FORD WSS-M1H692-D2-2008 FABRIC PHOENIX PATTERN WOVEN JACQUARD 6 mm TO BE USED WITH FORD WSS-M99P1111-A (Shown on FORD WSS-M1H692-A)《凤凰(PHOENIX)图案的6 mm厚提花机织织物 与标准FORD WSS-M99P111.pdf

1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Action Revisions 2008 11 20 N-STATUS No Replacement L. Schmalz, FNA / M. Montogomery, FOE 2003 03 28 Revised Para 3.0 inserted ; Para 3.1, 3.2, 3.3, 3.19 3.20 4 deleted 1995 07 31 Activated C10460395 K. J. Komatsu Printed co

2、pies are uncontrolled Page 1 of 6 Copyright 2008, Ford Global Technologies, Inc. FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, UNLAMINATED WSS-M1H692-A FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, 3 mm WSS-M1H692-B1 FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, 6 mm WSS-M1H692-B2 FABRIC, PHOENIX PATTERN, WOVEN JA

3、CQUARD, 3 mm WSS-M1H692-C1 FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, 6 mm WSS-M1H692-C2 FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, 6 mm WSS-M1H692-D2 FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, HFW WSS-M1H692-G FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, HFW WSS-M1H692-H FABRIC, PHOENIX PATTERN, WOVEN JACQUA

4、RD, HFW WSS-M1H692-J FABRIC, PHOENIX PATTERN, WOVEN JACQUARD, HFW WSS-M1H692-K NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by these specifications is a woven jacquard polyester face fabric which can be flame laminated to polyester or polyether urethane foam and backed with a knitted

5、fabric. It can also be backed with an HFW weldable backcoating. 2. APPLICATION WSS-M1H692-A is used for molded headrests and also adhesive coated for use on inner door panels. WSS-M1H692-B1, B2, C1, C2 are used for seat wearing surfaces. WSS-M1H692-D2 is used for adhesively bonded door quarter trim

6、panel applications. WSS-M1H692-G, H, J, K are used for inner door, quarter trim panels and/or as specified on Engineering Drawings. PHOENIX PATTERN WSS-M1H692-A Unlaminated WSS-M1H692-B1 3.0 mm, flame laminated to polyether foam and knitted fabric. WSS-M1H692-B2 6.0 mm, flame laminated to polyether

7、foam and knitted fabric. WSS-M1H692-C1 3.0 mm, flame laminated to polyester foam and knitted fabric (EAO use only). WSS-M1H692-C2 6.0 mm, flame laminated to polyester foam and knitted fabric (EAO use only). WSS-M1H692-D2 6.0 mm, flame laminated to polyester foam ENGINEERING MATERIAL SPECIFICATION WS

8、S-M1H692-A/B1/B2/C1/C2/ D2/G/H/J/K Page 2 of 6 Copyright 2008, Ford Global Technologies, Inc. WSS-M1H692-G HF-weldable vinyl film, adhesive bonded, or an engineering approved alternative. WSS-M1H692-H HF-weldable acrylic backcoating applied by the doctor-knife spreading technique, or an engineering

9、approved alternative. WSS-M1H692-J HF-weldable vinyl backcoating applied by the doctor-knife spreading technique, or an engineering approved alternative. WSS-M1H692-K HF-weldable PU backcoating applied by the doctor-knife spreading technique, or an engineering approved alternative. 3. REQUIREMENTS I

10、n addition to the requirements listed herein, the fabric shall meet all requirements of WSB-M8P1-H. 3.0 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.4 FABRIC CONSTR

11、UCTION 3.4.1 Fabric Count, +/- 5 % tolerance (ASTM D 3775) Warp 180 ends/10 cm Weft 155 picks/10 cm 3.4.2 Fabric Weight, range 300 - 340 g/m2(FLTM BN 106-01) 3.5 COMPOSITION (ASTM D 629) Fabric 100 % Polyester 3.6 YARN CONSTRUCTION (ASTM D 1244) Warp 830 +/- 50 dtex f 192 +/- 15 (polyester, dul, rou

12、nd, air texturised). Weft 830 +/- 50 dtex f 192 +/- 15 (polyester, dul, round, air texturised). ENGINEERING MATERIAL SPECIFICATION WSS-M1H692-A/B1/B2/C1/C2/ D2/G/H/J/K Page 3 of 6 Copyright 2008, Ford Global Technologies, Inc. 3.7 METHOD OF DYEING Yarn dyed and spun dyed or as approved by Materials

13、Engineering. 3.8 FINISHED OPERATIONS As approved by Materials Engineering. 3.9 REQUIREMENTS FOR POLYESTER FOAM As specified in WSD-M2D43-A4. 3.10 REQUIREMENTS FOR POLYETHER FOAM As specified in WSD-M2D43-A2. 3.11 REQUIREMENTS FOR THE BACKING FABRIC (C1,C2) As pecifed inWSD-M9H136-A. 3.12 REQUIREMENT

14、S FOR THE As pecifed in BACKING FABRIC (B1,B2) ESD-M9H111-B. 3.13 REQUIREMENTS FOR THE FLAME LAMINATED MATERIAL 3.13.1 Thickness, range (ASTM D 1777, circular presser foot area 645 mm2, 2.8 g Force, 43 Pa pressure) WSS-M1H692-B1 3.0 +/- 1.0 mm WSS-M1H692-B2 6.0 +/- 1.0 mmWSS-M1H692-C1 3.0 +/- 1.0 mm

15、 WSS-M1H692-C2 6.0 +/- 1.0 mmWSS-M1H692-D2 6.0 +/- 1.0 mm 3.13.2 Weight, min WSS-M1H692-B1 470 +/- 40 g/m2WSS-M1H692-B2 580 +/- 40 g/m2WSS-M1H692-C1 450 +/- 40 g/m2WSS-M1H692-C2 540 +/- 40 g/m2WSS-M1H692-D2 480 +/- 40 g/m2ENGINEERING MATERIAL SPECIFICATION WSS-M1H692-A/B1/B2/C1/C2/ D2/G/H/J/K Page 4

16、 of 6 Copyright 2008, Ford Global Technologies, Inc. 3.13.3 Stretch & Set, range (SAE J855) Stretch Warp 1 -10 %eftSet Warp 0 -5 %eft3.13.4 Modulus, max (D2) (6 % strain) Warp 100 N Weft 150 N 3.14 REQUIREMENTS FOR THE BACKCOATED MATERIAL (WSS-M1H692-G) 3.14.1 Weight, min (FLTM BN 106-01) PVC film 1

17、00 g/m2Face fabric weight as specified in para 3.4.2. Or an engineering approved alternative. 3.15 REQUIREMENTS FOR BACKCOATED MATERIAL (WSS-M1H692-H) 3.15.1 Weight, min (FLTM BN 106-01) Acrylic Backcoating 35 g/m2Face fabric as specified in para 3.4.2. Or an engineering approved alternative. ENGINE

18、ERING MATERIAL SPECIFICATION WSS-M1H692-A/B1/B2/C1/C2/ D2/G/H/J/K Page 5 of 6 Copyright 2008, Ford Global Technologies, Inc. 3.16 REQUIREMENTS FOR THE BACKCOATED MATERIAL (WSS-M1H692-J) 3.16.1 Weight, min (FLTM BN 106-01) PVC Backcoating 40 g/m2Face fabric weight as specified in para 3.4.2. Or an en

19、gineering approved alternative. 3.17 REQUIREMENTS FOR THE BACKCOATED MATERIAL (WSS-M1H692-K) 3.17.1 Weight, min (FLTM BN 106-01) PU Backcoating 40 g/m2Face fabric weight as specified in para 3.4.2. Or an engineering approved alternative. 3.18 FLAMMABILITY (ISO 3795/SAE J369) Burn rate, max 100 mm/mi

20、nute Note: Not required on face fabric when used as a fully bonded composite. 3.19 REQUIREMENTS FOR THE FULLY BONDED DOOR PANELS The fully bonded finished component must satisfy the requirements of engineering component specification S-77FBB-23942-AA or equivalent if specified on the engineering dra

21、wing. In addition to these requirements fabric general performance should not be reduced by the bonding process. Ford Motor Company at its discretion may perform test on the finished components to verify this. Minimum bond strengths will be specified which may vary according to the method of bonding

22、 employed. ENGINEERING MATERIAL SPECIFICATION WSS-M1H692-A/B1/B2/C1/C2/ D2/G/H/J/K Page 6 of 6 Copyright 2008, Ford Global Technologies, Inc. 3.18.1 Peel Adhesion Strength, min (FLTM BN 151-05) Fabric press formed to adhesion coated board. As received 20 N/50mm width After ageing 20 N/50mm width (4

23、h at 100 +/- 2 C, 20 h at 40 +/- 2 C and 98 +/- 2 % R.H.) These bond values are provisional and may be reassessed subsequent to statistical process control. 5. GENERAL INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of these specifications. 5.1 Purchase departments will ensure that both materials defined in these specifications and shipped to any one assembly plant will be produced by one supplier only.