FORD WSS-M2D241-A2-2004 TUBING ECO EPICHLOROHYDRIN C FUEL AND OIL RESISTANT TO BE USED WITH FORD WSS-M99P1111-A ((Formerly ESE-M2D241-A2))《耐燃料和油表氯醇(ECO)管件 与标准FORD WSS-M99P1111-A.pdf

上传人:testyield361 文档编号:752779 上传时间:2019-01-14 格式:PDF 页数:3 大小:68.47KB
下载 相关 举报
FORD WSS-M2D241-A2-2004 TUBING ECO EPICHLOROHYDRIN C FUEL AND OIL RESISTANT  TO BE USED WITH FORD WSS-M99P1111-A  ((Formerly ESE-M2D241-A2))《耐燃料和油表氯醇(ECO)管件  与标准FORD WSS-M99P1111-A.pdf_第1页
第1页 / 共3页
FORD WSS-M2D241-A2-2004 TUBING ECO EPICHLOROHYDRIN C FUEL AND OIL RESISTANT  TO BE USED WITH FORD WSS-M99P1111-A  ((Formerly ESE-M2D241-A2))《耐燃料和油表氯醇(ECO)管件  与标准FORD WSS-M99P1111-A.pdf_第2页
第2页 / 共3页
FORD WSS-M2D241-A2-2004 TUBING ECO EPICHLOROHYDRIN C FUEL AND OIL RESISTANT  TO BE USED WITH FORD WSS-M99P1111-A  ((Formerly ESE-M2D241-A2))《耐燃料和油表氯醇(ECO)管件  与标准FORD WSS-M99P1111-A.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 2004 07 21 Revised Format Updated 2002 08 19 Revised Rev para 1, updated & renumbered A. Reaume 2002 03 07 Activated A. Reaume Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 1 of 3 TUBING, ECO, EPICHLOROHYDR

2、IN FUEL AND OIL RESISTANT WSS-M2D241-A2 1. SCOPE The material defined by this specification is epichlorohydrin rubber. 2. APPLICATION This specification was released originally for material used in non-reinforced vacuum tubing in engines and where gasoline, ozone, heat and tear resistance are major

3、requirements. This material does not use lead compounds in the formulation. 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). 3.2 MATERIAL TESTING 3.2.

4、1 Preparation of Test Specimens All test specimens shall be die-cut from molded test slabs. The test sheets shall have the following dimensions: 150 x 150 mm, min x 2.0 +/- 0.2 mm 3.3 ORIGINAL PROPERTIES 3.3.1 Hardness, Durometer A, +/- 5 70 (ISO 868/ASTM D 2240, instantaneous, plied-up specimen. Ha

5、nd held durometers shall not be used) 3.3.2 Tensile Strength, MPa, min 8.3 (ISO 37/ASTM D 412, Die C) 3.3.3 Elongation at Break, min 200 (Test Method according to para 3.6.3)3.3.4 Modulus at 100%, Elongation, MPa, min 3.0 (Test Method according to para 3.6.3)ENGINEERING MATERIAL SPECIFICATIONWSS-M2D

6、241-A2Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 2 of 3 3.3.5 Tear Strength, k N/m, min 26 (ISO 34, Method B, procedure Ca)/ASTM D 624, Die C1) 3.3.6 Compression Set, %, max 30 (ISO 815/ASTM D 395, Method B, except 25% compression, solid button specimens. 22 h

7、 at 100 C) 3.3.7 Ozone Resistance, max 0 (FLTM BP 101-01) 50 pphm for 70 hours at 38 C, 20% elongation 3.3.8 Low Temperature -34 Retraction, TR-10, C, min (ASTM D 1329) 3.4 HEAT AGED (ISO 188/ASTM D 573, 150 +/- 50 air changes/h, 1,000 h at 120 +/- 2 C) Hardness, Durometer A, Change, max + 20 Tensil

8、e Strength Change, %, max -50 Elongation at Break Change, %, max -75 3.5 HEAT AGED (ISO 188/ASTM D 573, 150 +/- 50 air changes/h, 168 h at 130 +/- 2 C) Hardness, International, Change, max + 10 Tensile Strength Change, %, max -50 Elongation at Break Change, %, max -60 3.6 IMMERSION IN OIL NO. 3 or I

9、RM 903 OIL (ISO 1817/ASTM D 471, 168 h at 130 +/- 2 C) Hardness International, Change, max -10 to +15 Tensile Strength Change, %, max -30 Elongation at Break Change, %, max -60 Volume Change, % max -5 to +15 ENGINEERING MATERIAL SPECIFICATIONWSS-M2D241-A2Printed copies are uncontrolled Copyright 200

10、4, Ford Global Technologies, LLC Page 3 of 3 3.7 IMMERSION IN FUEL C (ISO 1817/ASTM D 471, 70 h at 23 +/- 2 C) Hardness, International, Change, max -25 Tensile Strength Change, %, max -50 Elongation at Break Change, %, max -50 Volume Change, %, max + 40 3.8 IMMERSION IN FUEL C Dry out 24 h at 70 +/- 2 C) Volume Change, %, max -15 to + 5 4. GENERAL INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of this specification. 4.1 RECYCLING CODE ECO

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 2713-005-1995 Aerospace Series Cables Electrical Single and Multicore for General Pupose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 005  Screen.pdf AECMA PREN 2713-005-1995 Aerospace Series Cables Electrical Single and Multicore for General Pupose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 005 Screen.pdf
  • AECMA PREN 2713-006-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 006  Scree.pdf AECMA PREN 2713-006-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 006 Scree.pdf
  • AECMA PREN 2713-007-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures Between - 55 Degrees Celsius and 200 Degrees Celsius Par.pdf AECMA PREN 2713-007-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures Between - 55 Degrees Celsius and 200 Degrees Celsius Par.pdf
  • AECMA PREN 2713-008-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 008  Scree.pdf AECMA PREN 2713-008-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 008 Scree.pdf
  • AECMA PREN 2713-009-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures Between - 55 Degrees Celsius and 200 Degrees Celsius Par.pdf AECMA PREN 2713-009-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures Between - 55 Degrees Celsius and 200 Degrees Celsius Par.pdf
  • AECMA PREN 2713-010-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 010  Scree.pdf AECMA PREN 2713-010-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 200 Degrees C Part 010 Scree.pdf
  • AECMA PREN 2713-011-2000 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures Between -55 Degrees C and 200 Degrees C Part 011 Silver .pdf AECMA PREN 2713-011-2000 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures Between -55 Degrees C and 200 Degrees C Part 011 Silver .pdf
  • AECMA PREN 2714-002-2003 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between -55 Degrees C and 260 Degrees C Part 002 Screene.pdf AECMA PREN 2714-002-2003 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between -55 Degrees C and 260 Degrees C Part 002 Screene.pdf
  • AECMA PREN 2714-003-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 260 Degrees C Part 003  Scree.pdf AECMA PREN 2714-003-1995 Aerospace Series Cables Electrical Single and Multicore for General Purpose Operating Temperatures between - 55 Degrees C and 260 Degrees C Part 003 Scree.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