FORD WSS-M2D496-A9-2004 POLYURETHANE (PUR) FOAM CELLULAR GASKET TO BE USED WITH FORD WSS-M99P1111-A 《蜂窝状垫片用聚氨酯(PUR)泡沫 与标准FORD WSS-M99P1111-A一起使用 列于标准WSS-M2D496-A1上》.pdf

上传人:rimleave225 文档编号:752850 上传时间:2019-01-14 格式:PDF 页数:5 大小:96.21KB
下载 相关 举报
FORD WSS-M2D496-A9-2004 POLYURETHANE (PUR) FOAM CELLULAR GASKET  TO BE USED WITH FORD WSS-M99P1111-A  《蜂窝状垫片用聚氨酯(PUR)泡沫  与标准FORD WSS-M99P1111-A一起使用  列于标准WSS-M2D496-A1上》.pdf_第1页
第1页 / 共5页
FORD WSS-M2D496-A9-2004 POLYURETHANE (PUR) FOAM CELLULAR GASKET  TO BE USED WITH FORD WSS-M99P1111-A  《蜂窝状垫片用聚氨酯(PUR)泡沫  与标准FORD WSS-M99P1111-A一起使用  列于标准WSS-M2D496-A1上》.pdf_第2页
第2页 / 共5页
FORD WSS-M2D496-A9-2004 POLYURETHANE (PUR) FOAM CELLULAR GASKET  TO BE USED WITH FORD WSS-M99P1111-A  《蜂窝状垫片用聚氨酯(PUR)泡沫  与标准FORD WSS-M99P1111-A一起使用  列于标准WSS-M2D496-A1上》.pdf_第3页
第3页 / 共5页
FORD WSS-M2D496-A9-2004 POLYURETHANE (PUR) FOAM CELLULAR GASKET  TO BE USED WITH FORD WSS-M99P1111-A  《蜂窝状垫片用聚氨酯(PUR)泡沫  与标准FORD WSS-M99P1111-A一起使用  列于标准WSS-M2D496-A1上》.pdf_第4页
第4页 / 共5页
FORD WSS-M2D496-A9-2004 POLYURETHANE (PUR) FOAM CELLULAR GASKET  TO BE USED WITH FORD WSS-M99P1111-A  《蜂窝状垫片用聚氨酯(PUR)泡沫  与标准FORD WSS-M99P1111-A一起使用  列于标准WSS-M2D496-A1上》.pdf_第5页
第5页 / 共5页
亲,该文档总共5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 2004 10 21 Revised Inserted 3.0; Deleted 3.1, 3.2, 3.3, 3.6, 3.7 & 4 1998 08 12 Revised Revised Table 1 K. Gerhards D. Whyte 1997 06 26 Activated K. Gerhards D. Whyte Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LL

2、C Page 1 of 5 POLYURETHANE (PUR) FOAM, CELLULAR GASKET WSS-M2D496-A1/A2/A3/A4/ A5/A6/A7/A8/A9/A10/A11 1. SCOPE The materials defined by these specifications are high density cellular polyurethane foams with low compression set. 2. APPLICATION These specifications were released originally for materia

3、l used for gaskets in the instrument cluster and speed control. 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). 3.4 APPEARANCE The foam shall have a

4、homogeneous medium sized cell structure with no large voids or cracks which may impair the serviceability of the part. 3.5 TEST SPECIMEN The following material properties shall be determined on specimens taken from the molded part with surface skin cut off wherever possible. In case the part dimensi

5、ons do not allow the preparation of specimens as requested, specimens shall be prepared from a 200 x 200 x 40 mm molded foam block. The specimen shall be free of voids, hard spots and densification lines. 3.5.1 Color (see Table 1) 3.5.2 Density, kg/m3 +/- 10, % (see Table 1) (ISO 845/ASTM D 3574, Te

6、st A) 3.5.3 Tensile Strength, kPa, min (see Table 1) (ISO 1798/ASTM D 3574, Test E, 50 mm bench marks, 5 specimens min) 3.5.4 Elongation at Break, %, min (see Table 1) (Test according to para 3.5.3) 3.5.5 Tear Strength, N/m, min (see Table 1) (ISO DIS 8067/ASTM D 3574, Test F, 50 mm/minute test spee

7、d) ENGINEERING MATERIAL SPECIFICATIONWSS-M2D496-A1/A2/A3/A4/A5/A6/A7/A8/A9/A10/A11 Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 2 of 5 3.5.6 Compression Set, %, max (see Table 1) (ISO 1856, Method A/ASTM D 3574, Test D, 22 h at 70 C, 50% deflection Ct calculatio

8、n, 3 specimens min) 3.5.7 Compression Deflection Stress, kPa (see Table 1) (ISO 3386/1 at 25% compression, 25.4 x 25.4 mm specimen size, determine sample thickness under 45 kg preload, 12.7 mm/minute test speed, 3 specimens min) 3.5.8 Heat Aging (ISO 2440/ASTM D 3574, Test K, 22 h at 140 +/- 2 C) 3.

9、5.8.1 Compression Deflection (see Table 1) Stress Change, %, max (Test according to para 3.5.7) 3.5.9 Humidity Aging (AUTOCLAVE) (ISO 2440/ASTM 3574, Test J, 100 x 100 x 50 mm specimen, 5 h at 120 C) 3.5.9.1 Compression Deflection (see Table 1) Stress Change, +/- %, max (Test according to para 3.5.7

10、) 3.5.10 Dimensional Stability, % (see Table 1) Test Method: Linear dimensional expansion or shrinkage after being subjected to dry heat at 80 +/- 2 C for 3 h. Specimen size should be as large as sample part permits but should not exceed 300 x 300 mm x part thickness. 3.5.11 FOGGING (SAE J1756, 3 h

11、at 100 C heating, 21 C cooling plate, post test conditioning 1 + 16 h) Fog Number, min 70 Formation of clear film, droplets or crystals is cause for rejection. 3.5.12 Odor, max Rating 2 (FLTM BO 131-01/SAE J1351) 3.5.13 Cold Flexibility at -40 C No cracking (FLTM BN 102-01, diameter of mandrel shall

12、 be 5 times of specimen thickness) ENGINEERING MATERIAL SPECIFICATIONWSS-M2D496-A1/A2/A3/A4/A5/A6/A7/A8/A9/A10/A11 Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 3 of 5 3.5.14 Solvent Resistance No surface tackiness or evidence of foam deterioration Test Method: I

13、mmerse specimens of the foam in petroleum light naphtha, trichloroethylene, currently released antifreeze (50/50 with water), currently released Windshield Washer Solution, currently released Electrical Grease, and a soap solution (50/50 with water). 3.5.15 Flammability (ISO 3795) Burn Rate, max 100

14、 mm/minute ENGINEERING MATERIAL SPECIFICATIONWSS-M2D496-A1/A2/A3/A4/A5/A6/A7/A8/A9/A10/A11 Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 4 of 5 Table 1 _ A1 A2 A3 A4 A5 A6 A7 A8 A9 A10 A11 _ 3.5.1 black black black black black black black black black black black

15、Color 3.5.2 240 320 400 240 320 240 320 480 240 320 400 Density 3.5.3 137 205 240 275 518 553 829 1382 1030 1380 1725 Tensile Strength 3.5.4 100 100 100 100 100 100 100 90 50 50 50 Elongation 3.5.5 (A) Tear 0.2 0.4 0.7 0.5 0.9 1 1.8 2.3 2 2.5 3.5 Strength 3.5.6 10 10 10 10 10 10 10 10 10 10 10 Compr

16、ession Set 3.5.7 7-35 20-55 34-83 28-55 47-90 47-96 89-161 206 138 275 410 Compression -442 -345 -552 -895 Deflection 3.5.8 (B) Heat 90 60 60 60 60 60 60 60 60 60 60 Aging 3.5.9 60 60 60 60 60 60 60 60 60 60 60 Humidity Aging 3.5.10 +/- +/- +/- +/- +/- +/- +/- +/- +/- +/- +/- Dimen- 4.0 4.0 4.0 2.5

17、2.5 2.5 2.5 2.5 5.0 5.0 5.0 sional Stability Note (A): Tear strength should be ASTM D624 Die C Note (B): Heat aging is at 120 C for Types A1, A2, A3 ENGINEERING MATERIAL SPECIFICATIONWSS-M2D496-A1/A2/A3/A4/A5/A6/A7/A8/A9/A10/A11 Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 5 of 5 5. GENERAL INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of these specifications. 5.1 RECYCLING CODE PUR

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 2240-099-1996 Aerospace Series Lamps Incandescent Part 099 Lamp Code 416700 Product Standard Edition P 1《航空航天系列白炽灯.第099部分 码指示灯416700产品标准.P1版》.pdf AECMA PREN 2240-099-1996 Aerospace Series Lamps Incandescent Part 099 Lamp Code 416700 Product Standard Edition P 1《航空航天系列白炽灯.第099部分 码指示灯416700产品标准.P1版》.pdf
  • AECMA PREN 2240-100-1998 Aerospace Series Lamps Incandescent Part 100 Lamp Code 2078 Product Standard Edition P 1《航空航天系列白炽灯.第100部分 码指示灯2078产品标准.P1版》.pdf AECMA PREN 2240-100-1998 Aerospace Series Lamps Incandescent Part 100 Lamp Code 2078 Product Standard Edition P 1《航空航天系列白炽灯.第100部分 码指示灯2078产品标准.P1版》.pdf
  • AECMA PREN 2240-101-1998 Aerospace Series Lamps Incandescent Part 101 Lamp Code 404-02 Product Standard Edition P 1《航空航天系列白炽灯.第101部分 码指示灯404-02产品标准.P1版》.pdf AECMA PREN 2240-101-1998 Aerospace Series Lamps Incandescent Part 101 Lamp Code 404-02 Product Standard Edition P 1《航空航天系列白炽灯.第101部分 码指示灯404-02产品标准.P1版》.pdf
  • AECMA PREN 2241-1990 Aerospace Series Lamp Base Dimensions Issue P 1《航空航天系列.灯座尺寸》.pdf AECMA PREN 2241-1990 Aerospace Series Lamp Base Dimensions Issue P 1《航空航天系列.灯座尺寸》.pdf
  • AECMA PREN 2242-1991 Aerospace Series Control of Tools Used for Crimping of Electric Cables with Conductors Defined by EN 2083 and EN 2346 Issue P 1《航空和航天.卷边工具和电缆工具的检验.定义EN 2083 和 .pdf AECMA PREN 2242-1991 Aerospace Series Control of Tools Used for Crimping of Electric Cables with Conductors Defined by EN 2083 and EN 2346 Issue P 1《航空和航天.卷边工具和电缆工具的检验.定义EN 2083 和 .pdf
  • AECMA PREN 2243-1-1980 Structural Adhesives Test Methods Part 1 - Single Lap Shear Aerospace Series Edition 1《结构用粘结剂试验方法.第1部分-单搭接剪切航空航天系列.第.第1版》.pdf AECMA PREN 2243-1-1980 Structural Adhesives Test Methods Part 1 - Single Lap Shear Aerospace Series Edition 1《结构用粘结剂试验方法.第1部分-单搭接剪切航空航天系列.第.第1版》.pdf
  • AECMA PREN 2243-2-2001 Aerospace Series Non-Metallic Materials Structural Adhesives Test Method Part 2 Peel Metal-Metal Edition P 1《航空航天系列非金属物质结构用粘结剂.第2部分 剥离金属.P1版》.pdf AECMA PREN 2243-2-2001 Aerospace Series Non-Metallic Materials Structural Adhesives Test Method Part 2 Peel Metal-Metal Edition P 1《航空航天系列非金属物质结构用粘结剂.第2部分 剥离金属.P1版》.pdf
  • AECMA PREN 2243-3-2001 Aerospace Series Non-Metallic Materials Structural Adhesives Test Method Part 3 Peeling Test Metal-Honeycomb Core Edition P 1《航空航天系列非金属物质结构用粘结剂.第3部分 剥离试验用金属-.pdf AECMA PREN 2243-3-2001 Aerospace Series Non-Metallic Materials Structural Adhesives Test Method Part 3 Peeling Test Metal-Honeycomb Core Edition P 1《航空航天系列非金属物质结构用粘结剂.第3部分 剥离试验用金属-.pdf
  • AECMA PREN 2243-4-2001 Aerospace Series Non-Metallic Materials Structural Adhesives Test Method Part 4 Metal-Honeycomb Core Flatwise Tensile Test Edition P 1《航空航天系列非金属物质结构用粘结剂.第4部分.pdf AECMA PREN 2243-4-2001 Aerospace Series Non-Metallic Materials Structural Adhesives Test Method Part 4 Metal-Honeycomb Core Flatwise Tensile Test Edition P 1《航空航天系列非金属物质结构用粘结剂.第4部分.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