GMKOREA EDS-M-2105-2011 Aluminum Alloy forgings (VERSION 4 English Korean This standard may be applied only for current project It is Superseded for all future projects and replace.pdf
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1、 ENGINEERING STANDARDS Material Specification SUPERCEDED EDS-M-2105 Aluminum Alloy forgings This standard may be applied only for current project. It is Superceded for all future projects and replaced by GMW15657. 6*-,# F07 38%P E:48x 957F$ . 2.1 17 E:4 / . ISO 6506 JIS Z2241 KS B0801 KS D0004 2.2 G
2、M E:4 / . GMW3059 2.3 dA E:4 / . TMC003 Material Safety Data Sheet guidance documents GM KOREA ENGINEERING STANDARDS EDS-M-2105 Copyright 2011 General Motors Company All Rights Reserved April 2011 Page 2 of 7 Version : 4 3 Requirements 3.1 Chemical Composition. 3 7 1F 3.1 GF 2e. . Table 2: Chemical
3、Composition (Unit: wt%) / E 2: GF 2e. ($88 : wt%) Type / 9* Si Fe Cu Mn Mg Cr Zn Zr+Ti Ti Others / dA Al Each / 55 Total / F A2014 0.50 ) 1.2 0.70 max. / 0.70 8F 3.9 ) 5.0 0.40 ) 1.2 0.20 ) 0.8 0.10 max. / 0.25 max. / 0.25 8F 0.20 max. / 0.20 8F 0.15 max. / 0.15 8F 0.05 max. / 0.05 8F 0.15 max. / 0.
4、15 8F Residue / !+l: A6151 0.6 ) 1.2 1.0 max. / 1.0 8F 0.35 max. / 0.35 8F 0.20 max. / 0.20 8F 0.45 ) 0.8 0.15 ) 0.35 0.25 max. / 0.25 8F - 0.15 max. / 0.15 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: A6061 0.40 ) 0.8 0.70 max. / 0.70 8F 0.15 ) 0.40 0.15 max. / 0.15 8F 0.8 ) 1.2 0.04 )
5、 0.35 0.25 max. / 0.25 8F - 0.15 max. / 0.15 8F 0.05 max. / 0.05 8F 0.15 max. / 0.15 8F Residue / !+l: 3.2 Mechanical Properties. 3.2.1 Unless otherwise specified, tensile strength, yield strength and elongation shall be performed on a test piece according to 3.6.2 and shall conform to the values sp
6、ecified in Table 3. However, in case the purchaser requires that the tensile test piece shall be taken in the direction not parallel to the metal flow, they shall conform to the values specified in Table 4. The hardness test may substitute the tensile test with the approval of purchaser. In this cas
7、e, the brinell hardness values shall conform to Table 5. 3.2 d95 2e: . 3.2.1 88 , F.)I$ -C 488t C-H :9IF: 6#F , 3.6.2 F7 &d( -$8 4G D8p) 4G F+ , E 38 F8x +9F6 F$ . $ +84 $*2T7 DFF: 6# -F8p) 884G D8x ?F 8x 7 F# 7 E 48 F8x +9F6 F$ . 884G 8t +88 388x 66 $4G 8p) $4=F 3L 88p+ 8 7 /*“ $ F8t E 5* &d*$ . Ta
8、ble 3: Tensile, Yield Strength and Elongation of Die Forgings (Test piece parallel to metal flow) / E 3: GI$9E8 88 , F.)I$ -C 48 ($*2T7 DFF 4G D ) Type / 9* Temper grade / :- Tensile test / 88 4G Maximum thickness at heat treatment, t(mm) / 7(=*48 $4% , t(mm) Tensile strength (N/mm2) / 88 I$ (N/mm2)
9、 Yield strength (N/mm2) / F.) I$ (N/mm2) Elongation (%) / 48 (%) Test piece / 4G D Product / 9PE A2014FD T4 t 100 380 min. / 380 81 205 min. / 205 81 16 min. / 16 81 11 min. / 11 81 GM KOREA ENGINEERING STANDARDS EDS-M-2105 Copyright 2011 General Motors Company All Rights Reserved April 2011 Page 3
10、of 7 Version : 4 Type / 9* Temper grade / :- Tensile test / 88 4G Maximum thickness at heat treatment, t(mm) / 7(=*48 $4% , t(mm) Tensile strength (N/mm2) / 88 I$ (N/mm2) Yield strength (N/mm2) / F.) I$ (N/mm2) Elongation (%) / 48 (%) Test piece / 4G D Product / 9PE A2014FD T6 t d 75 450 min. / 450
11、81 380 min. / 380 81 8 min. / 8 81 6 min. / 6 81 75 $4% , t(mm) Tensile strength (N/mm2) / 88 I$ (N/mm2) Yield strength (N/mm2) / F.) I$ (N/mm2) Elongation (%) / 48 (%) Product / 9PE A2014FD T6 t d 25 440 min. / 440 81 380 min. / 380 81 3 min. / 3 81 25 8 $*2T H*0 DFF$) $+8 :E4 .72P =x?F$ . 3.6.3 *A
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