FORD WSS-M1H792-A-2008 FABRIC LAUREL PATTERN WOVEN JACQUARD UNLAMINATED TO BE USED WITH FORD WSS-M99P1111-A 《月桂树(LAUREL)图案的不分层提花机织织物 与标准FORD WSS-M99P1111-A一起使用 》.pdf

上传人:dealItalian200 文档编号:752247 上传时间:2019-01-14 格式:PDF 页数:2 大小:19.74KB
下载 相关 举报
FORD WSS-M1H792-A-2008 FABRIC LAUREL PATTERN WOVEN JACQUARD UNLAMINATED  TO BE USED WITH FORD WSS-M99P1111-A  《月桂树(LAUREL)图案的不分层提花机织织物  与标准FORD WSS-M99P1111-A一起使用 》.pdf_第1页
第1页 / 共2页
FORD WSS-M1H792-A-2008 FABRIC LAUREL PATTERN WOVEN JACQUARD UNLAMINATED  TO BE USED WITH FORD WSS-M99P1111-A  《月桂树(LAUREL)图案的不分层提花机织织物  与标准FORD WSS-M99P1111-A一起使用 》.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 Material Name Specification Number Date Action Revisions 2008 12 03 N-STATUS No Replacement L. Schmalz, FNA / M. Montgomery, FOE2003 02 21 Revised Para 3.0 inserted ; Para 3.1, 3.2, 3.3, 3.10, 3.11, 4 deleted 1998 06 08 Activated N.J. KomatPrinted copies are uncon

2、trolled Page 1 of 2 Copyright 2008, Ford Global Technologies, Inc. FABRIC, LAUREL PATTERN, WOVEN JACQUARD, WSS-M1H792-A UNLAMINATED NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a woven jacquard polyester face fabric. 2. APPLICATION This specification was relea

3、sed originally for material used as an interior trim fabric for use in India. 3. REQUIREMENTS In addition to the requirements listed herein, the fabric shall meet all requirements of WSS-M8P18-A1/A2/A3/A4 as applicable. 3.0 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part p

4、roducers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.4 FABRIC CONSTRUCTION 3.4.1 Fabric Count, +/- 5 % tolerance (ASTM D375) Warp 250 ends/10 cm Weft 160 picks/10 cm 3.4.2 Fabric Weight, range (FLTM BN 106-01) 230 - 270 g/m23.5 COMPOSITION (ASTM D

5、629) Fabric 100 % polyester 3.6 YARN CONSTRUCTION (ASTM D 1244) Warp 500 dtex f130, round, air texturized Weft 500 dtex f130, round, ENGINEERING MATERIAL SPECIFICATION WSS-M1H792-A Page 2 of 2 Copyright 2008, Ford Global Technologies, Inc. air texturized 3.7 METHOD OF DYEING Yarn dyed or as approved

6、 by Materials Enginering 3.8 FINISHED OPERATIONS As approved by Materials Engineering 3.9 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 this specification: 5.1 Purchase departments will ensure that both materials defined in this specification and shipped to any one assembly plant will be produced by one supplier only.

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4573-1999 Aerospace Series Heat Resisting Alloy FE-PA4901 (X12CrNiCoMoW21-20) Solution Treated and Precipitation Treated Bar and Section De Less Than or Equal to 100 mm .pdf AECMA PREN 4573-1999 Aerospace Series Heat Resisting Alloy FE-PA4901 (X12CrNiCoMoW21-20) Solution Treated and Precipitation Treated Bar and Section De Less Than or Equal to 100 mm .pdf
  • AECMA PREN 4574-1999 Aerospace Series Heat Resisting Alloy FE-PA4901 (X12CrNiCoMoW21-20) Solution Treated and Precipitation Treated Forgings De Less Than or Equal to 100 mm Edition.pdf AECMA PREN 4574-1999 Aerospace Series Heat Resisting Alloy FE-PA4901 (X12CrNiCoMoW21-20) Solution Treated and Precipitation Treated Forgings De Less Than or Equal to 100 mm Edition.pdf
  • AECMA PREN 4575-1999 Aerospace Series Heat Resisting Alloy FE-PA4901 (X12CrNiCoMoW21-20) Solution Treated and Descaled Sheet and Plate 3 mm Less Than a Less Than or Equal to 50 mm .pdf AECMA PREN 4575-1999 Aerospace Series Heat Resisting Alloy FE-PA4901 (X12CrNiCoMoW21-20) Solution Treated and Descaled Sheet and Plate 3 mm Less Than a Less Than or Equal to 50 mm .pdf
  • AECMA PREN 4585-2000 Aerospace Series Clips Spring Tension Technical Specification Edition P 1《航空航天系列.夹弹簧张力技术规范.P1版》.pdf AECMA PREN 4585-2000 Aerospace Series Clips Spring Tension Technical Specification Edition P 1《航空航天系列.夹弹簧张力技术规范.P1版》.pdf
  • AECMA PREN 4588-2005 Aerospace Series Paints and Varnishes Two Component Cold Curing Polyurethane Paint Anti Slip Edition P 1《航空航天系列.防滑两成分冷聚亚安酯油漆涂料.P1版》.pdf AECMA PREN 4588-2005 Aerospace Series Paints and Varnishes Two Component Cold Curing Polyurethane Paint Anti Slip Edition P 1《航空航天系列.防滑两成分冷聚亚安酯油漆涂料.P1版》.pdf
  • AECMA PREN 4590-2000 Aerospace Series Retainers Spring Sheet Metal for Self-Locking Barrel Nuts in Corrosion Resisting Steel Passivated Editino P 1《航空航天系列.固定器弹簧金属片自动锁螺母抗腐蚀钢钝化.P1版》.pdf AECMA PREN 4590-2000 Aerospace Series Retainers Spring Sheet Metal for Self-Locking Barrel Nuts in Corrosion Resisting Steel Passivated Editino P 1《航空航天系列.固定器弹簧金属片自动锁螺母抗腐蚀钢钝化.P1版》.pdf
  • AECMA PREN 4591-2000 Aerospace Series Nuts Barrel Self-Locking Floating Self-Aligning in Heat Resisting Nickel Base Alloy MoS2 Lubricated Classification 1 550 MPa (at Ambient Tempe.pdf AECMA PREN 4591-2000 Aerospace Series Nuts Barrel Self-Locking Floating Self-Aligning in Heat Resisting Nickel Base Alloy MoS2 Lubricated Classification 1 550 MPa (at Ambient Tempe.pdf
  • AECMA PREN 4592-2005 Aerospace series Paints and varnishes Test method for determination of infrared reflectance Edition P 1《航空航天系列.油漆涂料试验方法红外线反射系数.P1版》.pdf AECMA PREN 4592-2005 Aerospace series Paints and varnishes Test method for determination of infrared reflectance Edition P 1《航空航天系列.油漆涂料试验方法红外线反射系数.P1版》.pdf
  • AECMA PREN 4593-2002 Aerospace Series Non-Metallic Materials Paints and Varnishes Test Method Determination of Solar Absorptance Edition P 1《航空航天系列.非金属物质油漆涂料试验方法太阳吸收.P1版》.pdf AECMA PREN 4593-2002 Aerospace Series Non-Metallic Materials Paints and Varnishes Test Method Determination of Solar Absorptance Edition P 1《航空航天系列.非金属物质油漆涂料试验方法太阳吸收.P1版》.pdf
  • 相关搜索
    资源标签

    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