1、 ENGINEERING STANDARDS Material Specification SUPERCEDED EDS-M-2106 Aluminum and Aluminum Alloy Extruded Shape This standard may be applied only for current project. It is Superceded for all future projects and replaced by GMW15665. 6*-,# F8 Note: 8 E:48t G8 =9 7 FF7 957%L+ , FG P-P Program .Bd# GMW
2、15665 ) $4=F7 957F$ . Copyright 2011 General Motors Company All Rights Reserved April 2011 Originating Department: GM Korea Engineering Standards Page 1 of 9 Version : 4 1 Scope 1.1 Material Description. This standard specifies the aluminum and aluminum alloy extruded shapes used by GM Korea Company
3、 (hereinafter referred to as the “GM Korea“). 1.1.1 Type and Use (Reference). 1 P7 1.1 8: 8-L C2e . 8 8t GM Korea Company (8F “$-1 ( F )72P 17F# 6*-,# F87 $4F7 9IF$ . 1.1.1 9* -C 7$ (=l ). Table 1: Type and Use / E 1: 9* -C 7$ Type / 9* Uses / 7$ Applications / 957 74)2e , 79E2e , !42e8 6Gl . 98dd .
4、E , 7( Gd7 &%7 17 . A1200S A3003S Somewhat superior to 1100 in strength. High extruding workability and corrosion resistance. Materials for heat exchanger, general mechanical parts etc. / 1100.($ 68 I$4 “ , 64)2e , !42e8 6Gl . 7( Gd7 8* , 8-Ld.E &%7 17 . A3203S A5052S Intermediate strength. High cor
5、rosion resistance and weldability. / :E8 9I$8 I$* 4: F7 F2e8 73LF7 .)8F $+GI18 .E7 .!42e , E+=*2e 6Gl . A7003S Though somewhat inferior to 7N01 in strength, rich in extruding property and provides thin large shapes. High corrosion resistance and weldability. / 7N01.($ I$# 68 !8p! , 62e8 96x -I8U8 $4
6、GI .E7 95FF . !42e , 79EI$ 6Gl . A7N01S Highly strength. Strength in weld zone recovers almost to base metal strength after aging at room temperature. High corrosion resistance. / I$4 “ CH 79E.8 I$4 17-?7 8F +8 I$7 4 G.) . !42e$ 6Gl . A7075S One of the highest strength of all the aluminum alloys. /
7、6*-,# F8 I$* 4: F07 38%P E:48x 957F$ . 2.1 17 E:4 / . ISO 6507 JIS Z2241 KS B0801 KS D0004 2.2 GM E:4 / . GMW3059 2.3 dA E:4 / . TMC003 Material Safety Data Sheet guidance documents GM KOREA ENGINEERING STANDARDS EDS-M-2106 Copyright 2011 General Motors Company All Rights Reserved April 2011 Page 3
8、of 9 Version : 4 3 Requirements 3.1 Chemical Composition. 3 7 1F 3.1 GF 2e. . Table 2: Chemical Composition (Unit: wt%) / E 2: GF 2e. ($88 : wt%) Type / 9* Si Fe Cu Mn Mg Cr Zn Zr, V Zr+Ti Ti Others / dA Al Each / 55 Total / F A1100 Si+Fe 1.0 max. / Si+Fe 1.0 8F 0.05 ) 0.20 0.05 max. / 0.05 8F . - -
9、 0.10 max. / 0.10 8F - - 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A1200 Si+Fe 1.0 max. / Si+Fe 1.0 8F 0.05 max. / 0.05 8F 0.05 max. / 0.05 8F - - 0.10 max. / 0.10 8F - 0.05 max. / 0.05 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A3003 0.6 max. / 0.6 8F 0.7 max. / 0.7 8F 0
10、05 ) 0.20 1.0 ) 1.5 - - 0.10 max. / 0.10 8F - - 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A3203 0.6 max. / 0.6 8F 0.7 max. / 0.7 8F 0.05 max. / 0.05 8F 1.0 ) 1.5 - - 0.10 max. / 0.10 8F - - 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A5052 0.25 max. / 0.25 8F 0.40 max. / 0.4
11、0 8F 0.10 max. / 0.10 8F 0.10 max. / 0.10 8F 2.2 ) 2.8 0.15 ) 0.35 0.10 max. / 0.10 8F - - 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A5454 0.25 max. / 0.25 8F 0.40 max. / 0.40 8F 0.10 max. / 0.10 8F 0.50 ) 1.0 2.4 ) 3.0 0.05 ) 0.20 0.25 max. / 0.25 8F - 0.20 max. / 0.20 8F 0.05 max. / 0
12、05 8F 0.15 max. / 0.15 8F Residue / !+l: A5083 0.40 max. / 0.40 8F 0.40 max. / 0.40 8F 0.10 max. / 0.10 8F . 0.40 ) 1.0 4.0 ) 4.9 0.05 ) 0.25 0.25 max. / 0.25 8F - 0.15 max. / 0.15 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A5086 0.40 max. / 0.40 8F 0.50 max. / 0.50 8F 0.10 max. / 0.
13、10 8F 0.20 ) 0.7 3.5 ) 4.5 0.05 ) 0.25 0.25 max. / 0.25 8F - 0.15 max. / 0.15 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A6061 0.40 ) 0.8 0.70 max. / 0.70 8F 0.15 ) 0.40 0.05 max. / 0.05 8F 0.8 ) 1.2 0.04 ) 0.35 0.25 max. / 0.25 8F - 0.15 max. / 0.15 8F 0.05 max. / 0.05 8F 0.15 max. /
14、 0.15 8F Residue / !+l: A6N01 0.40 ) 0.9 0.35 max. / 0.35 8F 0.35 max. / 0.35 8F 0.50(1) max. / 0.50(1) 8F 0.40 ) 0.8 0.30(1) max. / 0.30(1) 8F 0.25 max. / 0.25 8F - 0.10 max. / 0.10 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A6063 0.20 ) 0.6 0.35 max. / 0.35 8F 0.10 max. / 0.10 8F 0.
15、10 max. / 0.10 8F 0.45 ) 0.9 0.10 max. / 0.10 8F 0.10 max. / 0.10 8F - 0.10 max. / 0.10 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A7003 0.30 max. / 0.30 8F 0.35 max. / 0.35 8F 0.20 max. / 0.20 8F 0.30 max. / 0.30 8F 0.50 ) 1.0 0.20 max. / 0.20 8F 5.0 ) 6.5 Zr 0.05 ) 0.25 0.20 max. /
16、0.20 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: GM KOREA ENGINEERING STANDARDS EDS-M-2106 Copyright 2011 General Motors Company All Rights Reserved April 2011 Page 4 of 9 Version : 4 Type / 9* Si Fe Cu Mn Mg Cr Zn Zr, V Zr+Ti Ti Others / dA Al Each / 55 Total / F A7N01 0.30 max. / 0.3
17、0 8F 0.35 max. / 0.35 8F 0.20 max. / 0.20 8F 0.20 ) 0.7 1.0 ) 2.0 0.30 max. / 0.30 8F 4.0 ) 5.0 V 0.10 max, Zr 0.25 max. / V 0.10 8F , Zr 0.25 8F . 0.20 max. / 0.20 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A7075 0.40 max. / 0.40 8F 0.50 max. / 0.50 8F 1.2 ) 2.0 0.30 max. / 0.30 8F 2
18、1 ) 2.9 0.18 ) 0.28 5.1 ) 6.1 Zr+Ti 0.25 max / Zr+Ti 0.25 8F 0.20 max. / 0.20 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: (1) The content of Mn+Cr shall be within 0.50. / (1) Mn + Cr8t 0.50 8F) F$ . 3.2 Mechanical Properties. 3.2.1 Unless otherwise specified, for mechanical properties
19、 the test shall be performed on a separate test piece according to 3.4.2 and conform to the values specified in Table 3. 3.2 d95 2e: . 3.2.1 d95 2e:8t C-H :9IF: 6# F , 3.4.2 F7 &d( -$8 4G D8p) 4G F+ , E 38 F8x +9F6 F$ . Table 3: Mechanical Properties of Extruded Shapes / E 3: 688 d95 2e: Type / 9*
20、Temper grade / :- Hardness / $ Tensile Test / 88 4G Thickness, t(mm) / % , t(mm) HV Thickness, t(mm) / % , t(mm) Tensile strength (N/mm2) / 88 I$ (N/mm2) Yield strength (N/mm2) / F.) I$ (N/mm2) Elongation (%) / 48 (%) A1100S A1200S Hl12 - - - 75 min. / 75 81 20 min. / 20 81 - A3003S A3203S Hl12 - -
21、 95 min. / 95 81 35 min. / 35 81 - A5052S Hl12 - - - 175 min. / 175 81 70 min. / 70 81 - O - - - 175 ) 245 70 min. / 70 81 20 min. / 20 81 A5454S Hl12 - - t 130 215 min. / 215 81 85 min. / 85 81 12 min. / 12 81 O - - t 130 215 ) 285 85 min. / 85 81 14 min. / 14 81 A5083S Hl12 - - t 130 215 min. / 2
22、15 81 85 min. / 85 81 12 min. / 12 81 O - - t 38 275 ) 355 120 min. / 120 81 14 min. / 14 81 38 GI88 E+8t +!x)1 !F 9P9%L66 F$ . 3.3.2 4) -C 171 F* :8 3L 8# G$ 7( , 4 F d95 21.88 , dE , -1 , 8,p: &%8t F7%L: 6#$ . 3.4 4G . 3.4.1 +& 4G 8t 235 E72P 44F$ . 3.4.2 88 4G . 4G D8t 6-F8p) E 4 7 &d( =x?F+ , 4G
23、 D8 9*# E 57t M$ . Table 4: Sampling Method of Test Piece / E 4: 4G D =x? - Thickness, t(mm) / % , t(mm) Sampling location / =x? 88? 208 GI88 :0 $+ .88 D# 48 %7 .8 :E6.7 88?F$) =x?F$ . 40 8 GI88 E+0 :E4 08 :E6.7 88?F! , 48 %7 .8 488*7t :E4 08 :E6.7 88?F$) =x?F$ . Table 5: Kind of Test Piece / E 5: 4
24、G D8 9* Division / . Test piece / 4G D Thickness at sampling location. / =x?.888% . 20 mm max. / 20 mm 8F . No. 5 test piece. / 5Gl 4G D 20 mm min. / 20 mm 81 . No. 4 test piece. / 4Gl 4G D When it is impracticable to prepare No. 4 and No. 5 test pieces. / 4Gl , 5Gl 4G D8x =x?F 3L 6# 7 . No. 13B tes
25、t piece. / 13BGl 4G D When it is impracticable to prepare No. 4, No. 5 and No. 13B test pieces. / 4Gl , 5Gl, 13BGl 4G D8x =x?F 3L 6# 7 . Square or round test piece with a maximum sectional area or extruded as it is section test piece (gauge length is 50 mm). / 5 D# 88p) 4#F $4$+8 4G D D# 6 98$+ ,$4)
26、8 4G D (E9D* : 50 mm). Remark: In case it is impracticable to prepare No. 4, No. 5 and No. 13B test pieces, the elongation values shall be shown for informative reference. / /x : 4Gl , 5Gl , 13BGl 4G D8x =x?F 3L 6# 7 488t =l?) F$ . GM KOREA ENGINEERING STANDARDS EDS-M-2106 Copyright 2011 General Mot
27、ors Company All Rights Reserved April 2011 Page 7 of 9 Version : 4 3.4.3 Test Standards. ISO 6507: Vickers Hardness Test. JIS Z2241: Tensile Testing - Method of Test at Room Temperature. KS B0801: Tensile Test Piece for Metallic Materials - No. 4, No. 5, No. 13B. 3.4.3 4G . ISO 6507: Vickers Hardnes
28、s Test. JIS Z2241: Tensile Testing - Method of Test at Room Temperature. KS B0801: 8 88x 7 , F6* 72T8p) F$ . 5.3 1 -C -L)X . GM 8-LE:47 8F 9P%P .E8! 8*8 4G D8t ., 8-LE:47 9I%P 4G 8x 7 98x +94P6 F+ , 61 )= 987 :04 .2P8 388x -O6x6 F$ . &H88 , d# , 22e , 9P9 )9I ,* /D# 21: &%0 4)%P 6&F -8($ -P2%T 7 , 1
29、)7 388x -O6x6 F$ . $* F84 6# F , 8-L958p) 4 4=8x F6 F$ . -$8 GE84 6# F , )=8# 38%L: 68t 9PE8 61 )= 987 +& F$- 4G 8x -L.) 3LFF 0* ,l2PGF6 F$ . 8. 77 86 :04 .2P7t )=888 F87 8F $%P : 4G 8x 44F 3L 8$ . 5.4 FF2P# 6| %P$ . GM KOREA ENGINEERING STANDARDS EDS-M-2106 Copyright 2011 General Motors Company All
30、 Rights Reserved April 2011 Page 8 of 9 Version : 4 5.5 Material Safety Data Sheets/Safety Data Sheets (MSDS/SDS). For new product submissions, or when a change in chemical composition of an existing product has occurred, a complete copy of the Material Safety Data Sheet/Safety Data Sheet must be su
31、bmitted in compliance with the Globally Harmonized System of Classification and Labeling of Chemicals (GHS) requirements or other country-specific MSDS/SDS requirements. In addition, product MSDS/SDS submissions must be in compliance with specific country General Motors TMC003 Material Safety Data S
32、heet/Safety Data Sheet guidance documents where available. 5.6 All materials supplied to this standard must comply with the requirements of GMW3059, Restricted and Reportable Substances for Parts. 6 Approved Sources Engineering qualifications of an approved source are required for this standard. Onl
33、y sources listed in the GM Materials File under this standard number have been qualified by Engineering as meeting the requirements of this standard. For other GM locations, the responsible Engineering group should be contacted to obtain the approved source in that individual country. 7 Notes 7.1 Gl
34、ossary. Not applicable. 7.2 Acronyms, Abbreviations, and Symbols. GHS Globally Harmonized System MSDS Material Safety Data Sheet SDS Safety Data Sheet 8 Coding System This standard shall be referenced in other documents, drawings, etc., as follows: 5.5 ,p:6|98.(8* / 6|98.(8* (MSDS/SDS). 49PE8 )= D#
35、d97 )=%L# 9PE ! GF,p: 92e8 -%P 7 , GF ,p: .* y E47 4F 2l 9G 43B (GHS) D# 5 :7!- ,p:6|98.(8* / 6|98.(8* 7 1F8x +9F# ,p:6|98.(8* / 6|98.(8* 9PF6+ F$ . 4958p) 9PE8 ,p:6|98.(8* / 6|98.(8*# GM8 ,p:6|98.(8* / 6|98.(8*7 4F :?8 TMC0038 7 1F8x :43LF6+ F$ . 5.6 ., E:47 9P4%P +& 8:&8t GMW3059 (8TF,p: 179P )8 9
36、P* &d(6 F$ . 6 38 6= 8 E:48t 38%P 6=7 $4F d3T95 :8x 7F$ . 8 E:47 8F d3T958 :8 7x*%P GM 88 +2l7 !7(%P 6=+8 8 E:48 7 1F8x 94A$ . $* :7!7 88?F GM 8 7 , F$- 4-) 38%P 6= 9I.(* 83LFd 88F2P# F$- :04 .2P7t GE8F6 F$ . 7 768 9I8 7.1 98,l 76 . F$-1F 68 . 7.2 66 -C dGl . GHS Globally Harmonized System MSDS Mate
37、rial Safety Data Sheet SDS Safety Data Sheet 8 Ed - $* ,l2P! $+ &%72P ., E:48 87%T &# $80 M8 EdF$ . OOOOOO (EDS-M-2106) Material Specification Number / 8: E:4 -Gl Type / 9* GM KOREA ENGINEERING STANDARDS EDS-M-2106 Copyright 2011 General Motors Company All Rights Reserved April 2011 Page 9 of 9 Vers
38、ion : 4 9 Release and Revisions This standard was originated in July 1994. It was first approved by Engineering Standard Committee in July 1994. It was first published in July 1994. 9 9P9I -C P9I 8)Y ., E:48t 1994 “x 7 87 E:4 -Gl4 .7 %L6 , d3TE:41,h7 8F 1994“x 787 38%L6$ . ., E:48t 1994“x 787 ) 9P9I
39、 / -PF%L6$ . Issue / P9I8)Y Publication Date / 38 88 Description (Organization) / 9PP9I76 (:04.2P ) 4 APR 2011 Apply new Engineering Standard Template and change the referenced test standards. Superceded (Corrosion / Metallurgical Material Lab Team) / 4 d3TE:4 64 957 -C 957 4G - - . F9I957 =* (28*4G
40、 D4 ) Cross Index (Reference) / $48 /x (=l ) EDS-M-2106 KS D 6759 AA ASTM B221M A1100S A1100S 1100 1100 A1200S A1200S - - A3003S A3003S 3003 3003 A3203S A3203S - - A5052S A5052S - 5052 A5454S A5454S 5454 5454 A5083S A5083S 5083 5083 A5086S - 5086 5086 A6061S A6061S 6061 6061 A6N01S A6N01S - - A6063S A6063S 6063 6063 A7003S A7003S - - A7N01S A7N01S - - A7075S A7075S 7075 7075
