FORD WM961-1996 PERFORMANCE TESTING FOR THE RETAINING FEATURES ON PLASTIC FASTENERS《塑料紧固件的保持特性的性能试验》.pdf

上传人:priceawful190 文档编号:748584 上传时间:2019-01-14 格式:PDF 页数:3 大小:20KB
下载 相关 举报
FORD WM961-1996 PERFORMANCE TESTING FOR THE RETAINING FEATURES ON PLASTIC FASTENERS《塑料紧固件的保持特性的性能试验》.pdf_第1页
第1页 / 共3页
FORD WM961-1996 PERFORMANCE TESTING FOR THE RETAINING FEATURES ON PLASTIC FASTENERS《塑料紧固件的保持特性的性能试验》.pdf_第2页
第2页 / 共3页
FORD WM961-1996 PERFORMANCE TESTING FOR THE RETAINING FEATURES ON PLASTIC FASTENERS《塑料紧固件的保持特性的性能试验》.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、FORD WORLDWIDE FASTENER STANDARDDate: 1996-10-01Engineering Standards & 1 of 3 Printed copies are uncontrolled .Systems Engineering (ESSE)WM 961Performance Testing for the Retaining Features on Plastic Fasteners1. SCOPE. This standard covers the test methods for establishing the performance of panel

2、 retainingfeatures for various fasteners.Fir Tree/Bayonet and other push-in types.“T“ Weld Stud type.Weld Stud typePanel Edge type.The standard also covers the test methods for establishing the performance of pipe retaining features forvarious plastic pipe clips.Latch typePush-in type2. APPLICATION.

3、 This standard will normally be applied to plastic fasteners with a feature designed toretain the part in a panel hole, on welded “T“ stud attached to a panel, on a welded stud attached to apanel, or on the edge of a panel in a specially designed hole. It may also be applied to plastic plugs ortrim

4、retaining buttons.The standard can also be applied to plastic pipe clips such as latch and push-in (this includes spacer andswivel) type features.3. PERFORMANCE TEST METHODS.3.1 PANEL RETAINING FEATURE.3.1.1 FIR TREE/BAYONET AND OTHER PUSH-IN TYPE FEATURES.Figure 1 - Typical Fir Tree, Bayonet and Ot

5、her Push-in Type FeaturesThe feature shall be pushed into a hole in a steel test plate and the force measured. Thefeature shall then be pulled out of the test plate and the force measured.The diameter of the hole in the test plate, the thickness of the test plate, the maximum push-in force and the m

6、inimum pull-out force shall be as specified on the Ford drawingfor the part.FORD WORLDWIDE FASTENER STANDARDDate: 1996-10-01Engineering Standards & 2 of 3 Printed copies are uncontrolled .Systems Engineering (ESSE)WM 961Performance Testing for the Retaining Features on Plastic Fasteners3.1.2 “T“ Wel

7、d Stud Type FeatureFigure 2 - Typical “T“ Weld StudThe feature shall be pushed on to a steel “T“ welded stud in direction F 1 which meets thedimensional requirements of Ford part number W700569 and the force measured. Thefeature shall then be pulled off the “T“ welded stud in direction F 2 and the f

8、orce measured.The maximum push-on and the minimum pull-off forces shall be as specified on the Forddrawing for the part.Figure 3 - Typical Weld Stud3.1.3 Special Thread Weld Stud Type FeatureThe retaining feature molded into plastic parts to be used on special thread weld studs isoptional provided w

9、hen tested on a stud with the dimensional requirements of W700121(pushed-on and pulled-off) the maximum push-on force and the minimum pull-off forcesare specified on the Ford drawing.3.1.4 Panel Edge Type FeatureFigure 4 - Typical Panel Edge FeatureThe feature shall be pushed on to a steel test plat

10、e until securely fitted in the retaininghole and the force measured. The feature shall then be pulled off the test plate and theforce measured. The hole in the test plate, the thickness of the test plate, the maximumpush-on force and the minimum pull-off force shall be as specified on the Ford drawi

11、ngfor the part.FORD WORLDWIDE FASTENER STANDARDDate: 1996-10-01Engineering Standards & 3 of 3 Printed copies are uncontrolled .Systems Engineering (ESSE)WM 961Performance Testing for the Retaining Features on Plastic Fasteners3.2 Pipe Retaining Features3.2.1 Latch Type FeaturesFigure 5 - Typical Lat

12、ch FeatureThe Latch feature shall be closed securely so as to retain appropriate steel test mandrelsand the force (push-on) measured. Forces shall be applied to the assembly such that thelatch feature is loaded until failure occurs (latch pulls apart). The minimum force to causefailure shall be reco

13、rded.The test mandrels diameters shall have a tolerance of +/-0.1 and the assembly conditionsof the mandrels shall be as stated on the Ford drawing for the part.The maximum push-on force and the minimum pull-apart force for the feature shall be asspecified on the Ford drawing.3.2.2 Push In Type Feat

14、uresFigure 6 - Typical Push-In FeatureThe mandrels shall be pushed into the feature in the directions shown on the Forddrawing for the part and the forces recorded. The mandrels shall then be pulled out in theopposite direction and forces recorded.The test mandrels diameters shall have a tolerance o

15、f +/-0.1 and the assembly conditionsof the mandrels shall be as stated on the Ford drawing for the part.The maximum push-in force and the minimum pull-out force shall be as specified on theFord drawing for the part.4. GENERALAll testing shall be carried out at ambient temperature (23 c +/-2).The speed of testing shall be 100mm +/-5 per minute.NOTE : This does not apply to the testing of the latch type features.

展开阅读全文
相关资源
猜你喜欢
  • DIN EN 3145-2003 Aerospace series - Round bars hot rolled in steel - Normal tolerances Diameter 6 mm D 250 mm Dimensions German and English version EN 3145 2001《航空航天系列 热轧圆钢棒 标称公差 直.pdf DIN EN 3145-2003 Aerospace series - Round bars hot rolled in steel - Normal tolerances Diameter 6 mm D 250 mm Dimensions German and English version EN 3145 2001《航空航天系列 热轧圆钢棒 标称公差 直.pdf
  • DIN EN 3146-2003 Aerospace series - Round bars hot rolled in steel close tolerances diameter 6 mmD250 mm - Dimensions German and English version EN 3146 2001《航空航天系列 紧公差、直径6mm D 250.pdf DIN EN 3146-2003 Aerospace series - Round bars hot rolled in steel close tolerances diameter 6 mmD250 mm - Dimensions German and English version EN 3146 2001《航空航天系列 紧公差、直径6mm D 250.pdf
  • DIN EN 3148-2009 Aerospace series - Shank nuts self-locking flange restrained - Installation procedure German and English version EN 3148 2008《航空航天系列 法兰受控自锁紧细牙杆螺母 安装程序》.pdf DIN EN 3148-2009 Aerospace series - Shank nuts self-locking flange restrained - Installation procedure German and English version EN 3148 2008《航空航天系列 法兰受控自锁紧细牙杆螺母 安装程序》.pdf
  • DIN EN 3149-1996 Aerospace series - Shank nuts - Installation holes 60 swage flanges - Design standard German version EN 3149 1996《航空航天系列 铆接螺母 60度扩径安装孔法兰 设计标准》.pdf DIN EN 3149-1996 Aerospace series - Shank nuts - Installation holes 60 swage flanges - Design standard German version EN 3149 1996《航空航天系列 铆接螺母 60度扩径安装孔法兰 设计标准》.pdf
  • DIN EN 315-2000 Plywood - Tolerances for dimensions German version EN 315 2000《胶合板 尺寸公差》.pdf DIN EN 315-2000 Plywood - Tolerances for dimensions German version EN 315 2000《胶合板 尺寸公差》.pdf
  • DIN EN 3150-1995 Aerospace series - Pins shoulder headless in heat resisting nickel base alloy NI-P100HT (Inconel 718) German version EN 3150 1995《航空航天系列 耐高温镍基合金NI-P100HI(因康718)无头台.pdf DIN EN 3150-1995 Aerospace series - Pins shoulder headless in heat resisting nickel base alloy NI-P100HT (Inconel 718) German version EN 3150 1995《航空航天系列 耐高温镍基合金NI-P100HI(因康718)无头台.pdf
  • DIN EN 3151-1995 Aerospace series - Dowels plain in heat resisting nickel base alloy NI-P100HT (Inconel 718) German version EN 3151 1995《航空航天系列 耐高温镍基合金NI-P100HI(因康718)普通定位销 德文版本 EN.pdf DIN EN 3151-1995 Aerospace series - Dowels plain in heat resisting nickel base alloy NI-P100HT (Inconel 718) German version EN 3151 1995《航空航天系列 耐高温镍基合金NI-P100HI(因康718)普通定位销 德文版本 EN.pdf
  • DIN EN 3152-2005 de en 8930 Aerospace series - Nuts self-locking MJ threads in heat resisting steel FE-PA2601 (A286) silver plated or uncoated - Classification 1100 MPa (at ambient.pdf DIN EN 3152-2005 de en 8930 Aerospace series - Nuts self-locking MJ threads in heat resisting steel FE-PA2601 (A286) silver plated or uncoated - Classification 1100 MPa (at ambient.pdf
  • DIN EN 3155-001-2016 Aerospace series - Electrical contacts used in elements of connection - Part 001 Technical Specification German and English version EN 3155-001 2016《航空航天系列 连接元.pdf DIN EN 3155-001-2016 Aerospace series - Electrical contacts used in elements of connection - Part 001 Technical Specification German and English version EN 3155-001 2016《航空航天系列 连接元.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