FORD WSD-M1H669-H-2008 FABRIC FLIGHT PATTERN WOVEN JACQUARD HFW TO BE USED WITH FORD WSS-M99P1111-A 《FLIGHT图案的HFW提花机织织物 与标准FORD WSS-M99P1111-A一起使用 列于标准FORD WSD-M1H669-A上》.pdf

《FORD WSD-M1H669-H-2008 FABRIC FLIGHT PATTERN WOVEN JACQUARD HFW TO BE USED WITH FORD WSS-M99P1111-A 《FLIGHT图案的HFW提花机织织物 与标准FORD WSS-M99P1111-A一起使用 列于标准FORD WSD-M1H669-A上》.pdf》由会员分享，可在线阅读，更多相关《FORD WSD-M1H669-H-2008 FABRIC FLIGHT PATTERN WOVEN JACQUARD HFW TO BE USED WITH FORD WSS-M99P1111-A 《FLIGHT图案的HFW提花机织织物 与标准FORD WSS-M99P1111-A一起使用 列于标准FORD WSD-M1H669-A上》.pdf（5页珍藏版）》请在麦多课文档分享上搜索。

1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Action Revisions 2008 11 19 N-STATUS No Replacement L. Schmalz, FNA / M. Montogomery, FOE 2003 03 20 Revised Para 3.0 inserted ; Para 3.1, 3.2, 3.3, 3.18, 3.19, 4 deleted 1995 01 31 C10460360 Released N.J. Komatsu Printed co

2、pies are uncontrolled Page 1 of 5 Copyright 2008, Ford Global Technologies, Inc. FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, UNLAMINATED WSD-M1H669-A FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, 3mm WSD-M1H669-B1 FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, 6mm WSD-M1H669-B2 FABRIC, FLIGHT PATTERN, WOVEN JACQUARD

3、, 3mm WSD-M1H669-C1 FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, 6mm WSD-M1H669-C2 FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, 6mm WSD-M1H669-D2 FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, HFW WSD-M1H669-G FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, HFW WSD-M1H669-HFABRIC, FLIGHT PATTERN, WOVEN JACQUARD, HFW WSD-M1H

4、669-J FABRIC, FLIGHT PATTERN, WOVEN JACQUARD, HFW WSD-M1H669-KNOT 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 either a knitted fabric or

5、polyurethane film. It can also be backed with an HFW weldable backcoating. 2. APPLICATION WSD-M1H669-A is used for molded headrests and also adhesive coated for use on inner door panels. WSD-M1H669-B1, B2, C1, C2, are used for seat wearing surfaces. WSD-M1H669-D2 is used for adhesively bonded door a

6、nd quarter trim panel applications. WSD-M1H669-G, H, J & K are used for inner door, quarter trim panels and/or as specified on Engineering Drawings. FLIGHT DESIGN WSD-M1H669-A Unlaminated WSD-M1H669-B1 3.0 mm, flame laminated to polyether foam and knitted fabric WSD-M1H669-B2 6.0 mm, flame laminated

7、 to polyether foam and knitted fabric WSD-M1H669-C1 3.0 mm, flame laminated to polyester foam and knitted fabric (EAO use only) WSD-M1H669-C2 6.0 mm, flame laminated to polyester foam and knitted fabric (EAO use only) ENGINEERING MATERIAL SPECIFICATION WSD-M1H669-A/B1/B2/C1/ C2/D2/G/H/J/K Page 2 of

8、5 Copyright 2008, Ford Global Technologies, Inc. WSD-M1H669-D2 6.0 mm, flame laminated to polyether foam WSD-M1H669-G HF-weldable vinyl film, adhesive bonded, or an engineering approved alternative WSD-M1H669-H HF-weldable acrylic backcoating applied by the doctor-knife spreading technique, or an en

9、gineering approved alternative WSD-M1H669-J HF-weldable vinyl backcoating applied by the doctor-knife spreading technique, or an engineering approved alternative WSD-M1H669-K HF-weldable PU backcoating applied by the doctor-knife spreading technique, or an engineering approved alternative 3. REQUIRE

10、MENTS In 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

11、 CONSTRUCTION 3.4.1 Fabric Count, +/- 5 % tolerance (ASTM D 3775) (A, B1, B2, C1, C2, G, H, J, K) Warp 260 ends/10 cm Weft 135 picks/10 cm (D2) Warp 260 ends/10 cm Weft 157 picks/10 cm 3.4.2 Fabric Weight, range (FLTM BN 106-01) (A, B1, B2, C1, C2, G, H, J, K) 335 +/- 20 g/m2(D2) 245 +/- 20 g/m2ENGI

12、NEERING MATERIAL SPECIFICATION WSD-M1H669-A/B1/B2/C1/ C2/D2/G/H/J/K Page 3 of 5 Copyright 2008, Ford Global Technologies, Inc. 3.5 COMPOSITION (ASTM D 629) Fabric 100 % polyester 3.6 YARN CONSTRUCTION (ASTM D 1244) (A, B1, B2, C1, C2, G, H, J, K) Warp 830 dtex f192 (air texturised, semi-dul) Weft 88

13、0 dtex f192 (air texturised, semi-dul) (D2) Warp 550 dtex f128 (air texturised,semi-dull, dehntweed) Weft 550 dtex f128 (air texturised,semi-dull, dehntweed) 3.7 METHOD OF DYEING Yarn dyed or as approved by Materials Engineering 3.8 FINISHED OPERATIONS As approved by Materials Engineering 3.9 REQUIR

14、EMENTS 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 As pecifed inWSD-M9H136-A ENGINEERING MATERIAL SPECIFICATION WSD-M1H669-A/B1/B2/C1/ C2/D2/G/H/J/K Page 4 of 5 Copyright 2008, Ford Global

15、Technologies, Inc. 3.12 REQUIREMENTS FOR THE FLAME LAMINATED MATERIAL 3.12.1 Thickness, range (ASTM D 1777, circular presser foot area 645 mm2, 2.8 g Force, 43 Pa pressure) WSD-M1H669-B1 3.0 +/- 1.0 mm WSD-M1H669-B2 6.0 +/- 1.0 mmWSD-M1H669-C1 3.0 +/- 1.0 mm WSD-M1H669-C2 6.0 +/- 1.0 mmWSD-M1H669-D2

16、 6.0 +/- 1.0 mm 3.12.2 Weight, min WSD-M1H669-B1 475 +/- 40 g/m2WSD-M1H669-B2 585 +/- 40 g/m2WSD-M1H669-C1 455 +/- 40 g/m2WSD-M1H669-C2 445 +/- 40 g/m2WSD-M1H669-D2 450 +/- 40 g/m23.12.3 Stretch and Set, %, range (B1, B2, C1, C2) Stretch Warp 0 -10 eftSet Warp 0 -5 eft3.12.4 Modulus, max (D2) Strain

17、, 6 % Warp 200 N Weft 80 N3.13 REQUIREMENTS FOR THE BACKCOATED MATERIAL (WSD-M1H669-G) 3.13.1 Weight, min (FLTM BN 106-01) PVC film 100 g/m2Face fabric weight as specified in para 3.4.2. Or an engineering approved alternative. ENGINEERING MATERIAL SPECIFICATION WSD-M1H669-A/B1/B2/C1/ C2/D2/G/H/J/K P

18、age 5 of 5 Copyright 2008, Ford Global Technologies, Inc. 3.14 REQUIREMENTS FOR BACKCOATED MATERIAL (WSD-M1H669-H) 3.14.1 Weight, min (FLTM BN 106-01) Acrylic Backcoating 35 g/m2Face fabric weight as specified in para 3.4.2. Or an Engineering Approved Alternative. 3.15 REQUIREMENTS FOR THE BACKCOATE

19、D MATERIAL (WSD-M1H669-J) 3.15.1 Weight, min (FLTM BN 106-01) PVC Backcoating 40 g/m2Face fabric weight as specified in para 3.4.2. Or an Engineering Approved Alternative. 3.16 REQUIREMENTS FOR THE BACKCOATED MATERIAL (WSD-M1H669-K) 3.16.1 Weight, min (FLTM BN 106-01) PU Backcoating 40 g/m2Face fabr

20、ic weight as specified in para 3.4.2. Or an Engineering Approved Alternative. 3.17 FLAMMABILITY (ISO 3795/SAE J369) Burn rate, max 100 mm/minute Note: Not required on face fabric when used as a fully bonded composite. 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.