GMKOREA EDS-T-4571-2011 Test Procedure of Surface Hardness.pdf
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1、 ENGINEERING STANDARDS Test Procedure LIMITED USE EDS-T-4571 Test Procedure of Surface Hardness Do Not Use on New Program; No Replacement. Seat E+I$ 4G 98 88x 7 , F6* 72T8p) F$ . 1.1 +95 . Seat Cushion -C Back8 E+$ C2e G88x +958p) F$ . 1.2 957 -88 . +& Seat7 957F$ . 2 4) E:4 / :0 : C-H +d%P 9I8 6# F
2、 48 07 38%P E:48x 957F$ . 2.1 17 E:4 / . None 2.2 GM E:4 / . None 2.3 dA E:4 / . None 3 4G 88 3.1 4G 8/x . 3.1.1 Seat* 4= M8 9IF 3L 8# Jig. 3.1.2 9I-L . 3.1.3 F:E84 8? . 3.1.4 -88?U9I 8? . 3.1.5 F:E?U9I 8? . 3.1.6 - 50 mm 8d% (,* 1 =l9 ). GM KOREA ENGINEERING STANDARDS EDS-T-4571 Copyright 2011 Gene
3、ral Motors Company All Rights Reserved September 2011 Page 2 of 4 Version : 3 Figure 1 / ,* 1 3.2 Test Piece. Minimum three new assembled seats. 4 Procedures 4.1 Preparation. 4.1.1 Fit the seat-fixing jig on the leveling surface table, and mount the seat on the jig. 4.1.2 Set the other seat adjuster
4、 systems to the positions specified in the design standard. 4.1.3 If the positions specified in the design standard are unknown, set the positions as follows: y Slider: center. y Torso angle: 25 28q. y Lifter: Lowermost position. y Lumbar support: weakest position. 4.2 Conditions. 4.2.1 Test Conditi
5、ons. Deviations from the requirements of this standard shall have been agreed upon. Such requirements shall be specified on component drawings, test certificates, reports, etc. 4.3 Instructions. 4.3.1 Fit the jig on the position shown in fig. 2, and install the weight loading equipment on the cushio
6、n in perpendicular to the ground, and on the back in perpendicular to the torso line. 4.3.2 Load the weight of 6 kgf on the cushion and 3 kgf on the seat back with preliminary compression. 4.3.3 Load the weight on the cushion (0 kgf 6 kgf 0 kgf) and on the seat back (0 kgf 3 kgf 0 kgf) with the init
7、ial load of 0.5 kgf with a speed of 150 300 mm/min to create a load-displacement line graph. 3.2 4G D . 4E ASSY1B8 Seat* 3P 81 4G F$ . 4 4G 9F$ . y Lumbar Support: 6F 88? . 4.2 8-L 9 . 4.2.1 4G 9 . .,E:48p).Bd-6!#7 1F8t $-188 F8F6 F+ , 4)$+ , 4G 2e952P , .(2P&%7$+d%L66F$ . 4.3 4G - . 4.3.1 ,* 27t M8
8、t 88?7 Jig * 8=F Cushion8t :+7 3L:-F , Back8t Torso Line7 3L: -F8p) F:E84 8?* 8=F$ . 4.3.2 78p) Cushion8t 6 Kgf , Back8t 3 Kgf 8x 1G 84F$ . 4.3.3 0.5Kgf * 6 Kgf - 0 Kgf), BACK (0 Kgf - 3 Kgf - 0 Kgf)8 F:E8x 84F7 F:E -88 2T$* F$ . GM KOREA ENGINEERING STANDARDS EDS-T-4571 Copyright 2011 General Motor
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