FORD FLTM BN 117-03-2001 EVALUATION OF TRIM MATERIALS AFTER ACCELERATED EXPOSURE IN A CONTROLLED IRRADIANCE WATER COOLED XENON ARC APPARATUS《内饰材料在某一控制发光的水冷式氙弧灯设备中加速暴露后的评估》.pdf

上传人:amazingpat195 文档编号:747253 上传时间:2019-01-14 格式:PDF 页数:2 大小:90.59KB
下载 相关 举报
FORD FLTM BN 117-03-2001 EVALUATION OF TRIM MATERIALS AFTER ACCELERATED EXPOSURE IN A CONTROLLED IRRADIANCE WATER COOLED XENON ARC APPARATUS《内饰材料在某一控制发光的水冷式氙弧灯设备中加速暴露后的评估》.pdf_第1页
第1页 / 共2页
FORD FLTM BN 117-03-2001 EVALUATION OF TRIM MATERIALS AFTER ACCELERATED EXPOSURE IN A CONTROLLED IRRADIANCE WATER COOLED XENON ARC APPARATUS《内饰材料在某一控制发光的水冷式氙弧灯设备中加速暴露后的评估》.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、FORD LABORATORY TEST METHOD BN 117-03 Date 2001 O9 12 I99001 16 EVALUATION OF TRIM MATERIALS AFTER ACCELERATED EXPOSURE IN A CONTROLLED IRRADIANCE WATER COOLED XENON ARC APPARATUS Action Revisions Revised Editorial - no technical change A. Cockman Application This procedure is used to determine the

2、effects of ultraviolet radiation on deterioration of fabrics after controlled irradiance water cooled xenon arc weatherometer exposure. Scope This procedure provides for two methods of evaluating deterioration after weatherometer exposure. These involve measuring either retained tensile strength or

3、surface fiber deterioration. Apparatus Required Weatherometer Atlas CI Series Xenon Arc Weatherometer with 3 tier rack or equivalent. Sample Holder Atlas SL-3 holder or equivalent. Tensile Testing Machine Instron Model 7M or equivalent constant rate of extension type tensile tester. Conditioning and

4、 Test Conditions All test values indicated herein are based on material conditioned in a controlled atmosphere of 23 +/- 2 OC and 50 +/- 5 % relative humidity for not less than 24 h prior to testing and tested under the same conditions unless otherwise specified. Procedure A. Method A - Retained Ten

5、sile Strength 1. Measure and cut 8 samples - 70 x 145 mm, 4 with the long dimension in the warp direction and 4 with the long dimension in the fill direction. Copynght02001, Ford Global Technologies, Inc FORD LABORATORY TEST METHOD BN 117-03 2. Mount 2 warp and 2 fill samples in sample holders with

6、an exposure area of 50 x 120 mm. Back weatherometer samples with white card stock as described in SAE JI 885. The other 4 samples, 2 in each direction, will be used for original tensile strength values. 3. Expose the fabrics in axenon arc weatherometer as specified in the relevant material specifica

7、tion, under the operating conditions described in SAE JI 885. 4. Test the tensile strength of the original and exposed samples as follows: (a) Secure test specimen centrally in the clamps of a constant rate of extension type of tensile machine having an initial jaw separation of 75 mm. The face of o

8、ne jaw of each clamp shall be 25 x 25 mm; the other jaw face of each clamp shall be at least as large. All jaws shall be rubber faced. Cross-head speed shall be 305 mm/min. (b) Compute the average tensile strength in each direction for the two aged and the two original samples. 5. Calculate the perc

9、ent retained tensile (in each direction) as follows: % Retained Tensile = Aaed Tensile (Av x 100 Original Tensile (Avg) B. Method B - Surface Fiber Deterioration 1. Expose the fabrics in a xenon arc weatherometer for the exposure time specified in the applicable material specification, under the ope

10、rating conditions described in SAE J1885. 2. Firmly apply a piece of 3Ms Highland Brand 6200 Permanent Mending Tape or equivalent to the surface of the exposed fabric (yarn). Then rapidly strip the tape and mount it on a sheet of light or dark cardstock which contrasts with the color of the fiber. 3

11、. Repeat the test with a new piece of tape on an unexposed sample and compare the length and quantity of fibers removed by the tape. 4. Report fiber deterioration if a significantly larger number of fibers (usually of shorter lengths) are removed from the exposed versus unexposed sample. Chemicals, materials, parts, and equipment referenced in this document must be used and handled properly. Each party is responsible for determining proper use and handling in its facilities. Page 2 of 2 Copynght02001, Ford Global Technologies, Inc

展开阅读全文
相关资源
猜你喜欢
  • BS EN 3446-1995 Bearings precision ball without flange in corrosion resisting steel for instruments and equipment - Dimensions and loads《仪器和设备用的耐蚀钢的不带法兰的精密球轴承 尺寸规格和负荷》.pdf BS EN 3446-1995 Bearings precision ball without flange in corrosion resisting steel for instruments and equipment - Dimensions and loads《仪器和设备用的耐蚀钢的不带法兰的精密球轴承 尺寸规格和负荷》.pdf
  • BS EN 3451-2017 Aerospace series Titanium TI-P99002 Not heat treated Grade 2 forging stock for annealed forgings - a or D 300 mm《航空航天系列 钛钛- P9002 没有热处理过 退火锻件用2级锻坯- a或D 300 mm》.pdf BS EN 3451-2017 Aerospace series Titanium TI-P99002 Not heat treated Grade 2 forging stock for annealed forgings - a or D 300 mm《航空航天系列 钛钛- P9002 没有热处理过 退火锻件用2级锻坯- a或D 300 mm》.pdf
  • BS EN 3456-2012 Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Sheet and strip hot rolled - a 6 mm《航空航天系列 TI-P64001(Ti-6Al-4V)型钛合金 退火 热轧薄板材和带材 a 6 mm》.pdf BS EN 3456-2012 Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Sheet and strip hot rolled - a 6 mm《航空航天系列 TI-P64001(Ti-6Al-4V)型钛合金 退火 热轧薄板材和带材 a 6 mm》.pdf
  • BS EN 3459-2010 Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm a 50 mm《航空航天系列 TI-P63001(Ti-4Al-4Mo-2Sn)钛合金 经溶解处理和老化处理的6 mm .pdf BS EN 3459-2010 Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm a 50 mm《航空航天系列 TI-P63001(Ti-4Al-4Mo-2Sn)钛合金 经溶解处理和老化处理的6 mm .pdf
  • BS EN 3464-2012 Aerospace series Titanium alloy (Ti-6Al-4V) Annealed Plate 6 mm a 100 mm《航天航空系列 钛合金(TI-6AI-4V) 煅烧 板材 6 mm a 100 m》.pdf BS EN 3464-2012 Aerospace series Titanium alloy (Ti-6Al-4V) Annealed Plate 6 mm a 100 mm《航天航空系列 钛合金(TI-6AI-4V) 煅烧 板材 6 mm a 100 m》.pdf
  • BS EN 3469-2009 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D 200 mm - Rm 1310 .pdf BS EN 3469-2009 Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D 200 mm - Rm 1310 .pdf
  • BS EN 3474-2005 Aerospace series - Aluminium alloy AL-P2024-T81 - Sheet and strip - 0 25 mm $3l a 6 mm《航空航天系列 AL-P2024-T81型铝合金 薄板材和带材 0 25mm≤a≤6mm》.pdf BS EN 3474-2005 Aerospace series - Aluminium alloy AL-P2024-T81 - Sheet and strip - 0 25 mm $3l a 6 mm《航空航天系列 AL-P2024-T81型铝合金 薄板材和带材 0 25mm≤a≤6mm》.pdf
  • BS EN 3475-100-2010 Aerospace series Cables nelectrical aircraft use Test methods  nPart 100 General《航空航天系列 航空器用电缆 试验方法 总则》.pdf BS EN 3475-100-2010 Aerospace series Cables nelectrical aircraft use Test methods nPart 100 General《航空航天系列 航空器用电缆 试验方法 总则》.pdf
  • BS EN 3475-201-2002 Aerospace series - Cables electrical aircraft use - Test methods - Visual examination《航空航天系列 航空器用电缆 试验方法 目视检查》.pdf BS EN 3475-201-2002 Aerospace series - Cables electrical aircraft use - Test methods - Visual examination《航空航天系列 航空器用电缆 试验方法 目视检查》.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