FORD WSS-M2D514-A-2010 POLYURETHANE (PUR) FOAM OPEN CELL RETICULATED TO BE USED WITH FORD WSS-M99P1111-A 《非封闭网状聚氨酯(PUR)泡沫 与福特WSS-M99P1111-A 一起使用》.pdf

上传人:figureissue185 文档编号:752892 上传时间:2019-01-14 格式:PDF 页数:2 大小:32.01KB
下载 相关 举报
FORD WSS-M2D514-A-2010 POLYURETHANE (PUR) FOAM OPEN CELL RETICULATED  TO BE USED WITH FORD WSS-M99P1111-A  《非封闭网状聚氨酯(PUR)泡沫  与福特WSS-M99P1111-A  一起使用》.pdf_第1页
第1页 / 共2页
FORD WSS-M2D514-A-2010 POLYURETHANE (PUR) FOAM OPEN CELL RETICULATED  TO BE USED WITH FORD WSS-M99P1111-A  《非封闭网状聚氨酯(PUR)泡沫  与福特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 SPECIFICATIONDate Action Revisions 2010 12 16 Activated S. Stanciu, NA Printed copies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Page 1 of 2 POLYURETHANE (PUR) FOAM, OPEN CELL, RETICULATED WSS-M2D514-A 1. SCOPE The materials defined by this specification are

2、 slab stock open cell reticulated polyether polyurethane foams. 2. APPLICATION The specification was released originally for material used in seating application as a plus pad for perforated leather inserts. 3. REQUIREMENTS 3.1 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and pa

3、rt producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.2 APPEARANCE The foam shall have a homogeneous open cell structure with no large voids or solid spots which may impair the serviceability of the part. 3.3 TEST SPECIMEN The following material

4、 properties shall be determined on specimens taken from the core 6 - 10 mm from the surface skin, unless otherwise specified. The specimens shall be free of voids, hard spots and densification lines. 3.3.1 Density, range* 30 37 kg/m3 (ASTM D 3574, Test A) *Note: Foam density to be specified in the E

5、ngineering Specification 3.3.2 Tensile Strength, min (ASTM D 3574, Test E, 50 mm bench marks, 5 specimens minimum) 3.3.2.1 As Received 55 kPa 3.3.2.2 After Heat Aging, 22 hrs at 140 C 33 kPa 3.3.3 Elongation, 70% min (ASTM D 3574, Test E, 50 mm bench marks, 5 specimens minimum) ENGINEERING MATERIAL

6、SPECIFICATIONWSS-M2D514-APrinted copies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Page 2 of 2 3.3.4 Tear Strength, 300 N/m min (ASTM D 3574, Test F, 50 mm/minute test speed) 3.3.5 Compression Set, 20% max (ASTM D 3574, Test D, Ct calculation, 22 h at 70 C, 50% deflection, 3 spec

7、imens minimum) 3.3.6 Indentation Force Deflection, range (ASTM D 3574, Test B1, 25% and 65% deflection, 3 specimens min, 100 mm thick) 3.3.6.1 At 25% deflection 175 250 N 3.3.6.2 At 65% deflection 300 525 N 3.3.7 Fogging (SAE J1756, 3 h at 100 C heating, 21 C cooling plate, post test conditioning 16

8、 h) Fog Number, 70 min Formation of clear film, droplets or crystals is cause for rejection. 3.3.8 Odor, Rating 3 max (FLTM BO 131-03) 3.3.9 Flammability (ISO 3795/SAE J369) Burn Rate, 100 mm/minute max 3.4 ADDITIONAL REQUIREMENTS Specific requirements for material and/or manufactured parts shall be

9、 specified on the Engineering drawing, Engineering parts specification and/or performance specifications. All critical areas with respect to these properties shall be clearly designated on the engineering drawing. 4. GENERAL INFORMATION The information below is provided for clarification and assistance in meeting the requirements of this specification. 4.1 Permeability (ASTM D737), 1 in specimen 305- 455 cm3/s/cm24.2 RECYCLING CODE PUR

展开阅读全文
相关资源
猜你喜欢
  • EN 4496-2005 en Aerospace series - Screws 100 ountersunk normal head offset cruciform recess close tolerance normal shank short thread in titanium alloy anodized with aluminium pig.pdf EN 4496-2005 en Aerospace series - Screws 100 ountersunk normal head offset cruciform recess close tolerance normal shank short thread in titanium alloy anodized with aluminium pig.pdf
  • EN 4497-2005 en Aerospace series - Screws pan head offset cruciform recess close tolerance normal shank short thread in titanium alloy anodized with aluminum pigmented coating - Cl.pdf EN 4497-2005 en Aerospace series - Screws pan head offset cruciform recess close tolerance normal shank short thread in titanium alloy anodized with aluminum pigmented coating - Cl.pdf
  • EN 4498-2005 en Aerospace series - Bolts large bihexagonal head close tolerance normal shank medium length thread in heat resisting nickel base alloy passivated with aluminium pigm.pdf EN 4498-2005 en Aerospace series - Bolts large bihexagonal head close tolerance normal shank medium length thread in heat resisting nickel base alloy passivated with aluminium pigm.pdf
  • EN 4499-2009 en Aerospace series - Screws 100 Degree countersunk reduced head offset cruciform recess close tolerance normal shank short thread in titanium alloy anodized with alum.pdf EN 4499-2009 en Aerospace series - Screws 100 Degree countersunk reduced head offset cruciform recess close tolerance normal shank short thread in titanium alloy anodized with alum.pdf
  • EN 450-1-2012 en Fly ash for concrete - Part 1 Definition specifications and conformity criteria《混凝土用飞灰 第1部分 定义 规范和合格标准》.pdf EN 450-1-2012 en Fly ash for concrete - Part 1 Definition specifications and conformity criteria《混凝土用飞灰 第1部分 定义 规范和合格标准》.pdf
  • EN 450-2-2005 en Fly ash for concrete - Part 2 Conformity evaluation《混凝土用飞灰 第2部分 合格评价 代替EN 450-1994》.pdf EN 450-2-2005 en Fly ash for concrete - Part 2 Conformity evaluation《混凝土用飞灰 第2部分 合格评价 代替EN 450-1994》.pdf
  • EN 4500-001-2012 en Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 001 General rules《航空航天系列 金属材料起草规则和演示材料的标准 第001部分 一般规则》.pdf EN 4500-001-2012 en Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 001 General rules《航空航天系列 金属材料起草规则和演示材料的标准 第001部分 一般规则》.pdf
  • EN 4500-003-2012 en Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003 Specific rules for heat resisting alloys《航空航天系列 金属材.pdf EN 4500-003-2012 en Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003 Specific rules for heat resisting alloys《航空航天系列 金属材.pdf
  • EN 4500-004-2012 en Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 004 Specific rules for titanium and titanium alloys《航空航.pdf EN 4500-004-2012 en Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 004 Specific rules for titanium and titanium alloys《航空航.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