FORD WH901-1993 GENERAL REQUIREMENTS AND PHYSICAL PROPERTIES FOR SPRING PINS - COILED《盘绕弹簧销的一般要求和物理性能》.pdf

上传人:fatcommittee260 文档编号:748557 上传时间:2019-01-14 格式:PDF 页数:2 大小:27.27KB
下载 相关 举报
FORD WH901-1993 GENERAL REQUIREMENTS AND PHYSICAL PROPERTIES FOR SPRING PINS - COILED《盘绕弹簧销的一般要求和物理性能》.pdf_第1页
第1页 / 共2页
FORD WH901-1993 GENERAL REQUIREMENTS AND PHYSICAL PROPERTIES FOR SPRING PINS - COILED《盘绕弹簧销的一般要求和物理性能》.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、FORD WORLDWIDE FASTENER STANDARDDate: 1993-01-01Engineering Standards & 1 of 2 Printed copies are uncontrolled .Systems Engineering (ESSE)WH 901General Requirements and Physical Properties for Spring Pins - Coiled1. SCOPE. This standard specifies the material, heat treatment, gauging and physical pr

2、operties for metriccoiled spring pins intended for general use.1.1 REFERENCES.ISO 6507: 1982 - Metallic materials - Hardness test- Vickers test.ISO 6508 - Metallic materials - Hardness test - Rockwell test.WSD-M1A283-B50/B51/B52 - Steel, cross reference for standard parts.2. GENERAL REQUIREMENTS.2.1

3、 DIAMETER. The pin diameters shall be inspected using the Go/No Go ring gauges shown inTable 1.Table 1.Dimensions in mmPin Size 2 3 4 5 6 8 10Go 2.25 3.3 4.4 5.5 6.5 8.63 10.8Gage 2.24 3.29 4.39 5.49 6.49 8.62 10.79No Go 2.14 3.16 4.21 5.21 6.26 8.31 10.36Gauge 2.13 3.15 4.2 5.2 6.25 8.30 10.352.2 S

4、TRAIGHTNESS. The straightness of the pins shall be within the limits necessary to permit thepins to fall through a ring gauge by their own weight. Ring gauge dimensions are shown in Table2.Table 2.Dimensions in mmPin Length GaugeLengthGauge HoleDiameter *+/- 0.15 Max. Min.To & including 24 25 0.2 0.

5、18Over 24 to 50 50 0.34 0.3Over 50 75 0.48 0.42* Gauge hole diameter = Max pin diameter plus indicated values3. MATERIAL AND HEAT TREATMENT.3.1 MATE RIAL. Steel - WSD-M1A283-B50/51/52.3.2 HEAT TREATMENT. The pins are to be through hardened and tempered to HV 420-545(HR 15N82-86.4) or austempered to

6、HV 500-580 (HR 15N85-87.5).4. PHYSICAL PROPERTIES.4.1 HARDNESS TESTING. The hardness testing shall be performed in accordance with the followingprocedures:Vickers Hardness to ISO 6507:1982 10kg load.Rockwell Hardness to ISO 6508.NOTE: In case of dispute the Vickers Hardness test is decisive for acce

7、ptance.FORD WORLDWIDE FASTENER STANDARDDate: 1993-01-01Engineering Standards & 2 of 2 Printed copies are uncontrolled .Systems Engineering (ESSE)WH 901General Requirements and Physical Properties for Spring Pins - Coiled4.2 PERFORMANCE. Pins shall be capable of withstanding the double shear loads sp

8、ecified in Table3. The shear test shall be performed in a fixture in which the pin support member and the memberfor applying the load shall have holes with diameters as recommended for the pins and shall have ahardness of HV 700 minimum. The clearance between the supporting members and the loadmembe

9、r shall not exceed 0.15mm and the shear plane shall be at least one pin diameter away fromeach end and at least two diameters apart. Pins too short to be tested in double shear shall be testedby shearing two pins simultaneously in single shear. Speed of testing shall not exceed13mm/minute. Pins shal

10、l be tested to failure. The maximum load applied to the pin coincidentwith or prior to pin failure shall be recorded as the double shear strength of the pin. Pins tested forshear strength shall shown a ductile shear without longitudinal cracks.Table 3.Dimensions in mmNominal Pin Size 2 3 4 5 6 8 10M

11、in. Double Shear Strength -kN2.5 5.5 9.6 15 22 39 625. DEFECTS. Pins shall be free from burrs, loose scale, seams, notches, sharp edges and corners and anyother defects affecting serviceability.6. RECOMMENDED APPLICATION HOLE SIZES. See Table 4.Table 4.Dimensions in mmNominal Pin Size 2 3 4 5 6 8 10Hole Dia. max. 2.1 3.1 4.12 5.12 6.12 8.15 10.15min. 2 3 4 5 6 8 10

展开阅读全文
相关资源
猜你喜欢
  • EN 2535-2011 en Aerospace series - Vacuum deposition of cadmium《航空航天系列 镉的真空沉积》.pdf EN 2535-2011 en Aerospace series - Vacuum deposition of cadmium《航空航天系列 镉的真空沉积》.pdf
  • EN 2536-1995 en Aerospace Series - Hard Anodizing of Aluminium Alloys《航空航天系列 铝合金的硬阳极氧化》.pdf EN 2536-1995 en Aerospace Series - Hard Anodizing of Aluminium Alloys《航空航天系列 铝合金的硬阳极氧化》.pdf
  • EN 2542-2008 en Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - De Less Than or Equal to 40 mm - For prevailing torque nuts《航空航天系列 钢FE-PL1502(25CrMo4) 退火的棒.pdf EN 2542-2008 en Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - De Less Than or Equal to 40 mm - For prevailing torque nuts《航空航天系列 钢FE-PL1502(25CrMo4) 退火的棒.pdf
  • EN 2543-2009 en Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Sheet and strip 0 3 mm less than or equal to a less than or equal to 2 mm - For prevailing torque nuts《航空航.pdf EN 2543-2009 en Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Sheet and strip 0 3 mm less than or equal to a less than or equal to 2 mm - For prevailing torque nuts《航空航.pdf
  • EN 2544-1987 en Representation of Rivets on Drawings for Aerospace Equipment《航空航天系列 航空航天设备图纸上铆钉的画法》.pdf EN 2544-1987 en Representation of Rivets on Drawings for Aerospace Equipment《航空航天系列 航空航天设备图纸上铆钉的画法》.pdf
  • EN 2545-1-1995 en Aerospace Series - Titanium and Titanium Alloy Remelting Stock and Castings - Technical Specification - Part 1 General Requirements《航空航天系列 钛和钛合金重熔毛坯和铸件 技术规范 第1部分 .pdf EN 2545-1-1995 en Aerospace Series - Titanium and Titanium Alloy Remelting Stock and Castings - Technical Specification - Part 1 General Requirements《航空航天系列 钛和钛合金重熔毛坯和铸件 技术规范 第1部分 .pdf
  • EN 2545-2-1995 en Aerospace Series - Titanium and Titanium Alloy Remelting Stock and Castings - Technical Specification - Part 2 Remelting Stock《航空航天系列 钛和钛合金重熔毛坯和铸件 技术规范 第2部分 重熔》.pdf EN 2545-2-1995 en Aerospace Series - Titanium and Titanium Alloy Remelting Stock and Castings - Technical Specification - Part 2 Remelting Stock《航空航天系列 钛和钛合金重熔毛坯和铸件 技术规范 第2部分 重熔》.pdf
  • EN 2545-3-1995 en Aerospace Series - Titanium and Titanium Alloy Remelting Stock and Castings - Technical Specification - Part 3 Pre-Production and Production Castings《航空航天系列 钛和钛合金.pdf EN 2545-3-1995 en Aerospace Series - Titanium and Titanium Alloy Remelting Stock and Castings - Technical Specification - Part 3 Pre-Production and Production Castings《航空航天系列 钛和钛合金.pdf
  • EN 2546-2006 en Aerospace series - Washers lock with radial serrations in corrosion resisting steel passivated for flight control rods - Dimensions《航空航天系列 飞行操纵杆用钝化耐蚀钢制的径向锯齿锁紧垫圈 尺寸》.pdf EN 2546-2006 en Aerospace series - Washers lock with radial serrations in corrosion resisting steel passivated for flight control rods - Dimensions《航空航天系列 飞行操纵杆用钝化耐蚀钢制的径向锯齿锁紧垫圈 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