FORD WSD-M2D435-A-2010 RUBBER HYDROGENATED NITRILE (HNBR) OXIDIZED AND OXYGENATED FUEL RESISTANT TO BE USED WITH FORD WSS-M99P1111-A 《耐氧化和含氧燃料的氢化丁腈橡胶(HNBR) 与标准FORD WSS-M99P1111-.pdf

上传人:王申宇 文档编号:749867 上传时间:2019-01-14 格式:PDF 页数:3 大小:27.43KB
下载 相关 举报
FORD WSD-M2D435-A-2010 RUBBER HYDROGENATED NITRILE (HNBR) OXIDIZED AND OXYGENATED FUEL RESISTANT  TO BE USED WITH FORD WSS-M99P1111-A  《耐氧化和含氧燃料的氢化丁腈橡胶(HNBR)  与标准FORD WSS-M99P1111-.pdf_第1页
第1页 / 共3页
FORD WSD-M2D435-A-2010 RUBBER HYDROGENATED NITRILE (HNBR) OXIDIZED AND OXYGENATED FUEL RESISTANT  TO BE USED WITH FORD WSS-M99P1111-A  《耐氧化和含氧燃料的氢化丁腈橡胶(HNBR)  与标准FORD WSS-M99P1111-.pdf_第2页
第2页 / 共3页
FORD WSD-M2D435-A-2010 RUBBER HYDROGENATED NITRILE (HNBR) OXIDIZED AND OXYGENATED FUEL RESISTANT  TO BE USED WITH FORD WSS-M99P1111-A  《耐氧化和含氧燃料的氢化丁腈橡胶(HNBR)  与标准FORD WSS-M99P1111-.pdf_第3页
第3页 / 共3页
亲,该文档总共3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 05 25 N-STATUS No replacement named C. Mracna, NA 2004 09 24 Revised Inserted 3.0; Deleted 3.1, 3.2, 3.3, 3.13 & 4 1991 03 20 Released C10127030 B. Hennessey Printed copies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Pa

2、ge 1 of 3 RUBBER, HYDROGENATED NITRILE (HNBR) OXIDIZED WSD-M2D435-A AND OXYGENATED FUEL RESISTANT NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a hydrogenated nitrile rubber compound. 2. APPLICATION This specification was released originally for material used a

3、s an in-tank fuel pump insulator and mounting. The material has good resistance to oxygenated and oxidized fuels and ozone. It remains flexible at -40 C when fuel saturated. 3. REQUIREMENTS 3.0 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the C

4、ompanys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.4 MATERIAL TESTING 3.4.1 Preparation of Test Specimens All tests shall be carried out on finished parts. When not feasible, specimens cut from molded test sheets manufactured from the same material and with equivalent cure to

5、 molded parts are recommended. The test sheets shall have the following dimensions: 150 x 150 mm, min x 2.0 +/- 0.2 mm 3.5 ORIGINAL PROPERTIES 3.5.1 Hardness, International 55 - 65 (ISO 48/ASTM D 1415) 3.5.2 Tensile Strength, min 14.0 MPa (ISO 37/ASTM D 412, Die C) 3.5.3 Elongation at Break, min 300

6、 (Test method according to 3.5.4) 3.5.4 Modulus at 100% Elongation 1.0 to 3.0 MPa (Test method according to 3.5.4) 3.5.5 Compression Set, max 65% (ISO 815/ASTM D 395, Method B, except 25% compression, plied-up specimens, 70 h at 100 +/- 2 C) ENGINEERING MATERIAL SPECIFICATIONWSD-M2D435-A Printed co

7、pies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Page 2 of 3 3.6 HEAT AGED (ISO 188/ASTM D 573, 150 +/- 50 air changes/h, 1000 h at 80 +/- 2 C) 3.6.1 Hardness Change, max +5 3.6.2 Tensile Strength Change, max -10% 3.6.3 Elongation Change, max -25% 3.6.4 Visual Evaluation No surfac

8、e tackiness or cracks when folded flat against itself. 3.7 IMMERSION IN FUEL C (ISO 1817/ASTM D 471, 70 h at 23 +/- 2 C) 3.7.1 Hardness Change, max -25 3.7.2 Tensile Strength Change, max -70% 3.7.3 Elongation Change, max -30% 3.7.4 Volume Change, max +35% 3.7.4.1 Dry Out, Shrinkage, max -15% (24 h a

9、t 80 +/- 2 C, use specimens from 3.7.4) 3.8 IMMERSION IN 85% FUEL C +15% METHANOL (ISO 1817/ASTM D 471, 70 h at 23 +/- 2 C) 3.8.1 Hardness Change, max -30 3.8.2 Tensile Strength Change, max -70% 3.8.3 Elongation Change, max -30% 3.8.4 Volume Change, max +60% 3.8.4.1 Dry Out, Shrinkage, max -15% (24

10、h at 80 +/- 2 C, use specimens from 3.8.4) 3.9 IMMERSION IN OXIDIZED FUEL (SOUR GAS) (ISO 1817/ASTM D 471, 70 h at 60 +/- 2 C, PN 90, fuel according to FLTM AZ 105-01) 3.9.1 Hardness Change, max -30 3.9.2 Tensile Strength Change, max -75% 3.9.3 Elongation Change, max -30% 3.9.4 Visual Evaluation No

11、surface tackiness or cracks when folded flat against itself after drying out. ENGINEERING MATERIAL SPECIFICATIONWSD-M2D435-A Printed copies are uncontrolled Copyright 2010, Ford Global Technologies, LLC Page 3 of 3 3.10 COLD FLEXIBILITY AT -40 C (FLTM BN 102-01, Procedure B, after conditioning in Fu

12、el C for 70 h at 23 +/- 2 C) At the end of the aging period there shall be no signs of cracking, or disintegration when examined under 7X power glass. 3.11 OZONE RESISTANCE, max (FLTM BP 101-01) 3.11.1 After Conditioning in Fuel C +15% Methanol Rating 1 Completely immerse suitable lengths of materia

13、l in 85% Fuel C +15% Methanol for 48 h at 23 +/- 2 C after which they are dried by suspending vertically in a well ventilated area for an additional 48 h at 23 +/- 2 C. 3.12 CRYSTALLINE COPPER SALT FORMATION No crystal formation on the rubber or copper strip. No copper tarnish Test Method: ASTM D 13

14、0 (Automotive Gasoline Method), except use 150 mL Fuel C +15% Methanol in a 200 mL test tube. Mount 75 x 12.5 x 2 mm rubber sample parallel but held 10 mm away from the copper strip. Age for 168 h at 23 +/- 2 C. 5. GENERAL INFORMATION The information below is provided for clarification and assistance in meeting the requirements of this specification. 5.1 Density TBE (ISO 1183, METHOD A/ASTM D 297) 5.2 Hardness, Durometer A 55 - 65 (ISO 868/ASTM D 2240, instantaneous, plied-up specimen)

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 3824-1996 Aerospace Series Clinch-Nuts Blind Self-Locking with Counterbore in Corrosion Resisting Steel MoS2 Lubricated Classification 600 MPa (at Ambient Temperature.pdf ASD-STAN PREN 3824-1996 Aerospace Series Clinch-Nuts Blind Self-Locking with Counterbore in Corrosion Resisting Steel MoS2 Lubricated Classification 600 MPa (at Ambient Temperature.pdf
  • ASD-STAN PREN 3825-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 60 IRHD (Edition P 1)《航空航天系列 硬度60 IRHD的氟硅酮橡胶(FVMQ) 第P1版》.pdf ASD-STAN PREN 3825-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 60 IRHD (Edition P 1)《航空航天系列 硬度60 IRHD的氟硅酮橡胶(FVMQ) 第P1版》.pdf
  • ASD-STAN PREN 3826-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 70 IRHD (Edition P 1)《航空航天系列 硬度70 IRHD的氟硅酮橡胶(FVMQ) 第P1版》.pdf ASD-STAN PREN 3826-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 70 IRHD (Edition P 1)《航空航天系列 硬度70 IRHD的氟硅酮橡胶(FVMQ) 第P1版》.pdf
  • ASD-STAN PREN 3827-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 80 IRHD (Edition P 1)《航空航天系列 硬度80 IRHD的氟硅酮橡胶(FVMQ) 第P1版》.pdf ASD-STAN PREN 3827-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 80 IRHD (Edition P 1)《航空航天系列 硬度80 IRHD的氟硅酮橡胶(FVMQ) 第P1版》.pdf
  • ASD-STAN PREN 3830-1995 Aerospace Series Electrical System Load Analysis (Edition P 1)《航空航天系列 电气系统负载分析 第P1版》.pdf ASD-STAN PREN 3830-1995 Aerospace Series Electrical System Load Analysis (Edition P 1)《航空航天系列 电气系统负载分析 第P1版》.pdf
  • ASD-STAN PREN 3831-2000 Aerospace Series Inserts Thick Wall Self-Locking in Heat Resisting Steel FE-PM3801 (17-4PH) MoS2 Coated (Edition P 2)《航空航天系列 MoS2涂层的耐热钢FE-PM3801(17-4PH)制自锁厚.pdf ASD-STAN PREN 3831-2000 Aerospace Series Inserts Thick Wall Self-Locking in Heat Resisting Steel FE-PM3801 (17-4PH) MoS2 Coated (Edition P 2)《航空航天系列 MoS2涂层的耐热钢FE-PM3801(17-4PH)制自锁厚.pdf
  • ASD-STAN PREN 3832-1992 Aerospace Series Bolts Double Hexagon Head Relieved Shank Long Thread in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Classification 1 550 MPa (.pdf ASD-STAN PREN 3832-1992 Aerospace Series Bolts Double Hexagon Head Relieved Shank Long Thread in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Classification 1 550 MPa (.pdf
  • ASD-STAN PREN 3833-2015 Aerospace series Bolts MJ threads in heat resisting nickel base alloy NI-PH2601 (Inconel 718) passivated Classification 1 550 MPa (at ambient temperature)  .pdf ASD-STAN PREN 3833-2015 Aerospace series Bolts MJ threads in heat resisting nickel base alloy NI-PH2601 (Inconel 718) passivated Classification 1 550 MPa (at ambient temperature) .pdf
  • ASD-STAN PREN 3833-2018 Aerospace series - Bolts MJ threads in heat resisting nickel base alloy NI-PH2601 (Inconel 718) passivated - Classification 1 550 MPa (at ambient temperatur.pdf ASD-STAN PREN 3833-2018 Aerospace series - Bolts MJ threads in heat resisting nickel base alloy NI-PH2601 (Inconel 718) passivated - Classification 1 550 MPa (at ambient temperatur.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