FORD ESE-M2J66-A-2012 ENAMEL BLACK BAKING FLEXIBLE FAN TO BE USED WITH FORD WSS-M99P1111-A .pdf

上传人:twoload295 文档编号:745963 上传时间:2019-01-14 格式:PDF 页数:3 大小:45.46KB
下载 相关 举报
FORD ESE-M2J66-A-2012 ENAMEL BLACK BAKING FLEXIBLE FAN  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第1页
第1页 / 共3页
FORD ESE-M2J66-A-2012 ENAMEL BLACK BAKING FLEXIBLE FAN  TO BE USED WITH FORD WSS-M99P1111-A  .pdf_第2页
第2页 / 共3页
FORD ESE-M2J66-A-2012 ENAMEL BLACK BAKING FLEXIBLE FAN  TO BE USED WITH 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 SPECIFICATION Date Action Revisions Rev 03 2012 05 04 N Status No usage or replacement N. Benipal, NA 2008 01 15 Revised Updated Format, No Technical Change 1967 04 17 Released AV3-91 Controlled document at www.MATS Copyright 2012, Ford Global Technologies, LLC Page 1 of 3 ENAM

2、EL, BLACK BAKING, FLEXIBLE FAN ESE-M2J66-A NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a black baking enamel with good flexure characteristics and corrosion resistance properties. 2. APPLICATION This specification was released originally for enamels used for

3、flexible fan assemblies. 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). 3.1 COMPOSITION 3.1.1 Non-Volatiles, min 50% (FLTM BI 102-01) 3.1.2 Toxicity

4、 The enamel shall not contain benzol (benzene), chlorinated or other toxic compounds, hydrolyzable chlorine derivatives or have any obnoxious or objectionable odor. 3.2 PHYSICAL PROPERTIES 3.2.1 Color Black 3.2.2 Specific Gravity 1.15 - 1.19 3.2.3 Viscosity 23 - 27 s (FLTM BI 111-01) 3.2.4 Shelf Sta

5、bility (FLTM BI 102-03) The enamel shall not jell or liver upon standing and must be free from settling which is not dispersed by normal agitation. An increase in viscosity over 15 s shall indicate non-stability. ENGINEERING MATERIAL SPECIFICATION ESE-M2J66-A Copyright 2012, Ford Global Technologies

6、 LLC Page 2 of 3 3.2.5 Storage Stability The material after 6 months storage, shall show no excessive settling and shall mix readily to a smooth homogeneous state. 3.3 PREPARATION OF TEST PANELS (FLTM BI 103-02) All panels shall be cold rolled low carbon steel, phosphate coated per ESB-M3P1-A. Redu

7、ce enamel to 18 +/- 1 s with M14J245 thinner. Bake 5 - 7 min at 177 C - 190 C. Dry film thickness 0.8 to 1.0 mil (21 - 25 m). 3.4 FILM PROPERTIES 3.4.1 Final Hardness, max 40 (FLTM BI 112-01) 1 h after application sward rocker hardness at 25 C. 3.4.2 Adhesion No flaking (FLTM BI 106-01, scratch and

8、pull) 3.5 RESISTANCE PROPERTIES All panels must be aged 24 h at 22 +/- 2 C before testing for resistance properties. 3.5.1 Water Immersion, min 240 h (FLTM BI 104-01) No blisters 3.5.2 Salt Spray, min 168 h (FLTM BI 103-01) 1/8 in (3 mm) maximum corrosion, blisters or creepage permitted either side

9、of scribed line. 3.5.3 Flexibility (FLTM BI 105-01) No cracks shall appear in the enamel. 3.5.4 Heat and Cooling Cycling Resistance Must withstand a temperature of 135 +/- 2 C for 4 h and then expose to -40 +/- 2 C for 4 h. The panels must then meet the requirements of paragraphs 3.4.2 and 3.5.3. 3.

10、5.5 Gasoline Resistance Shall not blister or show more than slight softening or dulling when subjected to immersion in M-14J148 (Petroleum Naphtha for 5 h at 22 +/- 2 C). ENGINEERING MATERIAL SPECIFICATION ESE-M2J66-A Copyright 2012, Ford Global Technologies, LLC Page 3 of 3 3.5.6 Hot Oil Resistance

11、 Shall not blister or show more than slight softening or dulling when subjected to immersion in hot 66 +/- 2 C ASTM Oil #3 for 5 h. 3.5.7 Ethylene Glycol Resistance Shall not blister or show more than slight softening or dulling when subjected to immersion for 1 h in boiling solution of 50% water an

12、d 50% Ford permanent anti-freeze. 5. GENERAL INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of this specification. 5.1 FLASH POINT, min 24 C (ASTM D 92) 5.2 FLAMMABILITY AND/OR TOXICITY This material represents a potential fire and/or health hazard. The Manufacturing Engineering Department must notify both the Plant Security and the Safety Personnel of its presence in the plant to assure that proper fire and/or health precautions are provided. The location in which it is used or stored must be included in the notification.

展开阅读全文
相关资源
猜你喜欢
  • EN 3745-703-2005 en Aerospace series - Fibres and cables optical aircraft use - Test methods - Part 703 Durability of manufacturer-s marking《航空航天系列 航空器用光纤和光缆的试验方法 第703部分 厂标记的耐久性》.pdf EN 3745-703-2005 en Aerospace series - Fibres and cables optical aircraft use - Test methods - Part 703 Durability of manufacturer-s marking《航空航天系列 航空器用光纤和光缆的试验方法 第703部分 厂标记的耐久性》.pdf
  • EN 3745-705-2007 en Aerospace series - Fibres and cables optical aircraft use - Test methods - Part 705 Contrast measurement《航空航天系列 飞行器用光纤和电缆的试验方法 第705部分 反差测量》.pdf EN 3745-705-2007 en Aerospace series - Fibres and cables optical aircraft use - Test methods - Part 705 Contrast measurement《航空航天系列 飞行器用光纤和电缆的试验方法 第705部分 反差测量》.pdf
  • EN 3746-2007 en Aerospace series - O-rings in fluorosilicone rubber (FVMQ) Hardness 80 IRHD《航空航天系列 氟硅酮橡胶(FVMQ)O型密封圈 硬度为80IRHD》.pdf EN 3746-2007 en Aerospace series - O-rings in fluorosilicone rubber (FVMQ) Hardness 80 IRHD《航空航天系列 氟硅酮橡胶(FVMQ)O型密封圈 硬度为80IRHD》.pdf
  • EN 3747-2007 en Aerospace series - O-rings in fluorosilicone rubber (FVMQ) - Technical specification《航空航天系列 氟硅酮橡胶(FVMQ)O型密封圈 技术规范》.pdf EN 3747-2007 en Aerospace series - O-rings in fluorosilicone rubber (FVMQ) - Technical specification《航空航天系列 氟硅酮橡胶(FVMQ)O型密封圈 技术规范》.pdf
  • EN 3748-2001 en Aerospace Series - O-Ring Grooves - Dimensions《航空航天系列 O形环槽 尺寸》.pdf EN 3748-2001 en Aerospace Series - O-Ring Grooves - Dimensions《航空航天系列 O形环槽 尺寸》.pdf
  • EN 3750-2010 en Aerospace series - Nuts anchor self-locking fixed 90 Degrees corner reduced series with counterbore in heat resisting steel MoS2 lubricated - Classification 1 100 M.pdf EN 3750-2010 en Aerospace series - Nuts anchor self-locking fixed 90 Degrees corner reduced series with counterbore in heat resisting steel MoS2 lubricated - Classification 1 100 M.pdf
  • EN 3752-2004 en Aerospace series - Nuts self-locking MJ threads in heat resisting steel FE-PA2601 (A286) MoS2 coated - Classification 1 100 MPa (at ambient temperature)  425 degree.pdf EN 3752-2004 en Aerospace series - Nuts self-locking MJ threads in heat resisting steel FE-PA2601 (A286) MoS2 coated - Classification 1 100 MPa (at ambient temperature) 425 degree.pdf
  • EN 3753-2010 en Aerospace series - Nuts anchor self-locking fixed 60 Degrees corner with counterbore in alloy steel cadmium plated MoS2 lubricated - Classification 1 100 MPa (at am.pdf EN 3753-2010 en Aerospace series - Nuts anchor self-locking fixed 60 Degrees corner with counterbore in alloy steel cadmium plated MoS2 lubricated - Classification 1 100 MPa (at am.pdf
  • EN 3757-2009 en Aerospace series - Nuts anchor self-locking floating selfaligning two lugs in heat resisting steel MoS2 lubricated - Classification 900 MPa (at ambient temperature).pdf EN 3757-2009 en Aerospace series - Nuts anchor self-locking floating selfaligning two lugs in heat resisting steel MoS2 lubricated - Classification 900 MPa (at ambient temperature).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