D
D
D
D
D
D
0
D
0
D
D
D
D
D
C
0
0
D
0
D
A
A
A
A
D
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
D
A
A
A
A
A
1
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
D
D
D
0
B
B
B
C
D
B
C
C
c
C
B
B
B
0
G
C
A
A
A
A
A
C
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
B
A
A
A
A
A
h
• • c
11^
B
A
A
A
A
B
A
A
A
A
B
A
A
A
A
D
0
D
B
B
B
B
B
D
B
B
B
B
B
B
B
B
B
B
B
B
A
A
A
A
B
B
A
A
A
A
A
B
A
A
A
A
B
A
A
A
A
A
C
B
A
A
A
A
SOME
APPLICATIONS OF
ALLOYS
Chemical equipment, railroad tank cars
Sheet metal work, spun hollowware, fin
stock
Electrical conductors
Screw machine products
Truck frames, aircraft structures
Screw machine products, fittings
Aircraft engine cylinders, heads and
pistons
Truck wheels, screw machine products.
aircraft structures
Forgings, aircraft propellers
Auto t)ody panel sheet
Rivets
Aircraft structures
Jet engine impellers and rings
Structural uses at high temperatures
(to eOO-F)
High strength weklnrtents
Aircraft engines
Cooking untensils, chemical equipment.
pressure vessels, sheet metal work.
txjiMer's hardware, storage tanks
Sheet metal work, storage tanks
Resklential skiing, mobile homes, rain
carrying goods, sheet metal work
Pistons
Appliances, utensils, architectural,
electrical conductor
(continues)
4.8.4 Mechanical Considerations
523
Table 2—Continued
ALLOY AND TEMPER
5005-0
H32
H34
H36
H38
5050-0
H32
H34
H36
H38
5052-0
H32
H34
H36
H38
5056-0
Hill
H12.
H32
HI
4.
H34
HI8.
H38
HI 92
H392
5083-0
H321.H116
Hill
5086-0
H32.
H116
H34
H36
H38
Hill
5154-0
H32
H34
H36
H38
5252-H24
H25
H28
5254-0
H32
H34
H36
H38
5454-0
H32
H34
H111
5456-0
H321.H116
5457-0
5652-0
H32
H34
H36
H38
5657-H241
H25
H26
H28
600S-T1.T5
6053-0
T6.
T61
RESISTANCE
TO
CORROSION
e
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A®
A®
A®
A®
A®
B®
B®
A®
A®
A®
A®
A®
A®
A®
A®
A®
A®
A®
A®
A®
A®
A
A
A
A®
A®
A®
A®
A®
A
A
A
A
A®
A®
A
A
A
A
A
A
A
A
A
A
A
5
o
Sou
A
A
A
A
A
A
A
A
A
A
A
A
A
A
B®
B®
B®
B®
C®
D®
D®
A®
A®
B®
A®
A®
B®
B®
B®
A®
A®
A®
A®
A®
A®
A
A
A
A®
A®
A®
A®
A®
A
A
A
A
B®
B®
A
A
A
A
A
A
A
A
A
A
A
h
A
B
c
c
A
A
B
i
C
C
A
B
B
C
C
A
A
B
B
C
D
D
B
C
C
A
B
B
C
C
B
A
B
B
0
C
B
B
C
A
B
B
C
C
A
B
B
B
B
C
A
A
B
B
0
0
A
B
B
C
©
1
c
1
E
0
D
D
E
D
1
0
c
1
c
D
D
c
c
c
D
D
D
C
C
B
B
D
D
0
D
D
C
C
C
0
D
0
C
C
C
D
C
C
D
0
0
C
C
D
D
C
D
D
D
E
D
0
C
C
C
D
0
D
D
E
C
1
1
1
B
B
B
B
B
B
B
B
B
C
G
C
C
C
0
D
D
D
0
D
D
D
D
0
D
D
D
D
D
0
D
D
0
0
0
C
C
C
D
D
D
0
0
D
0
D
0
0
0
B
C
C
0
C
C
B
B
B
B
A
B
B
WELOABIUTY®
J
A
A
A
A
A
A
A
A
A
A
A
A
A-
A
C
C
c
c
c
c
c
0
c
c
c
c
c
c
c
c
c
c
c
c
c
A
A
A
C
C
C
c
c
c
c
0
c
0
c
A
A
A
A
A
A
A
A
A
A
A
A
A
1
A
A
A
A
A
A
A
1
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
ll
IIJ!
A
A
A
A
B
A
A
A
A
B
A
A
A
A
B
A
A
A
A
A
A
B
A
A
B
A
A
A
A
A
B
A
A
A
A
A
A
A
B
A
A
A
A
B
A
A
A
B
A
B
B
A
A
A
A
A
A
A
A
A
B
1
A
SOME
APPLICATIONS OF
ALLOYS
Builder's hardware, refrigerator
trim,
coiled tubes
Sheet metal work, hydraulic tube.
appiiarK:es
Cable sheathing, rivets
for
magrwsium,
screen wire, zipper
Unfired,
welded pressure vessles,
marine, auto aircraft cryogenics,
TV
towers, drilling rigs, transportation
equipment, missile components
Welded structures, storage tanks.
pressure vessels, salt water service
Automotive and appliance trim
Hydrogen peroxkle and chemk^l
storage vessels
WMded structures, pressure vessels.
marine service
High strength wekled structures,
pressure vessels, marine applications,
storage tanks
Hydrogen peroxide and chemtoal
storage vessels
Anodized auto and appliance
trim'
1
Wire and rod
for
rivets
(continues)
524
Chapter
4.8:
Aluminum-Based Vacuum Systems
Table 2—Continued
ALLOY AND TEMPER
6061-0
T4.
T451.T4510. T4511
T6. T651,
T652. T6510. T6511
6063-T1
T4
T5.
T52
T6
T83,
T831.T832
6066-0
T4,T4510,T4511
T6.
T6510. T6511
6070-T4. T4511
T6
6101-T6. T63
T61.T64
6151-T6. T652
6201-TBI
6262-T6.
T651.
T6510. T6511
T9
6351-T1
-T4
-T5
-T6
6463-T1
-T5
•T6
6951-T42. T62
7005-T53
7049-T73. T7352
7050-T73510. T73511
T74®. T7451(2). T74510<2).
T74511(2). T7452®.
T7651.
T76510.T76511
7075-0
T6. T651.
T652. T6510.
T6511,
T73.
T7351
7175-T74. T7452. T7454
7178-0
T6.
T651,T6510. T6511
7475-0
7475-T61.-T651
7475-T761.T735t
8017-H12. H22. H221
8030-H12, H221
8176-H14. H24
8177-H13, H23. H221
RESISTANCE
TO
CORROSION
S
B
B
B
A
A
A
A
A
C
C
C
B
B
A
A
A
B
B
A
A
A
A
A
A
C
C
CO)
C
C
C(D
C
c
A
A
A
A
J"
lii!
A
B
A
A
A
A
A
A
A
B
B
B
B
A
A
A
A
A
A
A
A
B
B
C
B
B
C
c
B
A
A
A
A
i
If
A
B
C
B
B
B
C
C
B
C
C
B
C
C
B
C
D
C
C
C
C
B
B
C
0
0
D
0
0
D
b
D
A
A
A
A
j
0
C
0
D
0
C
C
C
D
C
B
C
C
C
0
C
B
B
C
C
C
C
D
0
C
B
B
D
B
B
B
B
B
B
0
E
D
E
1
1
A
A
A
A
A
A
A
A
D
D
D
0
0
A
A
B
A
B
B
C
C
C
C
A
A
A
A
B
D
D
D
D
D
0
0
0
D
D
D
A
A
A
A
WEL0ABILITY(3)
s
A
A
A
A
A
A
A
A
0
D
D
A
A
A
A
A
B
B
B
B
B
B
A
A
A
A
C
D
D
D
D
D
D
0
0
D
D
D
A
A
A
A__
1
A
A
A
A
A
A
A
A
B
B
B
A
A
A
A
A
B
B
A
A
A
A
A
A
A
A
A
D
D
D
0
D
C
D
D
0
B
D
A
A
A
A
III
B
A
A
A
A
A
A
A
B
B
B
A
A
A
A
A
A
A
B
B
A
A
A
A
A
A
A
B
B
B
B
B
B
B
B
B
B
B
A
A
A
A
SOME
APPLICATIONS OF
ALLOYS
Heavy-duty structures requiring good
corrosion resistance, truck and marine,
railroad cars, furniture, pipelines
Pipe railing, furniture, architectural
extrusions
Forgings and extrusion for welded
structures
Heavy duty welded structures, pipelines
High strength txis conductors
Moderate strenght, intricate forgings for
machine and auto parts
High strength electric conductor wire
Screw machine products
Extruded shapes, structurals, pipe and
tube
Extruded architectural and trim
sections
Aircraft forgings
Aircraft and other structures
Aircraft and other structures
Aircraft and other structures
Shell Casings
Aircraft & Other
Structures
Electrical conductors
Electrical conductors
Electrical conductors
Electrical conductors
Source:
Aluminum Association,
Aluminum
Standards and Data, Tenth Edition, 900 19th St., N.W.,
Washington, D.C., 1990, p. 51, Table 3.3.
4.8.4 Mechanical Considerations
525
Table 3
Typical Mechanical Properties of Aluminum Alloys
ALLOY
AND L
TEMPER
1060-0
1060-H12
1060-H14
1060-H16
1060-H18 1
1100-0
1100-H12
1100-H14
1100-H16
1100-H18
2014-0
2014-T4. T451
2014-T6. T651
2024-0
2024-T3
2024-T4. T351
2024-T361®
2219^
2219-T42
2219-T31,
T351
2219-T37
2219-T62
2219-T81.T851
2219-TB7
3003-0
3003-H12
3003-H14
30C3-H16
3003-H18
5063-0
5083-H321.
H116
5086-0
5086-H32.H116
50e6-H34
5086-H112
5154-0
5154-H32
5154.H34
5154-H36
5154-H38
5154-H112
5456^
5456-H112
54S6-H321.
H116
6061-0
6061-T4. T451
6061-T6. T651
6063-0
6063-T1
6063-T4
6063-T5
6063-T6
6063-T83
6063-T831
6063-T832
TENSION 1"
STRENGTH 1
ksl
ULTIMATE
10
12
14
16
19
13
16
18
21
24
27 1
62
70 '
27
70
68
72
25 1
52
52
57
60
66
60
16
19
22
26
29
42
46
36
42
47
39
35
39
42
45
48
1 35
45
45
51
18
35
1 ^
13
22
25
27
35
37
30
42
YIELD
4
11
13
15
18
5
15
17 1
20
22
14
42
60
11
50
47
57
11
27
36
46
42
51
57
6
18
21
25
27
21
33
17
30
37
19
17
1 30
33
36
39
1
^7
23
24
37
8
21
1 ^
7
13
13
21
31
35
27
39
ELONGATION |
ptcmn
1/16
In.
1
Thick
Sp*clfn«n 1
43
16
12
8
6
35
12
9
6
5
20
18
20
13
18
20
17
11
10
10
10
30
10
8
5
4
22
12
10
1 14
27
IS
13
12
10
25
25
22
1
^2
20
22
12
12
9
10
12
In 2
In.
1
1/2
In.
1
Dtametar
Sp*clm*n 1
45
25
20
17
15
18
20
13
22
19
40
20
16
14
10 J
22
16
24
22
1
••*
1
30
25
1 ^^
HARDNESSH
BRINELL
NUMBER
500 kg load
10 mm tMll
19
23
26
30
35
23
28
32
38
44
45
105
135
47
120
120
130
28
35
40
47
55
58
67
73
78
80
63
90
30
65
95
25
42
60
73
82
70
95
SHEAR
ULTIMATE
SHEARING
STRENGTH
ksl
7
8 1
9
10
11
9
10
11
12
13
18
38
42
18
41
41
42
11
12
14
15
16
25
23
27
22
22
24
26
28
30
12
24
30
~lio
14
17
22
22
27
FATIGUE 1
ENDUR-
ANCECD
UMH-
k*i
3
4
5
6.5
6.5
5
6 1
7
9 ,
9
13
20
18
13
20
20
18
15
15
15
7
8
9
10
10
23
17
18
19
20
21
17
9
14
1 '''*
1
®
9
10
10
MODULUS
MODULUS0
OF
ELASTICITY
ksl
x10»
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.6
10.0
10.0
10.0
10.0
10.0
10.3
10.3
10.3
10.3
10.3
10.3
10.2
10.2
10.2
10.2
j 10.2
10.2
10.3
10.3
10.3
10.0
10.0
1 10.0
1 10.0
10.0
10.0
100
10.0
10.0
10.0
10.0
Source: Aluminum Association, Aluminum Standards and Data, Tenth Edition, 900 19th St., N.W.,
Washington, D.C., 1990, p. 30, Table 2.1.
Note: The above values are for comparison purposes only. Actual characteristics vary. To convert
ksi values in the table to Kgf/mm^, multiply by 0.7045.
526
Chapter
4.8:
Aluminum-Based Vacuum Systems
Table
4
Typical Tensile Properties
at
Various
Temperatures'
ALLOY
AND
TEMPER
1100-0
1100-H14
1100-H18
2011-T3
2014-T6, T651
2017-T4.T451
TEMP.
•F
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
75
212
300
400
500
600
700
-320
-112
18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
TENSILE
STRENGTH,
kai
ULTIMATE
25
15
14
13
10
8
6
4
2.9
2.1
30
20
19
18
16
14
10
4
2.9
2.1
34
26
25
24
21
18
6
4
2.9
2.1
55
47
28
16
6.5
3.1
2.3
84
74
72
70
63
40
16
9.5
6.5
4.3
80
65
64
62
57
40
16
YIELD®
6
5.5
5
5
4.6
4.2
3.5
2.6
•>
.6
20
18
17
17
15
12
7.5
2.6
2
1.6
26
23
23
22
19
14
3.5
2.6
2
1.6
43
34
19
11
3.8
1.8
1.4
72
65
62
60
57
35
13
7.5
5
3.5
53
42
41
40
39
30
13
ELON-
GATION
IN 2
IN.,
PERCENT
50
43
40
40
45
55
65
75
80
85
45
24
20
20
20
23
26
75
80
85
30
16
15
15
15
20
65
75
80
85
15
16
25
35
45
90
125
14
13
13
13
15
20
38
52
65
72
28
24
23
22
18
15
35
ALLOY
AND
TEMPER
2024-13
(sheet)
2024-T4.T351
(plate)
2024-T6. T651
2024-T81.T851
2024-T861
TEMP.
T
500~
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
TENSILE
STRENGTH,
Iwl
ULTIMATE
9
6
4.3
85
73
72
70
66
55
27
11
7.5
5
84
71
69
68
63
45
26
11
7.5
5
84
72
70
69
65
45
26
11
7.5
5
85
74
73
70
66
55
27
11
7.5
5
92
81
78
75
70
54
21
11
7.5
5
YIELO<Z>
T^i
5
3.5
62
52
51
50
48
45
20
9
6
4
61
49
47
47
45
36
19
9
6
4
68
59
58
57
54
36
19
9
6
4
78
69
68
65
62
49
20
9
6
4
85
77
74
71
67
48
17
9
6
4
ELON-
GATION
IN 2
IN.,
PERCENT
45
65
70
18
17
17
17
16
11
23
55
75
100
19
19
19
19
19
17
27
55
75
100
11
10
10
10
10
17
27
55
75
100
8
7
7
7
8
11
23
55
75
100
5
5
5
5
6
11
28
55
75
100
(continues)
4.8.4
Mechanical Considerations
527
Table
4—Continued
ALLOY
AND
TEMPER
2117-T4
2124-T851
2218-T61
2219-T62
2219-T81,T8551
2618-T61
TEMR
•F
-320
-112
-
18
75
212
300
400
500
600
700
-452
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
TENSILE
STRENGTH,
toi
ULTIMATE
56
45
44
43
36
30
16
7.5
4.7
2.9
102
86
76
73
70
66
54
27
11
7.5
5.5
72
61
59
59
56
41
22
10
5.5
4
73
63
60
58
54
45
34
27
10
4.4
83
71
69
66
60
49
36
29
7
4.4
78
67
64
YIELD®
33
25
24
24
21
17
12
5.5
3.3
2
90
79
71
68
64
61
49
20
8
6
4.1
52
45
44
44
42
35
16
6
3
2.5
49
44
42
40
37
33
25
20
6
3.7
61
54
52
50
47
40
29
23
6
3.7
61
55
54
ELON-
GATION
IN 2
IN.,
PERCENT
30
29
28
27
16
20
35
55
80
110
10
9
8
8
9
9
13
28
60
75
100
15
14
13
13
15
17
30
70
85
100
16
13
12
12
14
17
20
21
40
75
15
13
12
12
15
17
20
21
55
75
12
11
10
ALLOY
AND
TEMPER
3003-0
3003-H14
3003-H18
3004-0
3004-H34
TEMR
•F
75~
212
300
400
500
600
700
-320
-112
-18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
500
600
700
-320
-112
-
18
75
212
300
400
TENSILE
STRENGTH,
toi
ULTIMATE
64
62
50
32
13
7.5
5
33
20
17
16
13
11
8.5
6
4
2.8
35
24
22
22
21
18
14
7.5
4
2.8
41
32
30
29
26
23
14
7.5
4
2.8
42
28
26
26
26
22
14
10
7.5
5
52
38
36
35
34
28
21
YIELD®
54
54
44
26
9
4.5
3.5
8.5
7
6.5
6
5.5
5
4.3
3.4
2.4
1.8
25
22
21
21
19
16
9
4
2.4
1.8
33
29
28
27
21
16
9
4
2.4
1.8
13
11
10
10
10
10
9.5
7.5
5
3
34
30
29
29
29
25
15
ELON-
GATION
IN 2
IN..
PERCENT
10
10
14
24
50
80
120
46
42
41
40
43
47
60
65
70
70
30
18
16
16
16
16
20
60
70
70
23
11
10
10
10
11
18
60
70
70
38
30
26
25
25
35
55
70
80
90
26
16
13
12
13
22
35
(continues)
528
Chapter
4.8:
Aluminum-Based Vacuum Systems
Table
4--Continued
ALLOY
AND
TEMPER
TENSILE
STRENGTH,
ksi
500
600
700
-320
-112
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
14
7.5
56
55
50
37
6
3.9
28
28
34
32
32
7.5
5
43
38
36
7.5
5
3
46
46
8
8
8
7.5
6
4.2
2.6
30
25
24
24
24
22
7.5
6
4.2
2.6
36
30
29
29
29
25
7.5
6
4.2
2.6
ELON-
GATION
IN 2 IN.,
PERCENT
55
20
10
7
30
50
80
90
10
9
9
70
90
ALLOY
AND l
TEMPER
1
5052-0
5052-H34
5052-H38
5083-0
5086-0
5154-0
TEMR
•F
T
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700 '
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
TENSILE
STRENGTH, \
K»l
1
ULTIMATE
44
29
28 !
28 1
28
23
17
12
7.5
5
55
40
38
38
38
30
24
12
7.5
5
60
44
42
42
40
34
25
12
7.5
5
59
43
42
42
40
31
22
17
11
6
55
39
38
38
38
29
22
17
11
6
52
36
35
YIELD®
I
16
13
13
13
13
13
^1
7.5
5.5
3.1
36
32
31
31
31
27
15
7.5
5.5
3.1 '
44
38
37
37
36
28
15
7.5
5.5
3.1
24
21
21
21
21
19
17
11
7.5
4.2
19
17
17
17
17
16
15
11
7.5
4.2
19
17
17
ELON-
GATION
IN 2
IN.,
PERCENT
46
35
32
30
36
50
60
80
110
130
28
21
18
16
18
27
45
80
110
130
25
18
15
14
16
24
45
60
110
130
36
30
27
25
36
50
60
80
110
130
46
35
32
30
36
50
60
80
110
130
46
35
32
{continues)
4.8.4
Mechanical Considerations
529
Table 4—Continued
ALLOY
AND
TEMPER
5254-0
5454-0
5454-H32
5454-H34
5456-0
TEMP.
•F
75~
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
TENSILE
STRENGTH,
tol
ULTIMATE
ii
35
29
22
17
11
6
52
36
35
35
35
29
22
17
11
6
54
37
36
36
36
29
22
17
11
6
59
42
41
40
39
32
25
17
11
6
63
46
44
44
43
34
26
17
11
6
62
46
45
45
42
31
22
17
11
6
YIELD(2)
17
17
16
15
11
7.5
4.2
19
17
17
17
17
16
15
11
7.5
4.2
19
17
17
17
17
16
15
11
7.5
4.2
36
31
30
30
29
26
19
11
7.5
4.2
41
36
35
35
34
28
19
11
7.5
4.2
26
23
23
23
22
20
17
11
7.5
4.2
ELON-
GATION
IN 2
IN..
PERCENT
30
36
50
60
80
110
130
46
35
32
30
36
50
60
80
110
130
39
30
27
25
31
50
60
80
10
30
32
23
20
18
20
37
45
80
110
130
30
21
18
16
18
32
45
80
110
130
32
25
22
20
31
50
60
80
110
130
ALLOY
AND
TEMPER
5652-0
5652-H34
5652-H38
6053-T6. T651
6061-T6,T651
6063-T1
TEMR
•F
-320
-112
- 18
75
212
300
400
500
600
700
320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
TENSILE
STRENGTH.
k8i
ULTIMATE
44
29
28
28
28
23
17
12
7.5
5
55
40
38
38
38
30
24
12
7.5
5
60
44
42
42
40
34
25
12
7.5
5
37
32
25
13
5.5
4
2.9
60
49
47
45
42
34
19
7.5
4.6
3
34
26
24
22
22
21
9
4.5
3.2
2.3
YIELD®
16
13
13
13
13
13
11
7.5
5.5
3.1
36
32
31
31
31
27
15
7.5
5.5
3.1
44
38
37
37
36
28
15
7.5
5.6
3.1
32
28
24
12
4
2.7
2
47
42
41
40
38
31
15
5
2.7
1.8
16
15
14
13
14
15
6.5
3.5
2.5
2
ELON-
GATION
IN 2
IN.,
PERCENT
46
35
32
30
30
50
60
80
110
130
28
21
18
16
18
27
45
80
110
130
25
18
15
14
16
24
45
80
110
130
13
13
13
25
70
80
90
22
18
17
17
18
20
28
60
85
95
44
36
34
33
18
20
40
75
80
105
{continues)
530
Chapter 4.8: Aluminum-Based
Vacuum
Systems
Table 4—Continued
ALLOY
AND
TEMPER
6063-T5
6063-T6
6101-T6
6151'T6
6262-T651
6262-Tg
7075-T6.
T651
TEMP.
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
•
75
1
212 1
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
1 212
TENSILE STRENGTH,
tol
ULTIMATE
37
29
28
27
24
20
9
4.5
3.2
2.3
47
38
36
35
31
21
9
4.5
3.3
2.3
43
36
34
32
28
21
10
4.8
3
2.5
57
50
49
48
43
28
14
6.5
5
4
60
49
47
45
42
34
74
62
60
58
53
38
15
8.5
4.6
3
102
90
66
83
70
YIELO®
24
22
22
21
20
18
6.5
3.5
2.5
2
36
33
32
31
28
20
6.5
3.5
2.5
2
33
30
29
28
25
19
7
3.3
2.3
1.8
50
46
45
43
40
27
12
5
3.9
3.2
47
42
41
40
38
31
67
58
56
55
52
37
13
; 6
2.7
1.8
92
79
75
73
1 65
ELON-
GATION
IN 2
IN..
PERCENT
28
24
23
22
18
20
40
75
80
105
24
20
19
18
15
20
40
75
80
105
24
20
19
19
20
20
40
80
100
105
20
17
17
17
17
20
30
50
43
35
22
18
17
17
18
20
14
10
10
10
10
14
34
48
1 85
95
9
11
11
11
14
ALLOY
AND
TEMPER
7075-T73.
T7351
7175-T74
7178-T6.T651
7178-176.
T7651
7475-T61 Sheet
7475-T761 Sheet
TEMR
T
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
212
300
400
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
-320
-112
- 18
75
212
300
400
500
600
700
TENSILE STRENGTH,
ksl
ULTIMATE
31
16
11
8
6
92
79
76
73
63
31
16
11
8
6
106
90
87
72
35
18
106
94
91
88
73
31
15
11
8.5
6.5
106
91
88
83
69
31
15
11
8.5
6.5
99
88
84
80
70
30
14
9.5
6.5
5
95
84
80
76
64
30
14
9.5
6.5
5
YIELIX2)
Z7
13
9
6.5
4.6
72
67
65
63
58
27
13
9
6.5
4.6
98
83
80
69
31
13
94
84
81
78
68
27
12
9
7
5.5
89
78
76
73
64
27
12
9
7
5.5
87
79
75
72
65
26
11
7
5.5
3.8
82
73
70
67
61
26
11
7
S.S
3.6
ELON-
GATION
IN 2
IN.,
PERCENT
30
55
65
70
70
14
14
13
13
15
30
55
65
70
70
13
14
16
17
30
65
5
8
9
11
14
40
70
76
80
80
10
10
10
11
17
40
70
76
80
80
10
12
12
12
14
28
55
70
80
85
11
12
12
12
14
36
55
70
80
85
Source:
Aluminum Association,
Aluminum
Standards and Data, Tenth Edition, 900 I9th St., N.W.,
Washington, D.C., 1990, p. 34, Table 2.2.
Note: The above values are for comparison purposes only. Actual characteristics vary. To convert
ksi values in the table to Kgf/mm^, multiply by 0.7045.
4.8.4 Mechanical Considerations
531
Table
5
Chemical Composition Limits
of
Wrought Aluminum Alloys
AA
DESIG-
NATION
1050
1060
1100
1145®
1175®
1200
1230®
1235
1345
1350®
2011
2014
2017
2018
2024
2025
2036
2117
2124
2218
2219
2319
2618
3003
3004
3005
3105
4032
4043
4045®
4047(2)
4145®
4343®
5005
5050
5052
5056
5083
5086
5154
5183
5252
5254
5356
5454
5456
5457
5554
5556
5652
5654
5657
SILICON
0.25
0.25
0.95 Si
0.55 Si
0.15 Si
1.00
Si
0.70 Si
0.65 Si
0.03
0.10
0.40
0.05-1.2
0.20-0.8
0.9
0.50
0.50-1.2
0.50
0.8
0.20
0.9
0.20
0.20
0.10-0.25
0.6
0.30
0.6
0.6
11.0-13.5
4.5-6.0
9.0-11.0
11.0-13.0
9.3-10.7
6.8-8.2
0.30
0.40
0.25
0.30
0.40
0.40
0.25
0.40
0.08
0.45 Si
0.25
0.25
0.25
0.08
0.25
0.25
0.40 Sj
0.45 Si
0.08
IRON
0.40
0.35
f
Fe
f
Fe
f
Fe
f
Fe
f
Fe
f
Fe
0.40
0.40
0.7
0.7
0.7
1.0
0.50
1.0
0.50
0.7
0.30
1.0
0.30
0.30
0.9-1.3
0.7
0.7
0.7
0.7
1.0
0.8
0.8
0.8
0.8
0.8
0.7
0.7
0.40
0.40
0.40
0.50
0.40
0.40
0.10
+
Fe
0.40
0.40
0.40
0.10
0.40
0.40
+
Fe
+
Fe
0.10
COPPER
0.05
0.05
0.05-0.20
0.05
0.10
0.05
0.10
0.05
0.10
0.05
5.0-6.0
3.9-5.0
3.5-4.5
3.5-4.5
3.8-4.9
3.9-5.0
2.2-3.0
2.2-3.0
3.8-4.9
3.5-4.5
5.8-6.8
5.8-6.8
1.9-2.7
0.05-0.20
0.25
0.30
0.30
0.50-1.3
0.30
0.30
0.30
3.3-4.7
0.25
0.20
0.20
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.05
0.10
0.10
0.10
0.20
0.10
0.10
0.04
0.05
0.10
MAN-
GANESE
0.05
0.03
0.05
0.05
0.02
0.05
0.05
0.05
0.05
0.01
0.40-1.2
0.40-1.0
0.20
0.30-0.9
0.40-1.2
0.10-0.40
0.20
0.30-0.9
0.20
0.20-0.40
0.20-0.40
1.0-1.5
1.0-1.5
1.0-1.5
0.30-0.6
0.05
0.05
0.15
0.15
0.10
0.20
0.10
0.10
0.05-0.20
0.40-1.0
0.20-0.7
0.10
0.50-1.0
0.10
0.01
0.05-0.20
0.50-1.0
0.50-1.0
0.15-0.45
0.50-1.0
0.50-1.0
0.01
0.01
0.03
MAG-
NESIUM
0.05
0.03
o!o5
0.02
0.05
0.05
0.05
0.20-0.8
0.40-0.8
0.45-0.9
1.2-1.8
0.05
0.30-0.6
0.20-0.50
1.2-1.8
1.2-1.8
0.02
0.02
1.3-1.8
0.8-1.3
0.20-0.6
0.20-0.8
0.8-1.3
0.05
0.05
0.10
0.15
0.50-1.1
1.1-1.8
2.2-2.8
4.5-5.6
4.0-4.9
3.5-4.5
3.1-3.9
4.3-5.2
2.2-2.8
3.1-3.9
4.5-5.5
2.4-3.0
4.7-5.5
0.8-1.2
2.4-3.0
4.7-5.5
2.2-2.8
3.1-3.9
0.6-1.0
CHROM-
IUM
0.01
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.10
0.20
0.10
o!l5
0.10
0.10
0.15-0.35
0.05-0.20
0.05-0.25
0.05-0.25
0.15-0.35
0.05-0.25
0.15-^).35
0.05-0.20
0.06-0.20
0.05-0.20
0.05-0.20
0.05-0.20
0.15-0.35
0.15-0.35
NICKEL
1.7-2.3
1.7-2.3
0.9-1.2
0.50-1.3
ZINC
0.05
0.05
0.10
0.05
0.04
0.10
0.10
0.10
0.05
.
0.05
0.30
0.25
0.25
0.25
0.25
0.25
0.25
0.25
0.25
0.25
0.10
0.10
0.10
0.10
0.25
0.25
0.40
0.25
0.10
0.10
0.20
0.20
0.20
0.25
0.25
0.10
0.10
0.25
0.25
0.20
0.25
0.05
0.20
0.10
0.25
0.25
0.05
0.25
0.25
0.10
0.20
0.05
TITAN-
lUM
o!o3
0.03
0.03
0.02
0.05
0.03
0.06
0.03
0.15
0.15
0.15
0.15
0.15
0.15
0.02-0.10
0.10-0.20
0.04-0.10
0.10
0.10
0.20
0.20
0.15
0.15
0.20
0.15
o!65
0.06-0.20
0.20
0.20
0.05-0.20
0.05-0.20
0.05-0.15
OTHERS®
Each®
0.03®
0.03®
0.05®
0.03®
0.02®
0.05
0.03®
0.03®
0.03®
0.03®
0.05®
0.05
0.05
0.05
0.05
0.05
0.05
0.05
0.05
0.05
0.05®
0.05®
0.05
0.05
0.05
0.05
0.05
0.05
0.05®
0.05
0.05®
0.05®
0.05
0.05
0.05
0.05
0.05
0.05
0.05
0.05
0.05®
0.03®
0.05
0.05®
0.05
0.05
0.03®
0.05®
0.05®
0.05
0.05®
0.02®
Total®
o!l5
0.15
0.10
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.15
0.10
0.15
0.15
0.15
0.15
0.10
0.15
0.15
0.15
0.15
0.05
ALUMI-
NUM
MIn.®
99.50
99.60
99.00
99.45
99.75
99.00
99.30
99.35
99.45
99.50
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
Remainder
For all numbered footnotes,:
(continues)