FORD WSS-M15P45-B-2009 ASSEMBLY PERFORMANCE INSTRUMENT PANEL AND SOFT INTERIOR COMPONENTS FLEXIBLE COVER SKIN MATERIAL TO BE USED WITH FORD WSS-M99P1111-A 《使用柔性盖皮材料的仪表盘和软内饰部件的装配性.pdf

1、 ENGINEERING MATERIAL SPECIFICATIONDate Action Revisions Rev. 0 2009 06 08 Activated Y. Bankowski, FNA; C. Boese, FNA Printed copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 1 of 10 ASSEMBLY PERFORMANCE, INSTRUMENT PANEL AND SOFT WSS-M15P45-B INTERIOR COMPONENTS, FLEXIBLE

2、COVER SKIN MATERIAL 1. SCOPE The material defined by this specification is an instrument panel assembly, instrument panel component, floor console armrest, valence panel, hush panel, door panel or wrapped pillar, which utilizes a flexible (soft) cover skin material over a hard substrate with or with

3、out foam or spacer fabric, and with or without a topcoat. 2. APPLICATION This specification was released originally for material used for all soft interior components, not including seats, molded/foam-in-place armrests and headrests. Instrument panels containing an integrated airbag system must also

4、 meet any additional specifications on the Engineering Document. Hard instrument panels should be tested to WSS-M15P4-F. This specification includes top-coated (added for gloss control, haptics and/or cleanability) and in-mold coated (IMC) skins. All painted (20 m film build) flexible cover skins sh

5、all meet the requirements of WSS-M2P188-A1. Testing must be conducted on parts at DV and PV unless specified otherwise by Ford Engineering. See Tables 1 soft upper door trim panels): 7 days at 100 +/- 2 C 3.3.2.3 Horizontal or vertical parts BELOW THE BELT-LINE (e.g., door panels and soft consoles t

6、hat are not integrated with the instrument panel): 7 days at 90 +/- 2 C 3.3.2.4 Other non-sun loaded floor level parts. 7 days at 80 +/- 2 C Requirements: The trimmed assemblies shall remain relatively unaffected by the exposure cycles during and after the tests as demonstrated: (1) Tactually/visual

7、ly - no excessive tackiness, loss in surface-grain, or surface-color change (AATCC Procedure 1, Rating 4, min); no wrinkling, distortion, blistering, warping, delamination, blushing, hazing, milking, staining, waviness, or other objectionable visual appearance. (2) Functionally - no excessive expans

8、ion, shrinking, or warping that will interfere with normal functional operations. (3) Dimensionally - no movement exceeding 3.0 mm from the original installed position during or after the test; for the “significant characteristic locations“, no movement exceeding 0.5 mm from the original installed p

9、osition during or after the test. Dimensional exceptions to these requirements may be allowed on the Engineering drawing. For Instrument Panels Only (para 3.3.3 3.3.5): Test Method: After sunload testing/heat aging, cut test specimens (remove foam and substrate) and condition them for 24 h at 23 +/-

10、 2 C and 50 +/- 5% relative humidity prior to performing the following tests: 3.3.3 Color Stability Rating 3 min (ISO 105-A02/AATCC Evaluation Procedure 1) Shall show no evidence of tackiness, spewing, or exhibit staining. Any spotty or non-uniform staining or discoloration shall be cause for reject

11、ion. A color shift that reverses after 16 h Xenon weathering, per 3.9.1 is acceptable. 3.3.4 Cold Flexibility No cracks (180 bend at -20 C over a 20 +/- 1 mm diameter mandrel, sample size 50 x 150 +/- 1 mm) ENGINEERING MATERIAL SPECIFICATIONWSS-M15P45-BPrinted copies are uncontrolled Copyright 2009,

12、 Ford Global Technologies, LLC Page 5 of 10 3.3.5 Elongation at Break, Change from Original Value 50% max (ISO R 527, type 2, 100 mm/minute test speed, see para 3.7 for original elongation) 3.4 BOND STRENGTH - PEEL ADHESION, min 3.4.1 Initial Bond Strength, Peel Adhesion, min (ISO 2411/ FLTM BN 151-

13、05, 180opeel, 300 mm/minute, any direction) For Instruments Panels: Flexible cover-skin layer 175 N/m and 100% foam tear to foam (if applicable) (100% Cohesive) Flexible cover-skin layer to spacer fabric 1200 N/m (if applicable) (100% Cohesive) Cover-stock (knit backing or spacer fabric) 880 N/m and

14、 100% foam tear to substrate (if applicable) (100% Cohesive) Foam to substrate (if applicable) 400 N/m and 100% foam tear (100% Cohesive) For all other parts: Flexible cover-skin layer 175 N/m and 100% foam tear to foam (if applicable) (100% Cohesive) Cover-stock (knit backing or foam) 240 N/m and 1

15、00% foam tear to substrate (if applicable) (100% Cohesive) 3.4.2 After Aging Bond Strength Change, Peel Adhesion +/- 25% and 100% foam tear, (Sun Load or Long Term Heat Exposure per 3.3.2, (100% Cohesive) ISO 2411/ FLTM BN 151-05, 180opeel, 300 mm/minute, any direction) 3.5 INDENTATION AND RECOVERY

16、Complete recovery after 1 hour (FLTM BO 111-02, Method B) Only applicable for components with foam or spacer fabric between the skin and substrate. 3.6 COLOR AND APPEARANCE PROPERTIES Sample shall be tested as part of a production assembly composite (skin and foam or spacer fabric). Sample shall be

17、cut from the locations specified. The material shall not exhibit staining, color tone change or change in hue after exposure in accordance with Fade Testing below. Read and report the gloss change. In addition, there shall be no cracking, crazing or other deterioration. The material must remain flex

18、ible and exhibit no cracking when bent around a 20 +/- 2 mm mandrel after the specified exposure. Remove foam and bend with foam side of skin to the mandrel. ENGINEERING MATERIAL SPECIFICATIONWSS-M15P45-BPrinted copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 6 of 10 3.6.1

19、 Resistance to Fade (FLTM BO 116-01, ISO 105 A-02/AATCC Evaluation Procedure 1) In Vehicle Sunlight Exposure Level FLTM BO 116-01 Test Exposure AATCC Rating After Exposure, min. Severe Exposure: Instrument panel top parcel shelf assembly/package tray, interior rear view mirror housing. 3609.6 kJ/m2R

20、ating 4 Heavy Exposure: Instrument panel lower, 2 tone IP, IP bezel, airbag, steering wheel, message center, appliqus and center finish panel. 2406.4 kJ/m2Rating 4 Above the Belt-line: Instrument panel lower, door panel rollover, interior trim, pillars, garnish moldings, seats, head rest, sunshade,

21、sun visor, seat belt webbing then re-measure and recalculate the loss of reflectance. 3.13 RESISTANCE TO MIGRATION STAINING Rating 5 min AND BLOCKING (FLTM BN 103-01, ISO 105-A02/AATCC Evaluation Procedure 1) No evidence of injurious exudation, adhesion (tackiness), separation, color transfer, stain

22、ing, or flattening of the embossing when material is placed in the following positions: Top surface to top surface Top surface to standard vinyl test material Top surface to back surface 3.14 SOILING AND CLEANABILITY (FLTM BN 112-08, ISO 105-A02/AATCC Evaluation Procedure 2) Test Agents: Soil, Coffe

23、e, Grease Cleanability Rating 3 min ENGINEERING MATERIAL SPECIFICATIONWSS-M15P45-BPrinted copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 8 of 10 The following four tests (para 3.15 3.18) are only required for top-coated skins. For painted applications, follow the requirem

24、ents for WSS-M2P188-A1. 3.15 RESISTANCE TO ABRASION (SAE J 948, CS-10 wheels, 500g, 250 cycles) The surface shall show no evidence of wear through and the color shall be compatible to the adjacent unabraded area. A change in gloss is not acceptable. 3.16 RESISTANCE TO SCUFFING (SAE J365, 250 cycles)

25、 The surface shall show no evidence of wear through, lifting, peeling or excessive scuffing and the color shall be compatible to the adjacent unabraded area. A change in gloss is not acceptable. 3.17 RESISTANCE TO CLEANING AGENTS Rating 4 min (FLTM BN 107-01, 10 cycles, AATCC Evaluation Procedure 2)

26、 Test Procedure: Saturate white cotton cloth with the cleaners listed. Evaluation according to the AATCC Scale. Cleaners: 1) Deionized water 2) Window cleaner, see para 4.1 3) All purpose cleaner, see para 4.1 4) Dry (no cleaners or water) 3.18 RESISTANCE TO SUNTAN LOTION Rating 3 max AND INSECT REP

27、ELLENT (FLTM BI 113-08, 23oC and 74oC) No loss of adhesion 3.19 ENVIRONMENTAL STRESS CRACKING No cracking or crazing allowed (FLTM BO 127-03) All plastic parts in the assembly are to be tested with the grease or other materials listed in the BOM that come in contact with the plastic components. All

28、amorphous materials (such as PC, PC/ABS ABS, SMA, ASA, PPO) must be evaluated for potential incompatibility with other materials. For example, polycarbonate should be tested with grease used on fasteners; vinyl must be tested for compatibility with the substrate material they are covering. 4. GENERA

29、L INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of this specification. 4.1 CLEANING AGENTS (See para 3.17) 1) Window cleaner 2) All Purpose Cleaner* *or Ford Motor Company Recommended Equivalents ENGINEERING MATERIAL SPECIFICATIONWSS

30、-M15P45-BPrinted copies are uncontrolled Copyright 2009, Ford Global Technologies, LLC Page 9 of 10 MINIMUM SAMPLE REQUIREMENTS Table 1 * Testing depends on whether a 355 x 100 mm sample can be cut out from the part. * Testing may be run at DV if plaques/parts are available with the program specific

31、 grains Bolded Tests may be run on the skin test plaques. All other tests need to be run on parts. For paragraphs: # of Parts / Test Specimens, min Colors DV PV 3.3.1 Short Term Heat, Humidity and Cold Cycle 1 full assembly; 2 required if new technology darkest X X 3.3.2 Long Term Heat Exposure / Su

32、n Load 1 full assembly; 2 required if new technology darkest X X 3.3.3 Color Stability 1 specimen taken from para 3.3.2 darkest X 3.3.4 Cold Flexibility 3 test specimens taken from para 3.3.2 darkest X 3.3.5 Elongation at Break 6 test specimens (3 latitudinal and 3 longitudinal) taken from para 3.3.

33、2 darkest X 3.4.1 Initial Bond Strength 5 test specimens any X 3.4.2 After Aging Bond Strength 5 test specimens any X 3.5 Indentation and Recovery 3 test specimens any X 3.6.1 Resistance to Fade 2 test specimens all X 3.7 Original Elongation 6 test specimens (3 latitudinal and 3 longitudinal) darkes

34、t X 3.8 Fogging 3 test specimens any X 3.9 Flammability* 5 test specimens all X 3.10 Odor 1 test specimen per condition any X 3.11 Resistance to Dynamic Exudation 1 part any X 3.12 Degree of Soil Transfer to Leather and Polymeric Fabrics 1 test specimen per condition, per grain lightest X* 3.13 Resi

35、stance to Migration Staining and Blocking 1 test specimen per condition all X 3.14 Soiling and Cleanability 3 test specimens per condition, per grain lightest X* 3.15 Resistance to Abrasion 3 test specimens all X* 3.16 Resistance to Scuffing 3 test specimens all X* 3.17 Resistance to Cleaning Agents

36、 1 test specimen per condition any X* 3.18 Resistance Suntan Lotion and Insect Repellent 1 test specimen per condition any X 3.19 Environmental Stress Cracking 4 test specimens any X ENGINEERING MATERIAL SPECIFICATIONWSS-M15P45-BPrinted copies are uncontrolled Copyright 2009, Ford Global Technologie

37、s, LLC Page 10 of 10 TESTING REQUIREMENTS Table 2 For paragraphs: # of Parts / Test Specimens Carry-over Substrate, New Skin Carry-over Skin, New Substrate Carry-over Skin, Carry-over Substrate (new design) 3.3.1 Short Term Heat, Humidity and Cold Cycle 1 full assembly; 2 required if new technology

38、X X X 3.3.2 Long Term Heat Exposure / Sun Load 1 full assembly; 2 required if new technology X X X 3.3.3 Color Stability 1 specimen taken from para 3.3.2 X 3.3.4 Cold Flexibility 3 test specimens taken from para 3.3.2 X 3.3.5 Elongation at Break 6 test specimens (3 latitudinal and 3 longitudinal) ta

39、ken from para 3.3.2 X 3.4.1 Initial Bond Strength 5 test specimens X X X 3.4.2 After Aging Bond Strength 5 test specimens X X X 3.5 Indentation and Recovery 3 test specimens X X 3.6.1 Resistance to Fade 2 test specimens X only for new colors only for new colors 3.7 Original Elongation 6 test specime

40、ns (3 latitudinal and 3 longitudinal) X 3.8 Fogging 3 test specimens X X 3.9 Flammability* 5 test specimens X X X 3.10 Odor 1 test specimen per condition X X 3.11 Resistance to Dynamic Exudation 1 part X X X 3.12 Degree of Soil Transfer to Leather and Polymeric Fabrics 1 test specimen per condition,

41、 per grain X 3.13 Resistance to Migration Staining and Blocking 1 test specimen per condition X 3.14 Soiling and Cleanability 3 test specimens per condition, per grain X 3.15 Resistance to Abrasion 3 test specimens X only for new colors and/or grains 3.16 Resistance to Scuffing 3 test specimens X on

42、ly for new colors and/or grains 3.17 Resistance to Cleaning Agents 1 test specimen per condition X 3.18 Resistance Suntan Lotion and Insect Repellent 1 test specimen per condition X 3.19 Environmental Stress Cracking 4 test specimens X X *Testing depends on whether a 355 x 100 mm sample can be cut out from the part. Bolded Tests may be run on the skin test plaques. All other tests need to be run on parts.