FORD WSB-M99D61-A2-2013 DRY PAINT FILM LAMINATE FINISHED PARTS PLASTICS EXTERIOR TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions 2013 07 04 N-STATUS Replaced by WSS-M99P37-A A. Wedepohl,NA 2006 12 19 Revised Inserted 3.0; Deleted 3.1, 3.2, 3.3, 3.12, 3.13 Updated J. Faunt 1995 12 15 Activated J. Faunt Controlled document at www.MATS Copyright 2013, Ford Global Technolo
2、gies, LLC Page 1 of 6 DRY PAINT FILM LAMINATE, FINISHED PARTS, WSB-M99D61-A2 PLASTICS, EXTERIOR NOT FOR NEW DESIGN 1. SCOPE The material defined by this specification is a dry paint film laminate for use on thermoplastic exterior parts. 2. APPLICATION This specification was released originally for e
3、xterior mirror skull cap, a component in a mirror assembly. Production application of this material consists of injection molding behind a thermoformed laminate preform insert which has been configured to the finished part. 3. REQUIREMENTS 3.0 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material
4、suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.4 CONSTRUCTION LAYER MAJOR COMPONENT Clearcoat Acrylic polymer/polyvinylidene difluoride Print/Design Optional gravure ink Basecoat Pigmented acrylic/polyvinylidene difluoride
5、 Size and Varies with thermoplastic substrate backing Backing Sheet Total thickness and variation will be in a control plan agreed to by the supplier and user. Approval for the construction is granted by material class, e.g. ABS, TPO, PC, etc. 3.5 FILM PROPERTIES 3.5.1 Appearance (FLTM BI 109-01 and
6、 BI 110-01) Color, gloss and surface finish shall match the Master Appearance Sample or the initial sample as approved by Design Center. See para 5.1 table for gloss correction for index of refraction. 3.5.2 Adhesion min, Figure 1 (FLTM BI 106-01) No more flaking than Fig 1 (less than 5%). ENGINEERI
7、NG MATERIAL SPECIFICATION WSB-M99D61-A2 Copyright 2013, Ford Global Technologies, LLC Page 2 of 6 3.5.3 Manual Separation The individual layers of material must not be separable from each other by mechanical means without cohesive break. 3.5.4 Visual Evaluation The finished parts shall show no evide
8、nce of blisters or delamination. 3.5.5 Heat Aging The finished part shall show no visible evidence of warpage, deformation, cracks, delamination or any other failure to an extent that would affect its use in the ultimate assembly. There shall be no local shrinkage where the part has been gated which
9、 would interfere with assembly to relating parts, or affect its appearance. The finished part shall show no change in appearance when compared to the original part. The adhesion of the film laminate to itself and to the substrate shall meet para 3.5.2 after heat aging. 3.5.5.1 Assembly Mount the ass
10、embly on a suitable fixture in car position in a mechanical convection oven maintained at 80 +/- 2 C for 7 d. Evaluate after conditioning at 23 +/- 2 C. 3.5.5.2 Component As under 3.5.5.1, except the component is unmounted. 3.6 PAINT REPAIR OVEN RESISTANCE Not required for shielded assemblies - see
11、process manual The finished part shall show no visible evidence of warpage, deformation, cracks, delamination or any other failure to an extent that would affect its use in the ultimate assembly. There shall be no local shrinkage where the part has been gated which would interfere with assembly to r
12、elating parts, or affect its appearance. The finished part shall show no change in appearance when compared to the original part. The adhesion of the film laminate to itself and to the substrate shall meet para 3.5.2 after heat aging. Mount the assembly on a suitable fixture in car position in a mec
13、hanical convection oven maintained at 120 +/- 2 C for 30 minutes. Evaluate after conditioning at 23 +/- 2 C. 3.7 RESISTANCE PROPERTIES 3.7.1 ENVIRONMENTAL CYCLING (FLTM BQ 104-07, Procedure 1 and Procedure 8) ENGINEERING MATERIAL SPECIFICATION WSB-M99D61-A2 Copyright 2013, Ford Global Technologies,
14、LLC Page 3 of 6 The finished part shall show no visible evidence of warpage, deformation, cracks, delamination or any other failure to an extent that would affect its use in the ultimate assembly. The finished part shall show no change in appearance when compared to the original part. The adhesion o
15、f the film laminate to itself and to the substrate shall meet para 3.5.2 after heat aging. 3.7.2 RESISTANCE TO COLD IMPACT (FLTM BO 151-01, para 3.7.2.1; ASTM D 3763, para 3.7.2.2) 3.7.2.1 Drop Ball - Method 2 No shattering or breaking (any fissure through the full thickness of the material). 3.7.2.
16、2 Instrumented Impact 70% Retention Direct Use part section or plaques representative of the actual part with respect to materials thicknesses and molding conditions. Determine impact strength at 23 +/- 2 C and at -30 +/- 2 C. Record load and deformation at first crack max load and rate for brittle
17、or ductile failure. 3.7.3 SHOCK TEST The decorated component shall show no breaks, cracks or other failure. The adhesion of the individual surface coating shall meet the requirements of para 3.5.2. Maintain the finished part or section at -40 +/- 2 C for 16 h. Then, immediately immerse the part into
18、 a 70 +/- 2 C water bath for 5 minutes. Evaluate after conditioning test sample to 23 +/- 2 C. 3.8 RESISTANCE TO WEATHERING SAE J1545 (Florida exposure applicable to parts using materials without previous weathering approval.) After exposure the parts/decorated component shall meet the CIE values fo
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