FORD WSK-M3D176-A2-2005 PHENOLIC (PF) 30% GLASS FIBER REINFORCED COMPRESSION MOLDING COMPOUND TO BE USED WITH FORD WSS-M99P1111-A 《酚醛树脂(PF)30%玻璃纤维增强的模压成型料 与标准FORD WSS-M99P1111-A.pdf

上传人:progressking105 文档编号:750554 上传时间:2019-01-14 格式:PDF 页数:4 大小:141.54KB
下载 相关 举报
FORD WSK-M3D176-A2-2005 PHENOLIC (PF) 30% GLASS FIBER REINFORCED COMPRESSION MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《酚醛树脂(PF)30%玻璃纤维增强的模压成型料  与标准FORD WSS-M99P1111-A.pdf_第1页
第1页 / 共4页
FORD WSK-M3D176-A2-2005 PHENOLIC (PF) 30% GLASS FIBER REINFORCED COMPRESSION MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《酚醛树脂(PF)30%玻璃纤维增强的模压成型料  与标准FORD WSS-M99P1111-A.pdf_第2页
第2页 / 共4页
FORD WSK-M3D176-A2-2005 PHENOLIC (PF) 30% GLASS FIBER REINFORCED COMPRESSION MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《酚醛树脂(PF)30%玻璃纤维增强的模压成型料  与标准FORD WSS-M99P1111-A.pdf_第3页
第3页 / 共4页
FORD WSK-M3D176-A2-2005 PHENOLIC (PF) 30% GLASS FIBER REINFORCED COMPRESSION MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《酚醛树脂(PF)30%玻璃纤维增强的模压成型料  与标准FORD WSS-M99P1111-A.pdf_第4页
第4页 / 共4页
亲,该文档总共4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 01 04 Revised Inserted 3.0; Deleted 3.1, 3.2, 3.3, 3.7, 3.8 & 4 1994 12 01 Released EP00E10348618000 K. GerhardsPrinted copies are uncontrolled Copyright 2005, Ford Global Technologies, LLC Page 1 of 4 PHENOLIC (PF) 30% GLASS FIBER REINFO

2、RCED WSK-M3D176-A2 COMPRESSION MOLDING COMPOUND 1. SCOPE The material defined by this specification is a 30% glass fiber reinforced thermosetting compression molding compound based on phenolics. 2. APPLICATION This specification was released originally for material used as alternator thermal cover.

3、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). 3.1.1 All requirements of this specification, identified by symbol(s), shall be met with data represe

4、nting 3 sigma values. 3.4 MOLDING COMPOUND (s) 3.4.1 Filler Content 3.4.1.1 Ash Content 71 +/- 5% (ISO 3451/1, Method A, 1 h at 650 +/- 25 C) 3.4.1.2 Glass Fiber Content By Weight 30 +/- 3% Test Method: ISO 3451/1, Method B, 1 h at 650 +/- 25 C, except use 5% by volume hydrochloric acid solution for

5、 15 minutes. Rinse the glass fibers several times with distilled water before drying in an oven for 2 h at 120 +/- 2 C. After cooling, weigh the crucibles and calculate the percent glass fibers. 3.5 MOLDED TEST SPECIMEN 3.5.1 Preparation of Test Specimens Unless otherwise specified all tests shall b

6、e carried out on injection molded one-end gated test specimens. The following dimensions are required: A. 150 min x 10 x 4.0 +/- 0.2 mm (Tensile Bar, ISO 3167) B. 120 x 10 x 4.0 +/- 0.2 mm C. 13 x 13 x 25 mm (Compressive Strength Bar, ASTM D 695) ENGINEERING MATERIAL SPECIFICATIONWSK-M3D176-A2Printe

7、d copies are uncontrolled Copyright 2005, Ford Global Technologies, LLC Page 2 of 4 Specimens with shorter dimensions shall be cut from the center portion of the test specimen A and/or B. The specimens shall be prepared under optimum conditions as defined by the manufacturer of raw materials. No ann

8、ealing allowed. 3.5.2 Density 1.95 - 2.00 g/cm3(ISO 1183, Method A) (s) 3.5.3 Tensile Strength at Max Load, min 25 MPa (ISO R 527, 150 min x 10 x 4.0 +/- 0.2 mm specimen, 5 mm/min test speed) (s) 3.5.4 Flexural Modulus, min 9 GPa (ISO 178, 80 x 10 x 4.0 +/- 0.2 mm specimen, 2 mm/min test speed, 64 m

9、m support span) 3.5.5 Flexural Strength, min 65 MPa (ISO 178, 80 x 10 x 4.0 +/- 0.2 mm specimen, 2 mm/min test speed, 64 mm support span) 3.5.6 Shear Modulus at 23 C Range - GPa (ASTM D 4065, forced constant amplitude, fixed frequency of 1 Hz +/- 15%, strain level below 1%. Specimen approx. 60 x 10

10、x 4.0 +/- 0.2 mm cut from the center of specimen A. Specimen length between clamps 35-40 mm. Soak time at each temperature interval - 3 minutes minimum) Additionally, a Shear Modulus versus Temperature curve shall be plotted for -50 to +280 C temperature range, at 5 C minimum intervals. The plotted

11、curve must be within tolerance range shown on page 4. (s) 3.5.7 Impact Strength, Izod, min (ISO 180/1A, 80 x 10 x 4.0 +/- 0.2 mm specimen, 10 specimens for each test) 3.5.7.1 At 23 +/- 2 C 10 kJ/m23.5.7.2 At -40 +/- 1 C 10 kJ/m2The test specimens must be conditioned for minimum of 6 h at the above s

12、pecified temperature prior to impact test. Low temperature testing shall be done within the cold box. (s) 3.5.8 Heat Deflection Temperature, min 160 C (ISO 75, 120 x 10 x 4.0 +/- 0.2 mm specimen, edgewise, 0.32 +/- 0.01 mm deflection. At 1.80 MPa) ENGINEERING MATERIAL SPECIFICATIONWSK-M3D176-A2Print

13、ed copies are uncontrolled Copyright 2005, Ford Global Technologies, LLC Page 3 of 4 3.5.9 Heat Aging Performance (ISO 188, except 150 +/- 50 air changes/h, 1000 h at 160 +/- 2 C. Unaged property values shall be determined at the time of the aged properties determination) 3.5.9.1 Tensile Strength at

14、 Max Load Change +/- 25% (Test Method per para 3.5.3) 3.5.9.2 Flexural Strength Change +/- 25% (Test Method per para 3.5.5) 3.6 FLAMMABILITY (ISO 3795) Burn Rate, max 100 mm/minute The specimen size required for material approval is 355 x 100 x 4.0 +/- 0.1 mm with a smooth surface. 5. GENERAL INFORM

15、ATION The information below is provided for clarification and assistance in meeting the requirements of this specification. 5.1 COEFFICIENT OF LINEAR THERMAL EXPANSION 16-6/ C (ASTM E 228 or TMA, temperature range -30 - +30 C) 5.2 MOLD SHRINKAGE (ISO 2577, approx. 150 x 100 x 3.2 +/- 0.2 mm injectio

16、n molded specimen) 5.2.1 Molding Shrinkage . After 48 h at 23 +/- 2 C +/- 0 5.2.2 Post Shrinkage . After 48 h at 120 C +/- 0 5.3 COMPRESSIVE STRENGTH 155 MPa (ASTM D 695, 13 x 13 x 25 mm specimen, 1.3 mm/minute test speed) 5.4 WATER ABSORPTION 2.3% (ISO 62, 24 h, boiling water, compression molded multipurpose specimen 150 min x 10 x 4.0 +/- 0.2 mm) 5.5 RECYCLING CODE PF-GF30ENGINEERING MATERIAL SPECIFICATIONWSK-M3D176-A2Printed copies are uncontrolled Copyright 2005, Ford Global Technologies, LLC Page 4 of 4

展开阅读全文
相关资源
猜你喜欢
  • ASD-STAN PREN 3219-1988 Aerospace Series Heat Resisting Nickel Base Alloy (Ni-P101HT) Cold Worked and Softened Bar and Wire for Continuous Forging or Extrusion for Fasteners 3 Less.pdf ASD-STAN PREN 3219-1988 Aerospace Series Heat Resisting Nickel Base Alloy (Ni-P101HT) Cold Worked and Softened Bar and Wire for Continuous Forging or Extrusion for Fasteners 3 Less.pdf
  • ASD-STAN PREN 3220-1988 Aerospace Series Heat Resisting Nickel Base Alloy (Ni-P101HT) Cold Worked and Softened Bar and Wire for Continuous Forging or Extrusion for Fasteners 3 Less.pdf ASD-STAN PREN 3220-1988 Aerospace Series Heat Resisting Nickel Base Alloy (Ni-P101HT) Cold Worked and Softened Bar and Wire for Continuous Forging or Extrusion for Fasteners 3 Less.pdf
  • ASD-STAN PREN 3225-1-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 1 - General Req.pdf ASD-STAN PREN 3225-1-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 1 - General Req.pdf
  • ASD-STAN PREN 3225-2-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 2 - Atomized Po.pdf ASD-STAN PREN 3225-2-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 2 - Atomized Po.pdf
  • ASD-STAN PREN 3225-3-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 3 - Hot Compact.pdf ASD-STAN PREN 3225-3-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 3 - Hot Compact.pdf
  • ASD-STAN PREN 3225-4-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 4 - Pre-Product.pdf ASD-STAN PREN 3225-4-1993 Aerospace Series Heat Resisting Alloys Produced from Atomized Powder Powder Compacted Forging Stock and Parts Technical Specification Part 4 - Pre-Product.pdf
  • ASD-STAN PREN 3226-1992 Aerospace Series Nuts Hexagon Plain Normal Height Normal Across Flats in Steel Cadmium Plated Classification 1 100 MPa (at Ambient Temperature)  235 Degrees.pdf ASD-STAN PREN 3226-1992 Aerospace Series Nuts Hexagon Plain Normal Height Normal Across Flats in Steel Cadmium Plated Classification 1 100 MPa (at Ambient Temperature) 235 Degrees.pdf
  • ASD-STAN PREN 3227-1992 Aerospace Series Nuts Hexagon Plain Normal Height Normal Across Flats in Steel Cadmium Plated Left Hand Thread Classification 1 100 MPa (at Ambient Temperat.pdf ASD-STAN PREN 3227-1992 Aerospace Series Nuts Hexagon Plain Normal Height Normal Across Flats in Steel Cadmium Plated Left Hand Thread Classification 1 100 MPa (at Ambient Temperat.pdf
  • ASD-STAN PREN 3228-1992 Aerospace Series Nuts Hexagon Plain Reduced Height Normal Across Flats in Steel Cadmium Plated Classification 900 MPa (at Ambient Temperature)  235 Degrees .pdf ASD-STAN PREN 3228-1992 Aerospace Series Nuts Hexagon Plain Reduced Height Normal Across Flats in Steel Cadmium Plated Classification 900 MPa (at Ambient Temperature) 235 Degrees .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