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TABLE 1—ALLOY, TEMPER AND PRODUCT FORM USED IN
AUTOMOTIVE APPLICATIONS
Application Alloy and Temper(1)Product Form Body Sheet, Panels
Body Panels2036-T4Sheet
2038-T4Sheet
5052-0, H32, H34Sheet
5182-0, O2(2)Sheet
6010-T4, T6Sheet
6111-T4, T6Sheet
Interior Panels, Components3004-0, H32Sheet
5052-0, H32, H34Sheet
5182-0, O2(2)Sheet
6009-T4, T62Sheet
Bumper Components(3)
Reinforcements6061-T4, T6Sheet, Extrusions
Face Bar, Reinforcements6009-T4, T6(4)Sheet
7021-T61(4)Sheet
7029-T5,T6 (5)(4)Sheet, Extrusions
7116-T5(4)Extrusions
7129-T6(4)Extrusions
Structural & Weldable5083-H111, H112, H116,
H321Sheet, Plate, Extrusions
5086-H32, H34, H111Sheet, Plate,
Extrusions, Tube
5182-0, O2(2)Sheet
请你告诉我5454-0, H32, H34, H111Sheet, Plate,
Extrusions, Tube
6009-T4, T62Sheet
6061-T4, T6, T651Sheet, Plate,
Extrusions, Forgings,
Structural Shapes,
Tube, Rod, Bar
General Purpo3003-H14, H24Sheet
3004-0, H32Sheet
5052-0, H32, H34Sheet
5454-0, H32, H34Sheet, Plate,
Extrusions, Tube
6061-T4, T6, T651Sheet, Plate,
Extrusions, Forgings,
Structural Shapes,
Tube, Rod, Bar
6463-T521(5)Extrusions
6063-T1, T5, T6Extrusions, T ube
Trim
Name Plates, Appliques1100-0Sheet
3002-0Sheet
5005-0Sheet
Strength Paramount5252-H2X(6)Sheet
5457-H3X(6)Sheet
Brightness Paramount 5657-H2X (6)Sheet Wheels (7), Fabricated 5454-0, H32, H34 H111, H112Sheet, Plate, Extrusions
Fasteners (Mechanical)
2017-T4Rivet and Cold Heading Wire and Rod
六个柠檬2024-T42117-T46053-T616061-T4
Heat Exchangers
A wide variety of alloys and tempers are currently specified or under consideration for heat-exchangers.
1.Only the commonly ud tempers are listed for the alloys shown. Other tempers of the alloys are available. For
典雅的近义词temper definitions, e SAE J1434.
2.Registered temper for a material which reduces incidence of stretcher strain.
3.Normally supplied with mill finish for bumper components if anodized or chrome plated finish is not required.
4.Suitable for bright dip and anodizing.
5.Suitable for chrome plating.
6. A wide variety of tempers are available to meet specific customer requirements. Normally a 2X temper is sup-plied.
7.Aluminum automotive wheels are also produced by the casting process.
TABLE 1—ALLOY, TEMPER AND PRODUCT FORM USED IN
AUTOMOTIVE APPLICATIONS (CONTINUED)
Application
Alloy and Temper (1)
Product Form
TABLE 2A—TYPICAL MECHANICAL PROPERTIES AND COMPARATIVE CHARACTERISTICS
Typical Mechanical Properties(1)(2)
Tension Shear Fatigue Modulus
Resistance to Corrosion
Strength Elonga-
tion Comparative Characteristics
Weldability(3)
Alloy
and Temper(4)Ulti-
mate
MPa
Yield
0.2%
Offt
MPa
percent
in
一个人面对
50 mm
(1.60
mm
Thick
Speci-
men)
Ulti-
mate
Shear
Strength
MPa
Endur-
ance
Limit
MPa
Modu-
lus(5)
of
Elas-
ticity
MPa
x 10°General(6)
Stress(7)
corro-
sion
Crack-
毕业鉴定表ing
Tough-
ness(8)
Worka-
bility(9)
cold
Macha-
bility(9)Gas Arc
Resis-
tance
spot
and
高高在上什么意思Seam
1100-0 90 3535 60 35(10)69A A A E A A B 2017-T4425275 20(11)260125(10)75D C C B N/A N/A N/A 2024-T447032520285140(10)73D C C B N/A N/A N/A
2036-T434019524205125(12)71C A2(13)A B C—B B 2038-T432517025205125(12)71C A2(13)B C—B B 2117-T4295165 24(11)195 95(10)71C A B C N/A N/A N/A
3002-0 95 4033 7069A A A E A A B 3003-H14,H24150145 8 95 60(10)69A A B D A A A 3004-0180 70
20110 95(10)69A A B A D B A B -H3221517010115105(10)69A A B D B A A
5005-0125 4025 7569A A A E A A B 5052-0195 9025125110(10)70A A A A D A A B -H3223019512140115(10)70A A B D A A A -H3426021510145125(10)70A A B B C A A A
5083-H321,H116315230 14(11)160(10)71A B C D C A A 5086-H322902051271A A B D C A A -H343252*********A B B C C A A -H1122701301471A A A D C A B
5182-027513021165140(12)71A-B A2(14)A D C A B -022*********A-B A2(14)A D C A B 5252-H252351701114569A A B C A A A
5454-02501152216070A A A A D C A B -H322752*********A A B D C A A -H343052*********A A B B C C A A
5457-H251801601211069A A A E A A B 5657-H2516014012 9569A A B D A A A 6009-T422012525150115(12)69B A2A A C A A A
6010-T429016524195125(12)69B A2A B C A A A 6053-T6169A A——C N/A N/A N/A :
6061-T424014522165 95(10)69B B A B C A A A -T6,T65131027512205 95(10)69B A B
C C A A A 6063-T1150 9020 95 60(10)69A A B
D A A A -T518514512115 70(10)69A A B C A A A -T624021512150
70(10)69A A C
C A A A 6111-T129016026 69
69B A2A B C A A B 6463-T5218514512115
69A A B
C
A
A
A
7021-T6143038013140(10)
71B A2(15)7029-T5,T643038015270
反应的70
B A2157116-T536031516B
A115C
7129-T6430
380
15
270
145(16)
70B
A215
1.
T ypical properties are not guaranteed since in most cas they are averages for various sizes, product forms, and methods of manufacture and may not be exactly reprentative of any particular product or size. The data are intended only as a basis for comparing alloys and tempers and should not be specified as engi-neering requirements or ud for design purpos.2.The indicated typical mechanical properties for all except the 0 temper material are higher than the specified minimum properties. For 0 temper products,
typical ultimate and yield values are slightly lower than specified (maximum) values.3.Ratings A through D for weldability are relative ratings as follows:
A —Generally weldable by all commercial procedures and methods.
B —Weldable with special techniques.
C —Limited weldability due to crack nsitivity, loss in corrosion resistance, loss in mechanical properties.
D —No commonly ud welding methods have been developed.
N/A—Rating not applicable for end u application requirements, that is, rivets.
4.Only the commonly ud tempers are listed for the alloys shown. Other tempers of the alloys are available.
5.Average of tension and compression modulii. Compression modulus is about 2% greater than tension modulus.
6.General corrosion ratings are bad on exposures to sodum chloride solution by intermittent spraying or immersion. Ratings A through D are relative ratings
in decreasing order of merit. The ratings do not necessarily imply acceptable performance in the intended application.
7.Stress-corrosion cracking ratings are badon rvice experience and on laboratory tests of specimens expod to the 35% sodum chloride alternate immer-sion test for 2XXX, 6XXX, and copper containing 7XXX ries alloys and total immersion in boiling sodum chloride solution for 96 h for copper free 7XXX ries alloys.
蛋蜜汁
A —No known instance of failure in rvice or in laboratory tests.
A2—Insufficient rvice experience; no known instance of failure in laboratory tests.B —No known instance of failure in rvice; limited failures in laboratory rvice.B2—Insufficient rvice experience; limited failures in laboratory rvice.
C —Service failures with sustained tension stress acting in short transver direction relative to grain structure; limited failures in laboratory tests of long transver specimens.
D —Limited rvice failures with sustained longitudinal or long transver stress.
8.T oughness ratings are bad upon Kahn Tear Test of 1.60 mm thick sheet specimens in both longitudinal and transver directions. This data is bad on a
limited number of tests and should be ud for general comparisons only.
Ratings A—over 175 000 Nm/m 2
B—over 140 000 thru 175 000 Nm/m 2 C—over 105 000 thru 140 000 Nm/m 2 D—0 through 105 000 Nm/m 2
9.Ratings A through D for workability (cold) and A through E for machinability are relative ratings in d
ecreasing order of merit.10.Bad upon 500 000 000 cycles of completely reverd stress using the RR Moore type of machine and specimen.
11.Elongation in 50 mm apply for thickness up through 12.50 mm and in 5D (5.65√A) for thickness over 12.50 mm where D and A are the diameter and
cross-ctional area of the specimen. Values for elongations in 5D (5.65√A) are shown in brackets.
TABLE 2A—TYPICAL MECHANICAL PROPERTIES AND COMPARATIVE CHARACTERISTICS (CONTINUED)
Typical Mechanical Properties (1)(2)
Tension Shear
Fatigue
Modulus
Resistance to Corrosion
Strength
Elonga-tion
Comparative Characteristics
Weldability (3)
Alloy and Temper (4)Ulti-mate MPa Yield 0.2%Offt MPa percent in 50 mm (1.60mm Thick Speci-men)Ulti-mate Shear Strength MPa Endur-ance Limit MPa Modu-lus (5)of Elas-ticity MPa x 10°General
(6)
Stress (7)corro-sion Crack-ing
Tough-ness (8)
Worka-bility (9)cold Macha-bility (9)
Gas Arc Resis-tance spot and Seam :
