FORD ESB-M3G100-A-2005 TAPE PAPER BACKED-PRESSURE SENSITIVE-PRINTABLE TO BE USED WITH FORD WSS-M99P1111-A 《可印刷压敏型带纸背胶带 与标准FORD WSS-M99P1111-A一起使用 》.pdf

上传人:arrownail386 文档编号:745410 上传时间:2019-01-14 格式:PDF 页数:2 大小:71.01KB
下载 相关 举报
FORD ESB-M3G100-A-2005 TAPE PAPER BACKED-PRESSURE SENSITIVE-PRINTABLE  TO BE USED WITH FORD WSS-M99P1111-A  《可印刷压敏型带纸背胶带  与标准FORD WSS-M99P1111-A一起使用 》.pdf_第1页
第1页 / 共2页
FORD ESB-M3G100-A-2005 TAPE PAPER BACKED-PRESSURE SENSITIVE-PRINTABLE  TO BE USED WITH FORD WSS-M99P1111-A  《可印刷压敏型带纸背胶带  与标准FORD 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 2005 09 28 Revised Inserted 3.0; Deleted 3.1, 3.7, 4 1978 05 05 Metricated, Renumbered & Retyped CAH1-RD572066-30 1969 04 07 Released AY1-793 Printed copies are uncontrolled Copyright 2005, Ford Global Technologies, LLC Page 1 of 2 TAPE PAPER

2、BACKED-PRESSURE SENSITIVE-PRINTABLE ESB-M3G100-A 1. SCOPE The material defined by this specification is a printable, paper backed, pressure sensitive tape. 2. APPLICATION This specification was released originally for material used for temporary labeling of small parts such as acrylic body side refl

3、ectors. 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). 3.2 THICKNESS 0.007 +/- 0.001 in (ASTM D 1000) (0.18 +/- 0.03 mm) 3.3 BREAKING STRENGTH, min

4、15 lb/in (2.6 N/mm) (ASTM D 1000) 3.4 UNWIND PULL, max 35 oz/in (380 N/m) width Test Method: Condition roll of tape for 22 h at 23 +/- 2 C in a relative humidity atmosphere of 50- 55%. Place core of tape around a fixture which will allow it to revolve. Attach the free end of the tape to a 5 lb (2.3

5、kg) max limit spring scale. Pull tape from its roll at the rate of 12 in (305 mm) per min. Measure and record the unwind pull as a direct scale reading. 3.5 ADHESION TO ACRYLIC RESIN, min 16 oz/in (175 N/m) width (ASTM D 1000, except determine adhesion to acrylic resin). 3.6 AGED ADHESION The tape s

6、hall be easily removed in one piece from acrylic resin, stainless steel, anodized aluminum, zinc plated, cadmium plated, or chromium plated surfaces after the exposures listed below. No more than a trace of adhesive residue shall remain on these surfaces after the tape is removed. Any adhesive resid

7、ue must be easily cleaned from each test panel with M14J147-A Petroleum Naphtha. 3.6.1 1 week at 70 +/- 1 C 3.6.2 72 h at 38 +/- 1 C and 95-100% relative humidity ENGINEERING MATERIAL SPECIFICATIONESB-M3G100-APrinted copies are uncontrolled Copyright 2005, Ford Global Technologies, LLC Page 2 of 2 T

8、est Method: Apply a 4 in (100 mm) strip of tape to each of the following test surfaces: Acrylic resin Stainless steel Chromium plating Anodized aluminum Cadmium or zinc plating Roll the tape once in each direction with the 4.5 lb (2.0 kg) rubber covered roller described in ASTM D 1000 and expose one

9、 sample for each of the five test surfaces to the above environments. Slowly peel the tape from the test panels 2 h after exposure. Tape tearing, delamination, or excessive transfer to the test surface shall be cause for rejection. 5. GENERAL INFORMATION The information given below is provided for c

10、larification and assistance in meeting the requirements of this specification. 5.1 MATERIAL REFERENCES FOR TEST PANELS 5.1.1 Acrylic Resin: ESF-M4D9 5.1.2 Stainless Steel: ESB-M1A67 or ESB-M1A70 5.1.3 Chromium Plating: CRLC Steel or SAE 903 or 925 zinc die casting plated per ESB-M1P23. 5.1.4 Anodized Aluminum: ESB-M2A34 anodized coating per ESB-M4P6. 5.1.5 Cadmium or Zinc Plating: CRLC or HRLC steel plated per ESF-M1P5.

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 4238-1998 Aerospace Series Fibre Reinforced Plastics Determination of the Effect of Dry Heat on Physical and Mechanical Characteristics (Edition P 1)《航空航天系列 纤维增强塑料 干热.pdf ASD-STAN PREN 4238-1998 Aerospace Series Fibre Reinforced Plastics Determination of the Effect of Dry Heat on Physical and Mechanical Characteristics (Edition P 1)《航空航天系列 纤维增强塑料 干热.pdf
  • ASD-STAN PREN 4243-2001 Aerospace Series Cast Acrylic Sheets Technical Specification (Edition P 1)《航空航天系列 浇铸聚丙烯酸酯板材 技术规范 第P1版》.pdf ASD-STAN PREN 4243-2001 Aerospace Series Cast Acrylic Sheets Technical Specification (Edition P 1)《航空航天系列 浇铸聚丙烯酸酯板材 技术规范 第P1版》.pdf
  • ASD-STAN PREN 4244-1995 Aerospace Series Heat Resisting Alloy FE-PM1708 Vacuum Arc Remelted Hardened and Tempered Bar a or D is Less Than or Equal to 200 mm 1000 MPa is Less Than o.pdf ASD-STAN PREN 4244-1995 Aerospace Series Heat Resisting Alloy FE-PM1708 Vacuum Arc Remelted Hardened and Tempered Bar a or D is Less Than or Equal to 200 mm 1000 MPa is Less Than o.pdf
  • ASD-STAN PREN 4245-1995 Aerospace Series Heat Resisting Alloy FE-PM1708 Vacuum Arc Remelted As Forged Forging Stock De is Less Than or Equal to 300 mm (Edition P 1)《航空航天系列 耐热合金FE-P.pdf ASD-STAN PREN 4245-1995 Aerospace Series Heat Resisting Alloy FE-PM1708 Vacuum Arc Remelted As Forged Forging Stock De is Less Than or Equal to 300 mm (Edition P 1)《航空航天系列 耐热合金FE-P.pdf
  • ASD-STAN PREN 4246-1995 Aerospace Series Heat Resisting Alloy CO-PH4101 Vacuum Melted as Forged Forging Stock De is Less Than or Equal to 360 mm (Edition P 1)《航空航天系列 耐热合金CO-PH4101制.pdf ASD-STAN PREN 4246-1995 Aerospace Series Heat Resisting Alloy CO-PH4101 Vacuum Melted as Forged Forging Stock De is Less Than or Equal to 360 mm (Edition P 1)《航空航天系列 耐热合金CO-PH4101制.pdf
  • ASD-STAN PREN 4247-2003 Aerospace Series Aluminium Alloy AL-P2024-T42 Plate 6mm less than a Less Than or Equal to 140 mm (Edition P 2)《航空航天系列 6mm<a≤140mm的AL-P2024-T42铝合金厚板材 第P2版》.pdf ASD-STAN PREN 4247-2003 Aerospace Series Aluminium Alloy AL-P2024-T42 Plate 6mm less than a Less Than or Equal to 140 mm (Edition P 2)《航空航天系列 6mm<a≤140mm的AL-P2024-T42铝合金厚板材 第P2版》.pdf
  • ASD-STAN PREN 4248-1996 Aerospace Series Nuts Anchor Self-Locking Fixed Single Lug with Counterbore in Heat Resisting Steel Silver Plated Classification  1 100 MPa (at Ambient Temp.pdf ASD-STAN PREN 4248-1996 Aerospace Series Nuts Anchor Self-Locking Fixed Single Lug with Counterbore in Heat Resisting Steel Silver Plated Classification 1 100 MPa (at Ambient Temp.pdf
  • ASD-STAN PREN 4249-1996 Aerospace Series Nuts Anchor Self-Locking Fixed Single Lug Reduced Series with Counterbore in Heat Resisting Steel Silver Plated Classification  1 100 MPa (.pdf ASD-STAN PREN 4249-1996 Aerospace Series Nuts Anchor Self-Locking Fixed Single Lug Reduced Series with Counterbore in Heat Resisting Steel Silver Plated Classification 1 100 MPa (.pdf
  • ASD-STAN PREN 4250-2001 Aerospace Series Nickel Base Alloy NI-B41001 Filler Metal for Brazing Amorphous Foil (Edition P 2)《航空航天系列 钎焊用镍基合金NI-B41001填料金属 不定形薄膜 第P2版》.pdf ASD-STAN PREN 4250-2001 Aerospace Series Nickel Base Alloy NI-B41001 Filler Metal for Brazing Amorphous Foil (Edition P 2)《航空航天系列 钎焊用镍基合金NI-B41001填料金属 不定形薄膜 第P2版》.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