GMKOREA EDS-M-8620-2011 Sealer - Silicone.pdf
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1、 ENGINEERING STANDARDS Material Specification LIMITED USE EDS-M-8620 Sealer - Silicone Do Not Use on New Program; No Replacement. 4* 6d) Note: 8 E:48t G8 =97 FF7 957%L+ , FG P-P Program 72P# 957%L: 6#$ . Copyright 2011 General Motors Company All Rights Reserved June 2011 Originating Department: GM K
2、orea Engineering Standards Page 1 of 7 Version : 4 1 Scope 1.1 Material Description. Alcoxy Type based on Polydimethylsiloxane. One liquid type moisture hardening under normal temperature. 1.2 Typical Applications. This standard specifies the requirements of basic property for sealer-silicone, which
3、 is used for engine oil pan gasketing and sealing of automobiles. 2 References Note: Only the latest approved standards are applicable unless otherwise specified. 2.1 External Standards/Specifications. None 2.2 GM Standards/Specifications. EDS-M-0102 EDS-T-7406 EDS-T-7408 EDS-T-7418 EDS-T-7795 EDS-T
4、-7796 EDS-T-7902 GMW3059 2.3 Additional References. TMC003 Material Safety Data Sheet guidance documents 3 Requirements 3.1 General Properties. 1 P7 1.1 8: 8-L C2e . Polydimethylsiloxane8x :02e.8p) F# Alcoxy Type, 86GI -C 1772P 38X -G%L# -4.=9P 8 . 1.2 957 -88 . ., E:48t 8% = 7X8D8 Gasketing -C Seal
5、ing 7 957%L# Silicone Sealer8 8-L958 ,p2e 7 ?7 $4F7 9IF$ . 2 4) E:4 / :0 : C-H +d%P 9I8 6# F 48 07 38%P E:48x 957F$ . 2.1 17 E:4 / . None 2.2 GM E:4 / . EDS-M-0102 EDS-T-7406 EDS-T-7408 EDS-T-7418 EDS-T-7795 EDS-T-7796 EDS-T-7902 GMW3059 2.3 dA E:4 / . TMC003 Material Safety Data Sheet guidance docu
6、ments 3 7 1F 3.1 d., ,p2e . Table 1: General Properties / E 1: d., ,p2e Designations / 4G F+ Test Methods / 4G - Specifications / 3.1.1 Specific Gravity (g/ml). / /x:E (g/ml). EDS-T-7406 1.25 1.35 3.1.2 Extrusion Rate (sec/20g). / B8 (sec/20g). EDS-T-7796 Tip: 100 mm Taper nozzle, 3.5 mm Orifice. Ca
7、rtridge: 18 25 3.1.3 Solids Content (wt%). / GI. (wt%). Clause 3.2.1. / 3.2.1F =l9 . 96 min. / 96 81 . GM KOREA ENGINEERING STANDARDS EDS-M-8620 Copyright 2011 General Motors Company All Rights Reserved June 2011 Page 2 of 7 Version : 4 Designations / 4G F+ Test Methods / 4G - Specifications / 3.1.4
8、 Tac. Free Time (min). / := 9 48 (min). EDS-T-7795 2 30 3.1.5 Shear Strength (N/mm2). / 98$ I$ (N/mm2). EDS-T-7902-4, Clause 3.2.2. / 3.2.2F =l9 . 1.20 min. / 1.20 81 . 3.1.6 Tensile Strength (N/mm2). / 88 I$ (N/mm2). EDS-T-7408, Clause 3.2.3. / 3.2.3F =l9 . 1.50 min. / 1.50 81 . 3.1.7 Elongation at
9、 Break (%). / 48 (%). EDS-T-7408, Clause 3.2.3. / 3.2.3F =l9 . 400 min. / 400 81 . 3.1.8 Heat Resistance. / !7(2e . Change in tensile strength (%). / 88 I$ -G (%). EDS-T-7408, Clause 3.2.4. / 3.2.4F =l9 . (-10) +30 Change in Elongation ( ). / 48 -G ( ). 60 max. / 60 8F . 3.1.9 Eng Oil Resistance. /
10、!7:7X82e . Change in tensile strength (%). / 88 I$ -G (%). EDS-T-7408, 7418 Clause 3.2.5. / 3.2.5F =l9 . 40 max. / 40 8F . Change in Elongation ( ). / 48 -G ( ). 40 max. / 40 8F . Change in volume (%). / .Fp -G (%). Clause 3.2.6. / 3.2.6F =l9 . 35 max. / 35 8F . 3.1.10 Oil Resistance. / !8T2e . Chan
11、ge in tensile strength (%). / 88 I$ -G (%). EDS-T-7408, 7418, Clause 3.2.7. / 3.2.7F =l9 . 40 max. / 40 8F . Change in Elongation ( ). / 48 -G ( ). 40 max. / 40 8F . Change in volume (%). / .Fp -G (%). Clause 3.2.6. / 3.2.6F =l9 . 35 max. / 35 8F . 3.1.11 Durable air-tightness (ml/min). / ! d-42e (m
12、l/min). Clause 3.2.8. / 3.2.8F =l9 . 11 max. / 11 8F . 3.2 Test Methods. 3.2.1 Solids Content. 3.2.1.1 Clean 3 aluminum plates for specimen measurement with isopropyl alcohol and then dry them sufficiently. 3.2.1.2 Apply 3 5 g of sealant on each aluminum plate. 3.2 4G - . 3.2.1 GI. ?U9I - . 3.2.1.1
13、4* ?U9IF 6*-,# 9E4 2l P* 82F8)Fx 67) !8 2l=F .H 94A$ . 3.2.1.2 2l P8 6*-,# 9E47 55 Sealant* 6 3 5 g9I$ $E F$ . GM KOREA ENGINEERING STANDARDS EDS-M-8620 Copyright 2011 General Motors Company All Rights Reserved June 2011 Page 3 of 7 Version : 4 3.2.1.3 Weigh the specimen including the aluminum plate
14、 and record the reading to the second decimal place. 3.2.1.4 Expose the specimen to 23 E 5K 60%R.H, for 2 weeks to harden. 3.2.1.5 Take the specimen out and weigh it. 3.2.1.6 According the formula in EDS-T-7902-20, calculate ash content. 3.2.2 Shear Strength. 3.2.2.1 The pre-treatment and size of th
15、e test piece and test method shall conform to EDS-T-7902-4. 3.2.2.2 Apply the adhesive to an area of (25 12.7) mm and thickness 1 mm and subsequently harden it under conditions in clause 3.2.1.4. 3.2.2.3 The tensile speed shall be 50 mm/min. 3.2.3 Tensile Strength / Elongation at Break. 3.2.3.1 Afte
16、r dipping the release paper in water for 10 minutes, clean up moisture from the surface. 3.2.3.2 Spread the release paper in clause 3.2.3.1 on the painted steel sheet and carefully apply adhesive so as not to create bubbles. 3.2.3.3 Put another piece of release paper in clause 3.2.3.1 onto it and pl
17、ace the painted steel sheet and then press it with UTM so that thickness of 3 3.5 mm is maintained. 3.2.3.4 After hardening under 23 E 5K 60%R.H for 1 week, remove the release paper and harden it again for an additional week. If the test piece size is too large, cut it into several pieces and harden
18、 them. 3.2.3.5 With a test piece prepared as above, make a dumbbell-type test piece to EDS-T-7408-S1. 3.2.3.6 With the tensile speed set to 50 mm/min, measure the tensile strength / elongation at break. 3.2.4 Heat Resistance. After exposing the tensile strength / elongation at break test piece in cl
19、ause 3.2.3 to 175 E 168 hours, measure the tensile strength and elongation at break again as in clause 3.2.3 and compare the results with the initial tensile strength and elongation at break to calculate the change rate. 3.2.5 Engine Oil Resistance. After dipping the tensile strength / elongation at
20、 break test piece prepared as in clause 3.2.3 in 5W30 engine oil and subsequently exposing it to 150 E 336 hours, measure the tensile strength / elongation at break to EDS-T-7418 and then compare the results with the initial values to calculate the change rate. 3.2.1.3 6*-,# 9E48 ,h* E FF 4*8 ,h* ?U
21、9IF7 23L9D %;, 8*: d)F$ . 3.2.1.4 23 E 5K 60%R.H 8 972P 4* 2:08 -?F7 G4A$ . 3.2.1.5 4* !6 ,h* ?U9IF$ . 3.2.1.6 EDS-T-7902-208 47 8F7 GI.8x 1F$ . 3.2.2 98$I$ 4G - . 3.2.2.1 4D8 98=* , A d7t 4G -8t EDS-T-7902-47 :4F$ . 3.2.2.2 9E=9P8 $E +958x (25 12.7) mm ) F , $E % * 1 mm) F7 3.2.1.4 8 98p) G4A$ . 3.
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