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

上传人:brainfellow396 文档编号:745179 上传时间:2019-01-14 格式:PDF 页数:4 大小:29.74KB
下载 相关 举报
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_第1页
第1页 / 共4页
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_第2页
第2页 / 共4页
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_第3页
第3页 / 共4页
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_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

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.

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4170-2006 Aerospace series Paints and varnishes Test method for measurement of resistance to cold crack temperature cycle Edition P 1《航空航天系列.油漆涂料试验方法阻力测定冷裂缝温度循环.P1版》.pdf AECMA PREN 4170-2006 Aerospace series Paints and varnishes Test method for measurement of resistance to cold crack temperature cycle Edition P 1《航空航天系列.油漆涂料试验方法阻力测定冷裂缝温度循环.P1版》.pdf
  • AECMA PREN 4171-2005 Aerospace series Paints and varnishes Test method for determination of phosphoric acid index Edition P 1《航空航天系列.油漆涂料试验方法磷酸含量测定.P1版》.pdf AECMA PREN 4171-2005 Aerospace series Paints and varnishes Test method for determination of phosphoric acid index Edition P 1《航空航天系列.油漆涂料试验方法磷酸含量测定.P1版》.pdf
  • AECMA PREN 4172-1999 Aerospace Series Lockbolts Protruding Head Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized Metric Series Classification 1 100 MPa (at Ambient Te.pdf AECMA PREN 4172-1999 Aerospace Series Lockbolts Protruding Head Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized Metric Series Classification 1 100 MPa (at Ambient Te.pdf
  • AECMA PREN 4173-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized Metric Series Classification 1 100.pdf AECMA PREN 4173-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized Metric Series Classification 1 100.pdf
  • AECMA PREN 4174-1999 Aerospace Series Collars Swage Locking Sheartype in Aluminium Alloy 2024 Anodized or Chromated Metric Series Edition P 1《航空航天系列.阳极氧化或铬酸盐处理铝合金2024、铆紧剪式垫圈 米制系列》.pdf AECMA PREN 4174-1999 Aerospace Series Collars Swage Locking Sheartype in Aluminium Alloy 2024 Anodized or Chromated Metric Series Edition P 1《航空航天系列.阳极氧化或铬酸盐处理铝合金2024、铆紧剪式垫圈 米制系列》.pdf
  • AECMA PREN 4175-1999 Aerospace Series Collars Flanged Swage Locking Sheartype in Titanium TI-P99002 Metric Series Edition P 1《空航天系列 钛 TI-P99002、法兰式铆紧剪式垫圈 米制》.pdf AECMA PREN 4175-1999 Aerospace Series Collars Flanged Swage Locking Sheartype in Titanium TI-P99002 Metric Series Edition P 1《空航天系列 钛 TI-P99002、法兰式铆紧剪式垫圈 米制》.pdf
  • AECMA PREN 4176-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head or Protruding Head Tension- Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized or wit.pdf AECMA PREN 4176-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head or Protruding Head Tension- Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized or wit.pdf
  • AECMA PREN 4178-1994 Aerospace Series Screws Pan Head Six Lobe Recess Coarse Tolerance Normal Shank Medium Length Thread in Titanium Alloy Anodized MoS2 Lubricated Classification  .pdf AECMA PREN 4178-1994 Aerospace Series Screws Pan Head Six Lobe Recess Coarse Tolerance Normal Shank Medium Length Thread in Titanium Alloy Anodized MoS2 Lubricated Classification .pdf
  • AECMA PREN 4179-2008 Aerospace series Qualification and approval of personnel for non-destructive testing Edition P4《航空航天系列.无损检测人员的合格与核准》.pdf AECMA PREN 4179-2008 Aerospace series Qualification and approval of personnel for non-destructive testing Edition P4《航空航天系列.无损检测人员的合格与核准》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1