FORD WSB-M7C90-A-2004 RUST PREVENTIVE WATER BORNE TO BE USED WITH FORD WSS-M99P1111-A 《水性防锈剂 与标准FORD WSS-M99P1111-A一起使用 》.pdf

上传人:eastlab115 文档编号:749227 上传时间:2019-01-14 格式:PDF 页数:3 大小:76.08KB
下载 相关 举报
FORD WSB-M7C90-A-2004 RUST PREVENTIVE WATER BORNE  TO BE USED WITH FORD WSS-M99P1111-A  《水性防锈剂  与标准FORD WSS-M99P1111-A一起使用 》.pdf_第1页
第1页 / 共3页
FORD WSB-M7C90-A-2004 RUST PREVENTIVE WATER BORNE  TO BE USED WITH FORD WSS-M99P1111-A  《水性防锈剂  与标准FORD WSS-M99P1111-A一起使用 》.pdf_第2页
第2页 / 共3页
FORD WSB-M7C90-A-2004 RUST PREVENTIVE WATER BORNE  TO BE USED WITH FORD WSS-M99P1111-A  《水性防锈剂  与标准FORD WSS-M99P1111-A一起使用 》.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 03 11 Revised Para 3.0 inserted; paras 3.1, 3.2, 3.3, 3.9 and 4 deleted 1995 08 16 Activated J. A. Faunt Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 1 of 3 RUST PREVENTIVE, WATER BORNE WSB-M7C90-A 1.

2、 SCOPE The material defined by this specification is an alkaline strippable water borne rust preventive compound consisting of wax modified acrylic compounds. 2. APPLICATION This specification was released originally for material used to provide protection to the inside surfaces of bumpers made of c

3、hrome plated steel or bare, chrome plated and anodized aluminum materials. The materials dry to a soft, homogeneous film. 3. REQUIREMENTS 3.0 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materia

4、ls (WSS-M99P1111-A). 3.4 PHYSICAL PROPERTIES 3.4.1 Non-volatiles, min 32% (FLTM BI 102-01) 3.4.2 Color Smoke 3.4.3 Flash Point, min 93 C (ASTM D 93) 3.4.4 Shelf Stability, min 6 months The material shall be stored at ambient room temperature below 38 C away from all sources of heat. DO NOT FREEZE. 3

5、4.5 Weight per Volume 1.04 +/- 0.03 kg/L (ASTM D 1475) 3.4.6 Viscosity (ASTM D 2196, Method B, use #5 spindle) 20 RPM 6000 +/- 1500 mPa.s 100 RPM 2000 +/- 500 mPa.s ENGINEERING MATERIAL SPECIFICATIONWSB-M7C90-APrinted copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 2 of 3

6、 3.5 PREPARATION OF TEST PANELS (ASTM D 609, Method A) 3.5.1 Substrate In addition to the substrates in ASTM D 609, bumper sections will be prepared and dried per 3.6.2 and evaluated per para 3.7. 3.5.2 Application Procedure Spray the test compound to a dry film thickness of 45 to 55 micrometres usi

7、ng an airless spray pump equipped with appropriate size orifice to produce a “flat“ (in one plane) spray pattern. 3.6 DRY FILM PROPERTIES 3.6.1 Application Temperature 20 - 30 C 3.6.2 Drying Time Material must be tack free (no transfer of material to the fingertip after application of light pressure

8、) after 30 minutes at 23 +/- 2 C. 3.6.3 Dry Film Thickness, min 45 micrometres (ASTM D 1212) 3.6.4 Crack Resistance (FLTM BJ 128-03) No cracks, voids or shrinkage are to be evident. 3.7 RESISTANCE PROPERTIES 3.7.1 Salt Spray Resistance, min 500 h (ASTM B 117) 3.7.2 Resistance to UV Exposure, min 144

9、 h (ASTM G 53) No mud cracking or other surface failure. 3.7.2.1 Salt Spray Resistance After 336 h Exposure, min (ASTM B 117) Expose 3.7.2 panel to salt spray per ASTM B 117. No mud cracking or other surface failure. ENGINEERING MATERIAL SPECIFICATIONWSB-M7C90-APrinted copies are uncontrolled Copyri

10、ght 2004, Ford Global Technologies, LLC Page 3 of 3 3.7.3 Detergent Wash Resistance (FLTM BV 116-02, modified) 3.7.3.1 Apparatus and Materials Required Detergent: Select a detergent used commercially, that has a pH range of 7.0 to 7.5 when diluted to normal use concentration. Dupont # 7 Car Wash Con

11、centrate Borden Chemicals Columbus, Ohio or equivalent 3.7.3.2 Para A, line 3 of FLTM BV 116-02 shall read: 50 +/- 2 C. 3.7.3.3 Para A, line 4 of FLTM BV 116-02 shall read: 24 hours, min. 3.7.3.4 Para B, line 1 of FLTM BV 116-02 shall read: 30 seconds duration. 3.7.4 Corrosion Resistance, min 40 cyc

12、les (FLTM BI 123-01) There shall be no more than 1% of the surface covered with corrosion and not more than 4.8 mm of corrosion creep-in from the edges. No perforations or deep pitting permitted. 3.7.5 Freeze-Thaw Resistance, min 3 cycles Place test panels into a freezer set at - 30 +/- 2 C for one

13、hour. Remove the panels and store at room temperature for one hour. Examine panels. This completes the cycle. The material must not crack, peel or lift from the surface of the test panel. 3.7.6 Heat Resistance, 121 C, min 1 h (FLTM BV 118-01, modified, material applied per para 3.5.2) Any evidence o

14、f flow shall constitute a failure. 3.7.7 Chip Resistance at 0 C 3 C or better (ASTM D 3170) Panels coated per para 3.5, conditioned per para 3.3 of this specification, then conditioned per para 4.4 of ASTM D 3170; shall not exceed a chip rating of 3 C. 3.7.8 Stress Cracking Resistance No cracking or (FLTM BO 127-03) crazing 3.7.8.1 Para 3 - evaluate 1% strain 3.7.8.2 Para 6 - 24 hour soak with coating at 23 +/- 2 C and at 58 +/- 2 C.

展开阅读全文
相关资源
猜你喜欢
  • DIN 65576-1991 Aerospace quick-release pins in corrosion-resisting steel single locked with self-retaining cam lever release mechanism《航空航天 带自限动凸轮杆释放机构的单锁定耐蚀钢快卸销》.pdf DIN 65576-1991 Aerospace quick-release pins in corrosion-resisting steel single locked with self-retaining cam lever release mechanism《航空航天 带自限动凸轮杆释放机构的单锁定耐蚀钢快卸销》.pdf
  • DIN 65578-1991 Aerospace quick-release pins in corrosion-resisting steel single locked with pull or push release mechanism《航空航天 带推或拉释放机构的单锁定装置耐蚀钢快卸销》.pdf DIN 65578-1991 Aerospace quick-release pins in corrosion-resisting steel single locked with pull or push release mechanism《航空航天 带推或拉释放机构的单锁定装置耐蚀钢快卸销》.pdf
  • DIN 65581-1992 Aerospace titanium-alloy close-tolerance rivets and pure-titanium collars metric series technical specification《航空航天 米制系列的钛合金制紧公差铆钉和纯钛销套 技术规范》.pdf DIN 65581-1992 Aerospace titanium-alloy close-tolerance rivets and pure-titanium collars metric series technical specification《航空航天 米制系列的钛合金制紧公差铆钉和纯钛销套 技术规范》.pdf
  • DIN 65582-1990 Aerospace heat treatment of aluminium- and magnesium-alloy castings《航空航天 铝和镁合金铸件的热处理》.pdf DIN 65582-1990 Aerospace heat treatment of aluminium- and magnesium-alloy castings《航空航天 铝和镁合金铸件的热处理》.pdf
  • DIN 65583-1999 Aerospace - Fibre reinforced materials - Determination of glass transition of fibre composites under dynamic load《航空航天 纤维增强塑料 动态负荷下纤维复合材料的玻璃化转变的测定》.pdf DIN 65583-1999 Aerospace - Fibre reinforced materials - Determination of glass transition of fibre composites under dynamic load《航空航天 纤维增强塑料 动态负荷下纤维复合材料的玻璃化转变的测定》.pdf
  • DIN 65587-1992 Aerospace webbing technical specification《航空航天 织物带 技术规范》.pdf DIN 65587-1992 Aerospace webbing technical specification《航空航天 织物带 技术规范》.pdf
  • DIN 65590-1992 Aerospace braided cord technical specification《航空航天 编织绳索 技术规范》.pdf DIN 65590-1992 Aerospace braided cord technical specification《航空航天 编织绳索 技术规范》.pdf
  • DIN 65591-1998 Aerospace - Broad woven fabric uncoated - Technical specification《航空航天 非涂层的宽幅织物 技术规范》.pdf DIN 65591-1998 Aerospace - Broad woven fabric uncoated - Technical specification《航空航天 非涂层的宽幅织物 技术规范》.pdf
  • DIN 65594-1993 Aerospace closing heads for solid rivets pan head inch based series《航空和航天 英制系列盘头实心铆钉的铆钉上头》.pdf DIN 65594-1993 Aerospace closing heads for solid rivets pan head inch based series《航空和航天 英制系列盘头实心铆钉的铆钉上头》.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