FORD WSD-M2A137-B3-2003 ALUMINUM SILICON COPPER MAGNESIUM ALLOYS TO BE USED WITH FORD WSS-M99P1111-A (Shown on WSD-M2A137-B1)《铝、硅铜合金镁合金 与标准FORD WSS-M99P1111-A一起使用 列于标准WSD-M2A13.pdf

上传人:eastlab115 文档编号:749798 上传时间:2019-01-14 格式:PDF 页数:2 大小:60.58KB
下载 相关 举报
FORD WSD-M2A137-B3-2003 ALUMINUM SILICON COPPER MAGNESIUM ALLOYS  TO BE USED WITH FORD WSS-M99P1111-A  (Shown on WSD-M2A137-B1)《铝、硅铜合金镁合金  与标准FORD WSS-M99P1111-A一起使用  列于标准WSD-M2A13.pdf_第1页
第1页 / 共2页
FORD WSD-M2A137-B3-2003 ALUMINUM SILICON COPPER MAGNESIUM ALLOYS  TO BE USED WITH FORD WSS-M99P1111-A  (Shown on WSD-M2A137-B1)《铝、硅铜合金镁合金  与标准FORD WSS-M99P1111-A一起使用  列于标准WSD-M2A13.pdf_第2页
第2页 / 共2页
亲,该文档总共2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 2003 09 12 Revised Para 3.0 inserted; para 3.1, 3.7 and 4 deleted 1993 09 29 C10338491 Released R. Cooper, EAO; P. Lee, NAAO Printed copies are uncontrolled Copyright 2003, Ford Global Technologies, Inc. Page 1 of 2 ALUMINUM, SILICON COPPER MA

2、GNESIUM ALLOYS WSD-M2A137-B1 WSD-M2A137-B2 WSD-M2A137-B3 WSD-M2A137-B4 WSD-M2A137-B5 1. SCOPE The materials defined by these specifications are a series of high silicon aluminum alloys suitable for gravity die casting, which contain copper, nickel and magnesium to enhance elevated temperature proper

3、ties. 2. APPLICATION These specifications were released originally for materials used for automotive pistons. Mechanical properties at elevated temperature and wear resistance increase through the grades to B4 and B5, which are recommended for the most arduous applications. 3. REQUIREMENTS 3.0 STAND

4、ARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.2 CHEMICAL COMPOSITION (Weight %) B1 B2 B3 B4 B5 Silicon 8.5-10.5 11-13 11-13 14.8-18.0 17-19 Copper 2.0-4.0 0.7-1.5 0.7-1.5

5、 1.9-3.6 0.8-1.5 Iron 0.8 max 0.8 max 0.8 max 0.85 max* 0.8 max Magnesium 0.5-1.5 0.8-1.5 0.8-1.5 0.5-1.0 0.8-1.3 Nickel 1.0 max 0.7-1.3 0.7-1.3 0.35-0.8 1.3 max Manganese* 0.5 max 0.5 max 0.5 max 0.45 max 0.2 max Zinc 1.0 max 0.5 max 0.5 max 0.90 max 0.2 max Titanium 0.25 max 0.25 max 0.25 max 0.20

6、 max 0.25 maxChromium - - - 0.10 - Others each 0.1 max 0.1 max 0.1 max 0.1 max 0.1 max Total others 0.5 max 0.5 max 0.5 max 0.5 max 0.5 maxSodium/ 0.5 max 0.5 max 0.5 max 0.5 max 0.5 max Strontium (Total) Phosphorus * * * * * Aluminum Balance Balance Balance Balance Balance * High performance piston

7、s may require lower iron; iron content must be balanced by Mn content, 2:1 respectively. * Manganese content shall not be less than one-half the iron content. * Primary silicon refinement 0.0025 - 0.005% typical ENGINEERING MATERIAL SPECIFICATIONWSD-M2A137-B1/B5Printed copies are uncontrolled Copyri

8、ght 2003, Ford Global Technologies, Inc. Page 2 of 2 Supplied composition shall fall within the above ranges, and limits will be defined as part of the control plan. The control plan will also include modification, refining elements and processing detail. 3.3 MECHANICAL PROPERTIES (Cast Test Bars) R

9、oom Temperature 3.3.1 Tensile Strength, min B1 & B5 180 MPa (ASTM E 8/ E 8M) B2, B3, & B4 200 MPa Note: Cast test bars shall be processed and coded in a manner comparable to the casting they represent. 3.3.2 Hardness (500 Kg load, 10 mm ball) 90 - 130 HB (ASTM E 10) 3.4 MECHANICAL PROPERTIES (Finish

10、ed Components) Room Temperature 3.4.1 Tensile Strength, min 180 MPa Test bars machined from any location. The engineering drawing may designate a higher value for test bars from specified locations. 3.4.2 Hardness 90 - 130 HB (ASTM E 10) Rockwell F or Rockwell B measurements may be used on the finis

11、hed component in lieu of Brinell readings where section thickness precludes using Brinell impressions. Hardness measurement locations shall be specified on the Engineering Drawing. 3.5 MICROSTRUCTURE (ASTM E 3) B1 and B2: Aluminum rich dendrites in an aluminum silicon eutectic matrix, containing uni

12、formly distributed intermetallic compounds. B3, B4 and B5: Primary silicon crystallites in a acicular aluminum silicon matrix, containing uniformly distributed intermetallic compounds. Silicon particles must be randomly distributed and generally 10 to 50 micrometres in diameter, with no dimension to

13、 exceed 100 micrometres. High performance pistons may require finer silicon particle size. Surface depletion of primary silicon crystals should be kept to a minimum. 3.6 HEAT TREATMENT (T5 or T6) Cool from an elevated temperature casting process or solution heat treatment and then artificially age t

14、o improve mechanical properties or dimensional stability or both. Age for minimum 4 hours, typically 8 - 12 hours at temperatures selected between 195 - 240 C. Maintain selected ageing temperature to +/- 5 C. Specific heating/cooling and ageing practice or any deviation to the above shall form part of the component control plan.

展开阅读全文
相关资源
猜你喜欢
  • DIN EN 2591-7301-2003 Aeospace series - Elements of electrical and optical connection Test methods - Part 7301 Electrical elements Temperature endurance of couplers German and Engl.pdf DIN EN 2591-7301-2003 Aeospace series - Elements of electrical and optical connection Test methods - Part 7301 Electrical elements Temperature endurance of couplers German and Engl.pdf
  • DIN EN 2592-1991 Aerospace series three-pole circuit breakers temperature compensated rated currents up to 25 A product standard german version EN 2592 1990《航空航天 温度补偿的额定电流25A以下三极断路.pdf DIN EN 2592-1991 Aerospace series three-pole circuit breakers temperature compensated rated currents up to 25 A product standard german version EN 2592 1990《航空航天 温度补偿的额定电流25A以下三极断路.pdf
  • DIN EN 2593-001-2015 Aerospace series - Bases for 10 A electromagnetic plug-in relays two and four poles double thrown - Part 001 Technical specification German and English version.pdf DIN EN 2593-001-2015 Aerospace series - Bases for 10 A electromagnetic plug-in relays two and four poles double thrown - Part 001 Technical specification German and English version.pdf
  • DIN EN 2596-2007 Aerospace series - Washers lock with radial serrations in corrosion resisting steel cadmium plated for flight control rods - Dimensions German and English version .pdf DIN EN 2596-2007 Aerospace series - Washers lock with radial serrations in corrosion resisting steel cadmium plated for flight control rods - Dimensions German and English version .pdf
  • DIN EN 2597-1998 Aerospace series - Carbon fibre reinforced plastics unidirectional laminates - Tensile test perpendicular to the fibre direction German version EN 2597 1998《航空航天系列.pdf DIN EN 2597-1998 Aerospace series - Carbon fibre reinforced plastics unidirectional laminates - Tensile test perpendicular to the fibre direction German version EN 2597 1998《航空航天系列.pdf
  • DIN EN 2599-2002 Aerospace series - Strips in aluminium and aluminium alloys - Thickness 0 25 mm a 3 2 mm Dimensions German version EN 2599 2001《航空航天系列 铝和铝合金带材 厚度a为0 25mm-3 2mm 尺寸》.pdf DIN EN 2599-2002 Aerospace series - Strips in aluminium and aluminium alloys - Thickness 0 25 mm a 3 2 mm Dimensions German version EN 2599 2001《航空航天系列 铝和铝合金带材 厚度a为0 25mm-3 2mm 尺寸》.pdf
  • DIN EN 26-2015 Gas-fired instantaneous water heaters for the production of domestic hot water German version EN 26 2015《生成家用热水的燃气瞬时热水器 德文版本EN 26-2015》.pdf DIN EN 26-2015 Gas-fired instantaneous water heaters for the production of domestic hot water German version EN 26 2015《生成家用热水的燃气瞬时热水器 德文版本EN 26-2015》.pdf
  • DIN EN 2601-1996 Aerospace series - Fork ends adjustable - Technical specification German version EN 2601 1996《航空航天系列 可调叉头 交货技术条件》.pdf DIN EN 2601-1996 Aerospace series - Fork ends adjustable - Technical specification German version EN 2601 1996《航空航天系列 可调叉头 交货技术条件》.pdf
  • DIN EN 2602-2007 Aerospace series - Ports for adaptors threaded with lockring - Geometric configuration German and English version EN 2602 2005《航空航天系列 带锁环的螺纹适配器用端口 几何形状》.pdf DIN EN 2602-2007 Aerospace series - Ports for adaptors threaded with lockring - Geometric configuration German and English version EN 2602 2005《航空航天系列 带锁环的螺纹适配器用端口 几何形状》.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