FORD WSB-M3D173-A2-2004 UNSATURATED POLYESTER (UP) 40% GLASS FIBER REINFORCED SHEET MOLDING COMPOUND TO BE USED WITH FORD WSS-M99P1111-A 《40%玻璃纤维增强的不饱和聚酯(UP)片状成型料 与标准FORD WSS-M9.pdf

上传人:livefirmly316 文档编号:749029 上传时间:2019-01-14 格式:PDF 页数:5 大小:125.36KB
下载 相关 举报
FORD WSB-M3D173-A2-2004 UNSATURATED POLYESTER (UP) 40% GLASS FIBER REINFORCED SHEET MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《40%玻璃纤维增强的不饱和聚酯(UP)片状成型料  与标准FORD WSS-M9.pdf_第1页
第1页 / 共5页
FORD WSB-M3D173-A2-2004 UNSATURATED POLYESTER (UP) 40% GLASS FIBER REINFORCED SHEET MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《40%玻璃纤维增强的不饱和聚酯(UP)片状成型料  与标准FORD WSS-M9.pdf_第2页
第2页 / 共5页
FORD WSB-M3D173-A2-2004 UNSATURATED POLYESTER (UP) 40% GLASS FIBER REINFORCED SHEET MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《40%玻璃纤维增强的不饱和聚酯(UP)片状成型料  与标准FORD WSS-M9.pdf_第3页
第3页 / 共5页
FORD WSB-M3D173-A2-2004 UNSATURATED POLYESTER (UP) 40% GLASS FIBER REINFORCED SHEET MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《40%玻璃纤维增强的不饱和聚酯(UP)片状成型料  与标准FORD WSS-M9.pdf_第4页
第4页 / 共5页
FORD WSB-M3D173-A2-2004 UNSATURATED POLYESTER (UP) 40% GLASS FIBER REINFORCED SHEET MOLDING COMPOUND  TO BE USED WITH FORD WSS-M99P1111-A  《40%玻璃纤维增强的不饱和聚酯(UP)片状成型料  与标准FORD WSS-M9.pdf_第5页
第5页 / 共5页
亲,该文档总共5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 12 21 Revised Inserted 3.0; Deleted 31, 3.2, 3.3, 3.7, 3.8 & 4 1994 11 07 Released NB00I10043054383 M. TrappPrinted copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 1 of 5 UNSATURATED POLYESTER (UP), 40% GLASS FI

2、BER REINFORCED WSB-M3D173-A2 SHEET MOLDING COMPOUND 1. SCOPE The material defined by this specification is a 25 mm minimum long glass fiber reinforced unsaturated polyester (UP) sheet molding compound. 2. APPLICATION This specification was released originally for material used for cross-car truck be

3、ams. 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 r

4、epresenting 3 sigma values. 3.4 MOLDED TEST SPECIMEN 3.4.1 Preparation of Test Specimens All test specimens shall be prepared from cross-ply molded plaques or equivalent. The plaques are to be manufactured from the same material and under equivalent conditions as production parts. The plaques shall

5、have the following dimensions. 300 x 300 mm, minimum x 2.5 +/- 0.2 mm Prepared specimens must show no evidence of fiber tear or loose fiber strands protruding from the specimens. No additional annealing of specimens is allowed. 3.4.2 Density 1.75 - 2.05 g/cm3(ISO 1183, Method A) (s) 3.4.3 Filler Con

6、tent 3.4.3.1 Ash Content 52 - 72% (ISO 3451/1, Method A, 1 h at 650 +/- 25 C) 3.4.3.2 Glass Fiber Content, by Weight 30 - 47% Test Method: ISO 3451/1, Method B, 1 h at 650 +/- 25 C, except use 5% by volume hydrochloric acid solution for 15 minutes. Rinse the glass fibers several times with distilled

7、 water before drying in an oven for 2 h at 120 +/- 2 C. After cooling, weigh the crucibles and calculate the percent glass fibers. ENGINEERING MATERIAL SPECIFICATIONWSB-M3D173-A2Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 2 of 5 3.4.3.3 Glass Fiber Length, min

8、25 mm (Optical evaluation method) (s) 3.4.4 Tensile Strength at Break, min 68 MPa (ISO R 527, 150 minimum x 25 x 2.5 +/- 0.2 mm specimen, 5 mm/min test speed) (s) 3.4.5 Flexural Modulus, min 8.5 GPa (ISO 178, 60 x 25 x 2.5 +/- 0.2 mm specimen, 40 mm support span, 2 mm/minute test speed) (s) 3.4.6 Fl

9、exural Strength, min 179 MPa (ISO 178, 60 x 10 x 2.5 +/- 0.2 mm specimen, 40 mm support span 2 mm/minute test speed) 3.4.7 Shear Modulus At 23 C 3.9 - 6.5 GPa (ASTM D 4065, forced constant amplitude, fixed frequency of 1 Hz +/- 15%, strain level below 1%. Specimen approx. 60 x 10 x 4.0 +/- 0.2 mm cu

10、t 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 vs. Temperature curve shall be plotted for -50 to +290 C temperature range, at 5 C minimum intervals. The plotted curve must be within t

11、olerance range shown on page 6. (s) 3.4.8 Impact Strength, Izod, min (ISO 180/Method A, 63.5 x 12.7 x 2.5 +/- 0.2 mm specimen, 10 specimens minimum) 3.4.8.1 At 23 +/- 2 C 72 kJ/m23.4.8.2 At -40 +/- 2 C 87 kJ/m2The test specimens must be conditioned for minimum of 6 h at the above specified temperatu

12、re prior to impact test. Low temperature testing shall be done within the cold box. (s) 3.4.9 Heat Deflection Temperature, min 250 C (ISO 75, 120 x 10 x 2.5 +/- 0.2 mm specimen, 0.32 +/- 0.01 mm deflection. At 1.80 MPa) (s) 3.4.10 Water Absorption, max 0.7% (ISO 62, 24 h, 50 x 50 x 2.5 +/- 0.2 mm sp

13、ecimen ENGINEERING MATERIAL SPECIFICATIONWSB-M3D173-A2Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 3 of 5 3.4.11 Heat Aging Performance (ISO 188, except 150 +/- 50 air changes/h, 1000 h at 150 +/- 2 C. Unaged property values shall be determined at the time of th

14、e aged properties determination) 3.4.11.1 Tensile Strength at Max Load Change +/- 36% (Test Method per para 3.4.4) 3.4.11.2 Flexural Strength Change +/- 39% (Test Method per para 3.4.6) 3.4.11.3 Impact Strength, Izod Change +/ 41% (Test Method per para 3.4.8.1, specimens to be notched before heat ag

15、ing) 3.5 FOGGING (FLTM BO 116-03, 3 h at 100 C heating, 21 C cooling plate) Fog Number, min 80 Formation of clear film, droplets or crystals is cause for rejection. Interpretation of results: The acceptability of any material must be based on evaluation of all three glass plates. Questions on interp

16、retation of results should be directed to the responsible Materials Engineering Activity. 3.6 FLAMMABILITY (ISO 3795) Burn Rate, max 100 mm/minute Self-Extinguishing (SE) The specimen size required for material approval is 355 x 100 x 2.5 +/- 0.1 mm with a smooth surface. 5. GENERAL INFORMATION The

17、information given below is provided for clarification and assistance in meeting the requirements of this specification. 5.1 COEFFICIENT OF LINEAR THERMAL EXPANSION 2.33-5/ C (ASTM E 228 or TMA, temperature range -30 to +30 C) ENGINEERING MATERIAL SPECIFICATIONWSB-M3D173-A2Printed copies are uncontro

18、lled Copyright 2004, Ford Global Technologies, LLC Page 4 of 5 5.2 MOLD SHRINKAGE (ISO 2577, approx. 300 x 300 x 2.5 +/- 0.2 mm compression molded specimen) 5.2.1 Molding Shrinkage . After 48 h at 23 +/- 2 C 0.06% 5.2.2 Post Shrinkage . After 48 h at 120 C 0.00% 5.3 RECYCLING CODE UP- (GF+M) 70 ENGINEERING MATERIAL SPECIFICATIONWSB-M3D173-A2Printed copies are uncontrolled Copyright 2004, Ford Global Technologies, LLC Page 5 of 5

展开阅读全文
相关资源
猜你喜欢
  • CSN EN 2070-6-1994 Aerospace series Aluminium and aluminium alloy wrought products Technical specification Part 6 Rivet wire《航空航天系列 铝及铝合金锻造制品 技术规范 第6部分:铆钉线》.pdf CSN EN 2070-6-1994 Aerospace series Aluminium and aluminium alloy wrought products Technical specification Part 6 Rivet wire《航空航天系列 铝及铝合金锻造制品 技术规范 第6部分:铆钉线》.pdf
  • CSN EN 20811-1994 Textiles Determination of resistance to water penetration - Hydrostatic pressure test《纺织品 耐水渗性测定 水压试验》.pdf CSN EN 20811-1994 Textiles Determination of resistance to water penetration - Hydrostatic pressure test《纺织品 耐水渗性测定 水压试验》.pdf
  • CSN EN 2100-1995 Aerospace series Aluminium alloy AL-P2014A-T4511 Extruded bars and sections  a  or  D  = 200 mm《航空航天系列 铝合金AL-P2014A-T4511  a 或 D ≤ 200毫米的挤压棒及型材》.pdf CSN EN 2100-1995 Aerospace series Aluminium alloy AL-P2014A-T4511 Extruded bars and sections a or D = 200 mm《航空航天系列 铝合金AL-P2014A-T4511 a 或 D ≤ 200毫米的挤压棒及型材》.pdf
  • CSN EN 2126-1995 Aerospace series Aluminium alloy AL-P7075-T651 Plates 6 mm   a  = 80 mm《航空航天系列 铝合金AL-P7075-T651 6毫米  a ≤ 80 毫米板材》.pdf CSN EN 2126-1995 Aerospace series Aluminium alloy AL-P7075-T651 Plates 6 mm a = 80 mm《航空航天系列 铝合金AL-P7075-T651 6毫米 a ≤ 80 毫米板材》.pdf
  • CSN EN 2127-1995 Aerospace series Aluminium alloy AL-P7075-T73511 Extruded bars and section《航空航天系列  铝合金AL-P7075-T73511a 或 D ≤ 100毫米的挤压棒和型材》.pdf CSN EN 2127-1995 Aerospace series Aluminium alloy AL-P7075-T73511 Extruded bars and section《航空航天系列 铝合金AL-P7075-T73511a 或 D ≤ 100毫米的挤压棒和型材》.pdf
  • CSN EN 2128-1995 Aerospace series Aluminium alloy AL-P7075-T7351 Drawn bars 6 mm =  a  or  D  = 75 mm《航空航天系列 铝合金AL-P7075-T7351 6毫米 ≤ a 或 D ≤ 75毫米的拔钢棒》.pdf CSN EN 2128-1995 Aerospace series Aluminium alloy AL-P7075-T7351 Drawn bars 6 mm = a or D = 75 mm《航空航天系列 铝合金AL-P7075-T7351 6毫米 ≤ a 或 D ≤ 75毫米的拔钢棒》.pdf
  • CSN EN 225-1993 Atomizing oil burners Pumps with rotating shaft and external drive Dimensions《雾化油燃烧器 带转轴及外驱动器泵 尺寸》.pdf CSN EN 225-1993 Atomizing oil burners Pumps with rotating shaft and external drive Dimensions《雾化油燃烧器 带转轴及外驱动器泵 尺寸》.pdf
  • CSN EN 22568-1993 Hand- and machine- operated circular screwing dies and hand- operated die stocks (ISO 2568 1988)《手工和机械操作圆板牙及手动板牙扳手(ISO 2568-1988)》.pdf CSN EN 22568-1993 Hand- and machine- operated circular screwing dies and hand- operated die stocks (ISO 2568 1988)《手工和机械操作圆板牙及手动板牙扳手(ISO 2568-1988)》.pdf
  • CSN EN 226-1993 Atomizing oil burners Connecting dimensions between burners and heat generators《雾化油燃烧器 燃烧器和热发生器之间的连接尺寸》.pdf CSN EN 226-1993 Atomizing oil burners Connecting dimensions between burners and heat generators《雾化油燃烧器 燃烧器和热发生器之间的连接尺寸》.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