FORD WRS-M1H1229-A-2016 FABRIC OMNI WOVEN 43% PIR PCR UNLAMINATED TO BE USED WITH FORD WSS-M99P1111-A .pdf

上传人:Iclinic170 文档编号:748647 上传时间:2019-01-14 格式:PDF 页数:2 大小:47.12KB
下载 相关 举报
FORD WRS-M1H1229-A-2016 FABRIC OMNI WOVEN 43% PIR PCR UNLAMINATED  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第1页
第1页 / 共2页
FORD WRS-M1H1229-A-2016 FABRIC OMNI WOVEN 43% PIR PCR UNLAMINATED  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev. 3 2016 05 19 N Status A/A2 No future usage D. Murtonen, NA 2015 06 09 Released A20 No Back Coat Version D. Murtonen, FNA 2012 03 28 Activated M.Dumitrescu, NA Controlled document at www.MATS Copyright 2016, Ford Global Technologies, LLC

2、Page 1 of 2 FABRIC, OMNI, WOVEN, WRS-M1H1229-A 43% PIR/PCR UNLAMINATED NOT TO BE USED FOR NEW DESIGN FABRIC, OMNI, WOVEN, WSS-M1H1229-A2 UNLAMINATED NOT TO BE USED FOR NEW DESIGN FABRIC, OMNI, WOVEN, 43% MINIMUM PIR/PCR, NO BACK COAT WRS-M1H1229-A20 UNLAMINATED 1. SCOPE The material defined is a wov

3、en polyester face fabric. Material conforming to WRS-M1H1229-A and A20 contains 43% PIR/PCR (Post industrial/post consumer) recycled yarn. 2. APPLICATION This specification was released originally for material used as an interior trim fabric for 2013 Fusion seat insert and/or bolster for EU and Chin

4、a production. The fabric was originally approved as trilaminated with foam and backing fabric/scrim. 3. REQUIREMENTS 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).

5、Materials with recycled content as defined by WRS-M99P42-A2 (Textile Materials, Identification of Recycled Content) should be used whenever technically feasible. 3.1.1 WRS-M1H1229-A. This specification must contain 43% minimum recycled content as defined by WRS-M99P42-A2/latest. The remaining portio

6、n of the material can come from virgin sources. 3.1.2 WRS-M1H1229-A20. This specification must contain 43% minimum recycled content as defined by WRS-M99P42-A2/latest. The remaining portion of the material can come from virgin sources. 3.1.3 WSS-M1H1229-A2. This specification is based on virgin mate

7、rials. 3.1.4 In addition to the requirements listed herein, the fabric shall meet all requirements of WSS-M8P18-A1/A2/A3/A4 as applicable. 3.2 FABRIC CONSTRUCTION 3.2.1 Fabric Count, -10 /+ 10 % tolerance (ASTM D3775) Warp 905 / 10 cm Weft 283/ 10 cm ENGINEERING MATERIAL SPECIFICATION WRS-M1H1229-A/

8、A20 WSS-M1H1229-A2 Copyright 2016, Ford Global Technologies, LLC Page 2 of 2 3.2.2 Fabric Weight, -10 + 10 % tolerance (FLTM BN 106-01) WRS-M1H1229-A and WSS-M1H1229-A2 Face fabric 320 g/m2 Backcoat 55g/m2 Total Weight 375 g/m2 WRS-M1H1229-A20 Face fabric 320 g/m2 3.3 COMPOSITION (ASTM D629) WRS-M1H

9、1229-A and WSS-M1H1229-A2 Fabric 100% polyester Backcoating Acrylic Backing fabric/scrim 100% polyester, Circular knit WRS-M1H1229-A20 Fabric 100% polyester Backing fabric/scrim 100% polyester, Circular knit 3.4 YARN CONSTRUCTION (ASTM D1244) A/A20 A2 Warp 167 Dtex x1 167 Dtex x1 (polyester, false t

10、wist, (polyester false twist texturized) Texturized 100% recycled yarn) Weft 167Dtex x2, 167 Dtex x2, (polyester, false twist (polyester false twist texturized) Texturized 100% recycled yarn) 3.5 METHOD OF DYEING Solution dyed or as approved by Materials Engineering, 3.6 FINISHED OPERATIONS Wash, co

11、ating, drying, brushing (optional 4. GENERAL INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of this specification. Contact for questions concerning Engineering Material Specifications. 4.1 Purchase departments will ensure that the ma

12、terial defined in this specification and shipped to any one assembly plant will be produced by one supplier only. 4.2 If yarn is locally sourced it must meet the above fabric construction, composition and yarn construction. The fabric must also meet the requirements of WSS-M8P18-A1/A2/A3/A4. 4.3 Global strategy for this fabric is to use tri-laminate/foam & scrim construction in all regions

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 4608-002-2005 Aerospace Series Cable Electrical Fire Resistant Single and Twisted Multicore Assembly Screened (Braided) and Jacketed Operating Temperatures between - .pdf ASD-STAN PREN 4608-002-2005 Aerospace Series Cable Electrical Fire Resistant Single and Twisted Multicore Assembly Screened (Braided) and Jacketed Operating Temperatures between - .pdf
  • ASD-STAN PREN 4608-003-2004 Aerospace series Cables electrical fire resistant Single and twisted multicore assembly screened (braided) and jacketed Operating temperature between - .pdf ASD-STAN PREN 4608-003-2004 Aerospace series Cables electrical fire resistant Single and twisted multicore assembly screened (braided) and jacketed Operating temperature between - .pdf
  • ASD-STAN PREN 4608-004-2012 Aerospace series Single and twisted multicore assembly screened (braided) and jacketed Operating temperatures between 65 and 260 Part 004 DW family - Li.pdf ASD-STAN PREN 4608-004-2012 Aerospace series Single and twisted multicore assembly screened (braided) and jacketed Operating temperatures between 65 and 260 Part 004 DW family - Li.pdf
  • ASD-STAN PREN 4608-005-2005 Aerospace series Cable electrical fire resistant Single and twisted multicore assembly screened (braided) and jacketed Operating temperatures between - .pdf ASD-STAN PREN 4608-005-2005 Aerospace series Cable electrical fire resistant Single and twisted multicore assembly screened (braided) and jacketed Operating temperatures between - .pdf
  • ASD-STAN PREN 4610-2003 Aerospace Series Pipe coupling 80 degrees 30 inches in titanium alloy Elbows 45 degrees with thrust wire nut (Edition P 1)《航空航天系列 钛合金制80°30 '管接头 带止推金属丝帽的45°.pdf ASD-STAN PREN 4610-2003 Aerospace Series Pipe coupling 80 degrees 30 inches in titanium alloy Elbows 45 degrees with thrust wire nut (Edition P 1)《航空航天系列 钛合金制80°30 '管接头 带止推金属丝帽的45°.pdf
  • ASD-STAN PREN 4611-002-2004 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 002 General (Edition P 1)《航空航天系列 单芯和多芯配件XLETFE类通.pdf ASD-STAN PREN 4611-002-2004 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 002 General (Edition P 1)《航空航天系列 单芯和多芯配件XLETFE类通.pdf
  • ASD-STAN PREN 4611-002-2017 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 002 General (Edition P 2).pdf ASD-STAN PREN 4611-002-2017 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 002 General (Edition P 2).pdf
  • ASD-STAN PREN 4611-003-2004 Aerospace series Cables electrical for general purpose single and multicore assembley XLETFE Family Part 003 Tin plated copper Operating temperatures be.pdf ASD-STAN PREN 4611-003-2004 Aerospace series Cables electrical for general purpose single and multicore assembley XLETFE Family Part 003 Tin plated copper Operating temperatures be.pdf
  • ASD-STAN PREN 4611-003-2017 Aerospace series Cables electrical for general purpose single and multicore assembley XLETFE Family Part 003 Tin plated copper Operating temperatures be.pdf ASD-STAN PREN 4611-003-2017 Aerospace series Cables electrical for general purpose single and multicore assembley XLETFE Family Part 003 Tin plated copper Operating temperatures be.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