FORD WSS-M5H37-B1-2013 LAMINATE POLYESTER FABRIC POLYURETHANE FOAM PRISM LITE DENSE PATTERN KNIT TO BE USED WITH FORD WSS-M99P1111-A .pdf

1、 ENGINEERING MATERIAL SPECIFICATIONDate Action Revisions Rev. 12013 10 04 N Status No replacement named D. Murtonen, NA 2013 04 29 Activated See Summary of Revisions D. Murtonen FNAControlled document at www.MATS Copyright 2013, Ford Global Technologies, LLC Page 1 of 4 LAMINATE, POLYESTER FABRIC, P

2、OLYURETHANE FOAM, WSS-M5H37-B1 PRISM LITE DENSE PATTERN, KNIT NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a Prism Lite pattern, knit fabric, flame laminated to flame bondable polyether urethane foam. 2. APPLICATION This specification was released originally f

3、or material used as cover material for headliners. Any other applications must be evaluated and approved by the responsible Materials Engineering activity. 3. REQUIREMENTS Materials manufactured to this Specification shall also meet the requirements contained in WSS-M15P27-F. For all test methods, n

4、o individual specimen shall fall below the minimum values specified herein. 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). 3.2 APPEARANCE (FLTM BI 109-01) The color

5、, pattern, and finish shall match the approved Corporate Design master sample, or shall be as specified on the engineering drawing. 3.3 ROLL GOODS QUALITY The laminate shall be uniformly bonded, and the fabric shall not delaminate from the foam during shipping, handling or in-plant processing. 3.4 C

6、OMPOSITION (ASTM D276) Fabric 100% Polyester Foam Polyether Polyurethane 3.5 FABRIC REQUIREMENTS The following shall be conducted on unbonded fabric 3.5.1 Fabric count (ASTM D3887) Wales 125-145 wales/10 cm Courses 130-150 courses/10 cm ENGINEERING MATERIAL SPECIFICATIONWSS-M5H37-B1Copyright 2013, F

7、ord Global Technologies, LLC Page 2 of 4 3.5.2 Weight (FLTM BN 106-01) Fabric face only 80 - 110 g/m23.6 FOAM REQUIREMENTS The foam shall be polyether polyurethane and shall conform to ASTM D3574 USUEJ2. The following test shall be conducted on foam removed from the finished fabric/foam laminate or

8、from surrogate foam samples when the laminate is less than 4 mm thick. 3.6.1 Tensile Strength 80 kPa min (ASTM D3574, Test E) 3.6.2 Steam Autoclave Aging (ASTM D3574, Test E and Test J2) Cut out 25 mm wide strips from the fabric/foam laminate. By hand, carefully peel or cut the foam away from the fa

9、bric taking care to minimize damage to the foam. Die cut specimens for tension test to recover the thickness. Expose them to the required autoclave aging and test. 3.6.2.1 Retained Tensile Strength 70% min of original (After 2 autoclave cycles for 10 hours total exposure) 3.7 FABRIC-FOAM LAMINATE RE

10、QUIREMENTS 3.7.1 Thickness Production samples specified As on the Engineering Drawing Source Approval and Master samples 2.2 0.5mm 3.7.2 Ply Adhesion, both directions 6N min (FLTM BN 151-05) The fabric shall not separate clearly from the foam surface (cohesive failure of foam required). In the case

11、when sustained peel cannot be obtained due to the foam tearing or breaking away from the fabric, ply adhesion shall be considered acceptable if the peak load prior to break exceeds the above minimum requirement. If the laminate is less than 4 mm thick and a numerical ply adhesion value cannot be sat

12、isfactorily obtained, ply adhesion shall be acceptable if the fabric cannot be separated cleanly from the foam. 3.7.3 Resistance to Abrasion 150 cycles (SAE J948, 500g load, CS-10 wheels) No evidence of excessive surface deterioration. The resistance to abrasion of production material shall be equal

13、 to or better than the exhibited by the Fabric Proposal approved by the Materials Engineering Activity. ENGINEERING MATERIAL SPECIFICATIONWSS-M5H37-B1Copyright 2013, Ford Global Technologies, LLC Page 3 of 4 3.7.4 Strength Properties 3.7.4.1 Breaking Strength 35N min (ASTM D5034 Grab Method, 305 mm/

14、min speed of testing, Average of 5 samples in each Direction) 3.7.4.2 Ultraviolet Deterioration (FLTM BO 116-01, 225.6 kJ/m2) 3.7.4.2.1 Retained tensile strength 35 % of original (ASTM D5034 Grab Method, value, min 305 mm/min speed of testing, Average of 5 samples in each Direction) 3.7.5 Color Prop

15、erties 3.7.5.1 Resistance to Fade (FLTM BO 116-01, ISO 105-A02/ AATCC Evaluation Procedure 1) 225.6 kJ/m2 Rating 4 min 451.6 kJ/m2 Rating 3 min 3.7.5.2 Resistance to Heat Aging Rating 4 min (7 days at 1002C, ISO 105-02/ AATCC Evaluation Procedure 1) No individual yarn or combination of yarns shall e

16、xhibit fiber deterioration or color tone change in excess of the above rating. Backcoatings, if applied, shall exhibit only slight color change and no deterioration. 3.7.5.3 Resistance to Crocking (FLTM BN 107-01, AATCC Evaluation Procedure 2) Dry Rating 4 min Wet Rating 4 min 3.7.5.4 Resistance to

17、Bleeding and Perspiration Rating 4 min (FLTM AN 101-01/AATCC Evaluation Procedure 2) 3.7.5.5 Soiling and Cleanability Rating 3 min (FLTM BN 112-08, grease, soil and coffee only) In addition, marks with an artists charcoal crayon must be easily removed, using an approved brand interior trim cleaner,

18、without serious damage to the face fabric. The performance of production material shall be equal to or better than that exhibited by the sample originally approved for production by the Materials Engineering Activity. ENGINEERING MATERIAL SPECIFICATIONWSS-M5H37-B1Copyright 2013, Ford Global Technolo

19、gies, LLC Page 4 of 4 3.8 ODOR Rating 3 max (FLTM BO 131-03) 3.9 FOGGING (SAE J1756, 3 hrs at100C heating, 21C cooling plate, Post test conditioning 1 hour and 16 hrs) Fog number 70 min Formation of a clear film, droplets or crystals is cause for rejection. 3.10 FLAMMABILITY (ISO 3795/SAE J369) Burn

20、 Rate 100 mm/ minute max The fabric/foam laminate must be 100% bonded and must meet the above requirement. 4. GENERAL INFORMATION This information given below is provided for clarification and assistance in meeting the requirements of this specification. Contact for questions concerning Engineering Material Specifications. 5. SUMMARY OF REVISIONS 2013 04 29 Suffix was updated from A to B1 to accommodate updated submissions from supplier for Color Durability sign-offs