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    FORD ESB-M1H345-A-2009 BODYCLOTH CAMDEN PATTERN (VELOUR) TO BE USED WITH FORD WSS-M99P1111-A 《CAMDEN图案(丝绒)车身布 与标准FORD WSS-M99P1111-A一起使用 》.pdf

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    FORD ESB-M1H345-A-2009 BODYCLOTH CAMDEN PATTERN (VELOUR) TO BE USED WITH FORD WSS-M99P1111-A 《CAMDEN图案(丝绒)车身布 与标准FORD WSS-M99P1111-A一起使用 》.pdf

    1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Action Revision 2009 01 06 N-STATUS No Replacement B. Haggart, FNA 2003 03 20 Revised Para 3.0 inserted ; Para 3.1, 3.2, 3.3, 3.4, 3.18, 4 deleted 1986 02 14 Released CAP1-DR535711 Printed copies are uncontrolled Page 1 of 4

    2、 Copyright 2009, Ford Global Technologies, Inc. BODYCLOTH, CAMDEN PATTERN (VELOUR) ESB-M1H345-A NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a Camden pattern woven velour bodycloth of good quality and uniform composition. 2. APPLICATION This specification was

    3、released originally for material used as an interior trim fabric for the 1986 Taurus/Sable. 3. REQUIREMENTS 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). 3.5 FABRI

    4、C CONSTRUCTION 3.5.1 Fabric Count, +/- 5 % tolerance (ASTM D 1910) Warp 25.6 ends/cm Fill 13.4 picks/cm 3.5.2 Fabric Weight, g/m2, range 420 - 495 (FLTM BN 106-01) 3.6 COMPOSITION (ASTM D 629) Tolerance as specified in ESB-M8P1-D. Fabric 42 %Nylon 16Ra42 %Polyester Backoating Acrylic ENGINEERING MAT

    5、ERIAL SPECIFICATION ESB-M1H345-A Page 2 of 4 Copyright 2009, Ford Global Technologies, Inc. 3.7 YARN CONSTRUCTION (ASTM D 1244) Warp (A) 29.5 tex Z 551 tpm (nylon, 3.3 d tex, 38 mm staple) x 2 S 354 tpm Warp (B) 29.5 tex Z 709 tpm (polyester, 3.3 d tex, 51 mm staple) x 2 S 394 tpm Warp (C) 29.5 tex

    6、Z 551 tpm (nylon, 3.3 d tex, 38 mm staple) x 2 S 354 tpm Warp (D) 29.5 tex Z 748 tpm (50 percent nylon, 2.5 d tex, 38 mm staple and 50 percent rayon, bright, 1.7 d tex, 40 mm staple) x 2 S 354 tpm Fill 42 tex Z 551 tpm (polyester, 3.3 d tex, 51 mm staple) x 2 S 354 pm 3.8 METHOD OF DYEING Piec 3.9 F

    7、INISHING OPERATIONS Napped & Sheared 3.10 BREAKING STRENGTH, Dry & Wet, N, min (ASTM D 1682, Grab Method, 305 mm/min jaw speed, avg. of 5 samples, each direction) Dry Wet Warp 578 445 Fill 890 800 Test Method for Wet Breaking Strength: Completely immerse sample in clean tap water, 23 +/- 2 C, until

    8、specimen is thoroughly soaked (one or two drops of liquid detergent or soap may be added to assist wetting out). Blot off excess water a test immediately per ASTM D 1682, Grab Method. ENGINEERING MATERIAL SPECIFICATION ESB-M1H345-A Page 3 of 4 Copyright 2009, Ford Global Technologies, Inc. 3.11 SEAM

    9、 STRENGTH, N, min (FLTM BN 119-01, avg. of 5 samples, each direction) Warp 445 Fill 445 3.12 TEAR STRENGTH (TRAPEZOID), Dry & Wet, N, min (ASTM D 5733, avg. of 5 samples, each direction) Dry Wet Warp 53 53 Fill 82 82 Test Method for Wet Tear Strength: Completely immerse sample in clean tap water, 23

    10、 +/- 2 C, until specimen is thoroughly soaked (one or two drops of liquid detergent or soap may be added to assist wetting out). Blot off excess water and test immediately per FLTM BN 22-1. 3.13 STRETCH & SET, %, range (SAE J 855) Strech Set Warp 0 9 0 - 4 Fill 0 7 0 - 3 3.14 SHRINKAGE, %, max (FLTM

    11、 BN 105-01, Water Shrinkage) Warp 5 Fill 3 3.15 STIFFNESS, kg/cm2, max Warp 25 Fill 25 ENGINEERING MATERIAL SPECIFICATION ESB-M1H345-A Page 4 of 4 Copyright 2009, Ford Global Technologies, Inc. 3.16 FLAMMABILITY REQUIREMENT In order to comply with Federal Vehicle Safety Standard No. 302, the materia

    12、ls, portions of components, and composites shall not burn, or transmit a flame across its surface, at a rate of more than 101 mm/min. To demonstrate compliance, the sample size and method of testing shall be in accordance with FLTM BN 24-2. 3.17 FLAMMABILITY TEST PROGRAM Materials, portions of components, and composites governed by this specification must also comply with the requirements of ES-D3AB-11014-AA.


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