FORD WSS-M4G252-E2-2009 SEALER VINYL LOW DENSITY EXTRUDABLE SPRAYABLE ABRASION RESISTANT NON-PAINTABLE TO BE USED WITH FORD WSS-M99P1111-A 《低密度、可挤压、可喷涂、耐磨、不可油漆的乙烯基密封剂 与标准FORD WS.pdf
《FORD WSS-M4G252-E2-2009 SEALER VINYL LOW DENSITY EXTRUDABLE SPRAYABLE ABRASION RESISTANT NON-PAINTABLE TO BE USED WITH FORD WSS-M99P1111-A 《低密度、可挤压、可喷涂、耐磨、不可油漆的乙烯基密封剂 与标准FORD WS.pdf》由会员分享,可在线阅读,更多相关《FORD WSS-M4G252-E2-2009 SEALER VINYL LOW DENSITY EXTRUDABLE SPRAYABLE ABRASION RESISTANT NON-PAINTABLE TO BE USED WITH FORD WSS-M99P1111-A 《低密度、可挤压、可喷涂、耐磨、不可油漆的乙烯基密封剂 与标准FORD WS.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、 ENGINEERING MATERIAL SPECIFICATIONDate Action Revisions 2009 04 02 Revised See Summary of Revisions M. Mehandru, FNA 2006 10 27 Activated M. Mehandru Printed copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 1 of 9 SEALER, VINYL, LOW DENSITY, EXTRUDABLE, SPRAYABLE WSS-M4G25
2、2-E2 ABRASION RESISTANT, NON-PAINTABLE 1. SCOPE The material defined by this specification is a vinyl based, extrudable, sprayable, sag resistant, abrasion resistant, non-paintable, heat cured sealer. 2. APPLICATION This specification was released originally as an interior seam sealer and underbody
3、stone chip resistance material. The material will not have good appearance when top-coated and therefore should be used only on non-paintable surfaces. This material can be sealer gun extruded and spray applied to body electrocoat primed surfaces. Recommended material cure schedules are specified in
4、 para 5.3. A 0.50 mm wet film thickness is recommended for abrasion resistance. 3. REQUIREMENTS Material specification requirements are to be used for initial qualification of materials. 3.1 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Comp
5、anys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.2 SOLIDS, min 95% (ASTM D 2834, except heat at 102 +/- 1 C for 3 h in a mechanical convectional oven. Save sample for next test, para 3.3) 3.3 ASH (Based on solids weight), (ISO 3491, Method A, 760 +/- 30 C) The ash content tole
6、rance for any one supplier shall be +/- 5% based on the recorded ash content for their originally approved production sample. See paragraph 4.4. 3.4 WEIGHT PER VOLUME .87 kg/L, max (ASTM D 816) .93 kg/L sprayed max The weight per volume shall be measured after the material has undergone airless spra
7、ying. Spray the sealer at a 300 mm distance thru a -.79 mm/60 tip at 20 MPa onto a clean steel panel. Measure the density of sprayed sealer with a pycnometer. The weight tolerance for any one supplier shall be +/- 0.06 kg/L, based on the recorded weight of his original approved production sample See
8、 paragraph 4.5. ENGINEERING MATERIAL SPECIFICATIONWSS-M4G252-E2 Printed copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 2 of 9 3.5 VISCOSITY (SAE J1524, VIS-2, 1.32 mm orifice, 280 kPa) Final approval of a specific material viscosity for production shipments shall be made
9、by the affected manufacturing activity. In all cases, the viscosity shall be within process limits as identified on the material control plan. The viscosity tolerance for any one supplier shall be +/- 10%, based on the recorded viscosity of the original approved production sample. 3.5.1 As Received
10、Viscosity +/- 10% (Unagitated - Method “A“) 3.5.2 Aged Viscosity original +50% (Material aged in closed container for increase 72 h at 40 +/- 1 C, Unagitated - Method “A“) 3.6 BRIDGING, max 6.4 mm Test Method: Apply a 13 mm diameter material bead over the 6.4 mm diameter holes shown in sketch below.
11、 Condition the test fixture with material bead for 15 minutes at 23 +/- 2 C, then bake fixture at the minimum bake schedule per para 4.3. Measure the amount of material sag through hole. BRIDGING TEST FIXTURE ENGINEERING MATERIAL SPECIFICATIONWSS-M4G252-E2 Printed copies are uncontrolled Copyright 2
12、009, Ford Global Technologies, LLC Page 3 of 9 3.7 SAG RESISTANCE 3.7.1 Horizontal, max 6.4 mm 3.7.2 Vertical, max 6.4 mm 3.7.3 Inverted No loss of material Test Method: Apply a 3 x 30 x 200 mm ribbon of material along the center line of three electrocoated panels prepared per para 4.2 Scribe panels
13、 to mark the initial material location. Position the panels with the material in the attitude above for 1 h. Immediately after conditioning, place panels in an oven to cure material at the minimum bake schedule per para 4.3. Maintain panels in the specified attitude during baking and cooling. Allow
14、the panel to cool to 23 +/- 2 C. Determine the sag by measuring the material movement below the scribe mark. 3.8 ADHESION Shall not be peeled off in a continuous film at any thickness. Test Method: Apply 6.4 - 0 mm tapered material ribbon on two electrocoated panels prepared per para 4.2. See sketch
15、 below. Subject one test panel, to the minimum bake schedule and the other test panel to the maximum bake schedule identified per para 4.3. Condition panels after baking at 23 +/- 2 C for 1 h minimum. Evaluate adhesion by cutting a 25 mm wide strip across the tapered ribbon. Using the tip of a squar
16、e spatula, lift the material at both the thin and thick film edges then attempt to had peel material at 90 from substrate. Save test panels for Heat Stability Test, para 3.9 and Corrosion Resistance Test, para 3.10. ENGINEERING MATERIAL SPECIFICATIONWSS-M4G252-E2 Printed copies are uncontrolled Copy
17、right 2009, Ford Global Technologies, LLC Page 4 of 9 3.9 HEAT RESISTANCE TEST No evidence of blistering, cracking, charring or other deleterious effects Test Method: Examine the maximum bake panel prepared for Adhesion Test, para 3.8, for any of the above conditions. 3.10 CORROSION RESISTANCE TEST
18、No corrosion or adhesion loss 3.10.1 Option 1 (FLTM BI 123-03, 30 cycles for North America, 50 cycles for Europe) Or 3.10.2 Option 2 (CETP 00.00-L-467, 6 weeks) Note: Report the test method used. 3.11 MANDREL BEND TEST No cracking or (FLTM BV 122-01, material bake schedule adhesion failure per para
19、5.3, heat age test specimen 14 days at 70 +/- 1 C before test) 3.11.1 Test at 23 +/- 2 C 3.11.2 Test at -20 +/- 1 C 3.12 CRACK RESISTANCE, min 5,000 cycles (FLTM BV 115-01, except bake an additional set of panels for 15 minutes at 135 +/- 1 C for normal and aged test, use substrate identified per pa
20、ra 4.2) ENGINEERING MATERIAL SPECIFICATIONWSS-M4G252-E2 Printed copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 5 of 9 3.13 COMPATIBILITY WITH PRODUCTION PAINTS No color transfer of the topcoat from the sealer to other objects. Test Method: 3.13.1 Prepare test panels per F
21、LTM BV 153-08, Procedure “A“, but with the following modifications: Spray a 7 micrometer (top of panel) to 25 micrometer (bottom of panel) body primer film wedge wet-on-wet over the sealer and bake for 8 minutes at 135 +/- 1 C metal temperature. Spray a 7 micrometer (top of panel) to 25 micrometer (
22、bottom of panel) topcoat film wedge and bake for 10 minutes at 130 +/- 1 C metal temperature. Apply current production paint as identified by the B&CE Materials and Corrosion Protection Engineering Office. 3.13.2 Condition the test panels for 1 h at 23 +/- 2 C. 3.13.3 With moderate pressure, rub the
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