FORD WSS-M15P34-C1-2011 PERFORMANCE INTERIOR TRIM APPLIQUES HIGH WEAR TO BE USED WITH FORD WSS-M99P1111-A 《内部装饰嵌花的高磨损性能 与福特WSS-M99P1111-A 一起使用[使用 福特WSS-M15P34-D]》.pdf

1、 ENGINEERING MATERIAL SPECIFICATIONDate Action Revisions 2011 01 04 N-STATUS Replaced by WSS-M15P34-D S. Draheim, NA 2007 07 16 Revised Non-technical changes in paragraphs 1, 2, 3 and 4 J. Crist 2003 02 24 Activated L. Soreide Printed copies are uncontrolled Copyright 2011, Ford Global Technologies,

2、 LLC Page 1 of 6 PERFORMANCE, INTERIOR TRIM APPLIQUES, HIGH WEAR WSS-M15P34-C1 PERFORMANCE, INTERIOR TRIM APPLIQUES, LOW WEAR WSS-M15P34-C2 NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by these specifications is a high or low wear interior trim appliqu. 2. APPLICATION These specificat

3、ions were released originally for appliques used on instrument panels and interior door trim panels. A low wear application is a part that will not be in contact by the customer on a continual basis, such as the area behind the steering column or in a vertical area on the instrument panel that is no

4、t located near control adjustments . A high wear application is a part that is in contact continually, such as the door panel, console, the radio or any other control adjustments. 3. REQUIREMENTS In addition to the requirements listed, parts which are heat bonded shall also meet all applicable requi

5、rements of WSS-M15P4-E and any individual material specification, such as plastic substrate or paint over plastic, where applicable. Any hot stamp foil must be stampable over itself with no loss in physical properties. The paint system for painted plastic shall, in all cases, be compatible with both

6、 the decorative coating and the painted substrate and give results better than required by these specifications. 3.1 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). Part

7、 producers using this material in their products, must use Ford approved materials and must conform to a process control plan which has been approved by STA and/or the relevant Materials Activity. 3.2 PREPARATION OF PARTS/TEST SPECIMENS When it is not feasible to test the actual part because of size

8、, laboratory panels may be substituted. Test panels shall be processed concurrently with production parts and/or shall be representative of production parts with respect to all processes, including substrate, surface treatment, cleaning primer, film thickness, color coat and cure cycles. 3.3 INITIAL

9、 HARDNESS Color coat shall be sufficiently cured at time of packing to withstand normal handling and shipping without damage. ENGINEERING MATERIAL SPECIFICATIONWSS-M15P34-C1/C2 Printed copies are uncontrolled Copyright 2011, Ford Global Technologies, LLC Page 2 of 6 3.4 APPEARANCE (FLTM BI 109-01) T

10、he color, pattern and finish shall match approved Design Center master sample or shall be specified on the engineering drawing. In addition, all decorative coatings must provide a uniform continuous coating and design pattern with complete hiding, free from thin spots, blisters, and cracks. 3.5 INIT

11、IAL ADHESION Grade 0 (FLTM BI 106-01, Method B) No flaking, chipping, blistering or delamination. 3.6 ABRASION RESISTANCE, TABER (SAE J948) (C1) High Wear: 1,000 g load, CS-10 wheels 500 cycles (C2) Low Wear: 500 g load, CS-10 wheels 100 cycles The following conditions shall be cause for rejections:

12、 . Any visual wear-through to the substrate. . Any loss of the grained effect on woodgrain decorated parts. 3.7 MAR RESISTANCE, TABER, min 300 cycles (SAE J948, 250 g load, CS “0“ wheels) No loss of grain or color definition in the wear pattern. 3.8 DRAWABILITY The coatings must have the necessary f

13、lexibility and elongation characteristics to allow them to be formed in drawing operations without loss of embossing, delamination, color change, crazing or cracking. 3.9 FOGGING (SAE J1756, 3 h at 100 C heating, 21 C cooling plate, post test conditioning 1 h) Fog Number, min 70 Formation of clear f

14、ilm, droplets or crystals is cause for rejection. 3.10 WATER RESISTANCE 24 h Test Method: Immerse the part/test specimen in distilled or deionized water maintained at 32 +/- 2 C per FLTM BI 104-01. Remove parts from the water and immediately scribe an X through the film surface to the substrate. Dry

15、 the scribe area with a paper towel, cloth or air pressure and immediately apply, with firm thumb pressure, a minimum of 1290 mm2of 3M tape 898, 25 mm wide. Remove the tape by pulling one end at a 90 angle at a moderate speed. The following conditions shall be basis for rejection: . Removal of film

16、beyond 1.6 mm from any scribe line. Any evidence of blistering after tape removal. ENGINEERING MATERIAL SPECIFICATIONWSS-M15P34-C1/C2 Printed copies are uncontrolled Copyright 2011, Ford Global Technologies, LLC Page 3 of 6 3.11 RESISTANCE TO CLEANING AGENTS, min Rating 4 (AATCC Evaluation Procedure

17、 3) Only slight softening, dulling, color transfer or color change is allowed. Shall not blister or show evidence of loss of adhesion. Test Method: Place the part/test specimen in a 600 mL beaker half full of the following cleaning agents (see also para 4.2) for one hour at 23 +/- 2 C minimum. Then

18、remove the test specimen, wipe it with a soft cloth and examine the cloth for evidence of color transfer and the film surface for evidence of degradation. 1. Petroleum Naphtha-Aliphatic type 2. Window cleaner with ammonia 3. All purpose cleaner 4. IPA/water 50% v/v 3.12 RESISTANCE TO FADE, min (SAE

19、J1885 and ISO 105-A02/AATCC Evaluation Procedure 1) The specimen size shall be 60 x 150 mm with 1/3 of the area protected from exposure. Low sunload exposure - 225.6 kJ/m2*Rating 4 - Door and quarter trim panel below armrest. Moderate sunload exposure - 488.8 kJ/m2*Rating 4 - Door and quarter trim p

20、anel armrest and above. High sunload area - 1015.2 kJ/m2*Rating 4 Horizontal or vertical parts AT OR ABOVE THE BELT-LINE (e.g. sail; A-, B-, C-, and D-pillars; upper quarter panels; and roof-rail moldings): * There shall be a maximum of 15% gloss loss from original as determined by ASTM D 523. Parts

21、 shall also be completely free from evidence of cracking, checking, blistering or peeling. 3.13 WATER RESISTANCE AFTER WEATHERING After the part has been exposed to artificial weathering exposure as specified in para 3.12, it shall be tested for water resistance as described in para 3.10. If part fa

22、ils, retest after 5 minutes. The following conditions shall be basis for rejection: . Removal of coating beyond 3.2 mm from any scribe line. . Any evidence of blistering. ENGINEERING MATERIAL SPECIFICATIONWSS-M15P34-C1/C2 Printed copies are uncontrolled Copyright 2011, Ford Global Technologies, LLC

23、Page 4 of 6 3.14 LONG TERM HEAT EXPOSURE After exposure, the appliqu on the part shall not exhibit evidence of curling, edge lifting, delamination or blistering from substrate. In addition, the parts shall not exhibit any objectionable warpage, surface defects, or color change. Test one previously u

24、nexposed assembly as follows: 3.14.1 Horizontal or vertical parts AT OR ABOVE THE BELT-LINE (e.g. sail; A-, B-, C-, and D-pillars; upper quarter panels; and roof-rail moldings): . 7 days at 100 +/- 2 C 3.14.2 Horizontal or vertical parts BELOW THE BELT-LINE (e.g., lower door panels, lower quarter tr

25、im panels, consoles). . 7 days at 90 +/- 2 C 3.14.3 Scuff plates, kick panels and other non-sun loaded floor level parts. . 7 days at 80 +/- 2 C 3.15 SHORT TERM HEAT, HUMIDITY AND COLD CYCLE After exposure to the cycle of the test conditions listed below, the appliqu on the part shall not exhibit ev

26、idence of curling, edge lifting, delamination or blistering from the part substrate. In addition, the part shall not exhibit any objectionable warpage or surface defects. Test three previously unexposed assemblies: 3.15.1 Horizontal or vertical parts AT OR ABOVE THE BELT-LINE (e.g. sail; A-, B-, C-,

27、 and D-pillars; upper door panels, upper quarter trim panels; and roof-rail moldings): . 5 h at -40 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at 100 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 2 h at 50 +/- 2 C and 95 +/- 5% R.H. . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at -40 +/- 2 C . 3

28、0 min at 23 +/- 2 C and 50% R.H. . 5 h at 100 +/- 2 C 3.15.2 Horizontal or vertical parts BELOW THE BELT-LINE (e.g., lower door panels, lower quarter trim panels, consoles). . 5 h at -40 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at 90 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 2 h at 50 +

29、/- 2 C and 95 +/- 5% R.H. . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at -40 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at 90 +/- 2 C ENGINEERING MATERIAL SPECIFICATIONWSS-M15P34-C1/C2 Printed copies are uncontrolled Copyright 2011, Ford Global Technologies, LLC Page 5 of 6 3.15.3 Scuff plates,

30、 kick panels and other non-sun loaded floor level parts. . 5 h at -40 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at 80 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H. . 2 h at 50 +/- 2 C and 95 +/- 5% R.H. . 30 min at 23 +/- 2 C and 50% R.H. . 5 h at -40 +/- 2 C . 30 min at 23 +/- 2 C and 50% R.H

31、. . 5 h at 80 +/- 2 C High sunload area - increase heat in humidity portion of cycle to 90 +/- 2 C. 3.16 FLAMMABILITY, max 100 mm/minute (ISO 3795/SAE J369) In addition, the test specimen shall not exhibit any flashing or sudden flaming on either surface in excess of the above maximum value. 3.17 OD

32、OR, max Rating 2 (SAE J1351/FLTM BO 131-01) 3.18 BONDED BUTTONS, EMBLEMS, ETC., min Tensile 205 kPa (FLTM BN 121-04) Peel 1.1 N/mm width (FLTM BN 151-05) Buttons shall conform to the tensile requirement; linear bonded emblems shall conform to the peel requirement. 3.19 RESISTANCE TO SCRATCHING, MAX

33、Rating 1 (FLTM BN 108-13, 6 N force) 3.20 RESISTANCE TO SUNTAN LOTION and Insect Repellent, max Rating 3 (DVM-0036-MA, DVM-0039-MA) 3.21 FLEXIBILITY Required for substrates with a flexural modulus less than 450 MPa. 3.21.1 Room Temperature (23 +/- 2 C) Test Method: Cut 13 x 100 mm sample from plaque

34、. Grasp sample firmly at each end, place over mandrel painted side up, and bend around mandrel 180 min. Use 25 mm mandrel. ENGINEERING MATERIAL SPECIFICATIONWSS-M15P34-C1/C2 Printed copies are uncontrolled Copyright 2011, Ford Global Technologies, LLC Page 6 of 6 3.21.2 Cold Temperature Test Method:

35、 Cut 13 x 100 mm sample from plaque. Place sample, mandrel and gloves into a freezer at -30 +/- 2 C for 4 h min. Open freezer, put on gloves and grasp sample firmly at each end, place over mandrel painted side up, and bend around mandrel 180 min. Use 25 mm mandrel. No cracking of painted surface is

36、allowed when bent over 25 mm mandrel. 3.22 RESISTANCE TO DYNAMIC EXUDATION The system shall resist migration of ultraviolet light and heat stabilizers, plasticizers or any other substance that will exude to the surface of the tested specimen. No color change, whitening, blooming or spewing less than

37、 AATCC Rating 4-5. 3.22.1 Condensing Humidity Test Rating 4 - 5 (FLTM BI 104-02, Method A, 168 h, ISO 105-A02/AATCC Evaluation Procedure) 3.22.2 Heat Aging Rating 4 - 5 (7 days at 45 +/- 2 C) 4. GENERAL INFORMATION The information given below is provided for clarification and assistance in meeting t

38、he requirements of these specifications. 4.1 Each combination of decorative appliqu and painted/unpainted substrate must be submitted for approval. If a paint, paint source, appliqu source, plastic or plastic source is changed, a new part submission must be made. 4.2 CLEANING AGENTS (see para 3.11) 1. Petroleum naphtha-aliphatic type 2. Window cleaner with ammonia E4AZ-19C507-AA* 3. All purpose cleaner E0AZ-19526-AA* 4. Isopropyl alcohol/water 50% v/v * or Ford Motor Company recommended equivalents