SAE MA 3377B-2008
拉伸强度为1275MPa的米制UNS NO7718镍合金螺栓和螺钉的采购规范

Bolts and Screws, Nickel Alloy UNS NO7718, Tensile Strength 1275 MPa Procurement Specification, Metric


SAE MA 3377B-2008 发布历史

This document covers metric bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718. The following specification designations and their properties are covered: MA3377 1275 MPa minimum ultimate tensile strength at room temperature; 1000 MPa minimum ultimate tensile strength at 650 °C; 690 MPa stress-rupture strength at 650 °C; 720 MPa tension to 72 MPa tension fatigue at room temperature and MA3377-1 1275 MPa minimum ultimate tensile strength at room temperature; 765 MPa minimum ultimate shear strength at room temperature; 720 MPa tension to 72 MPa tension fatigue at room temperature. Primarily for use in aerospace propulsion systems as follows: a. for use up to approximately 650 °C where elevated temperature tensile strength, stress-rupture strength, and resistance to relaxation are required; and b. for use up to approximately 425 °C where fatigue resistance, tensile strength, and shear strength are required.

SAE MA 3377B-2008由美国机动车工程师协会 US-SAE 发布于 2008-11-05。

SAE MA 3377B-2008 在中国标准分类中归属于: V20 紧固件,在国际标准分类中归属于: 49.030.20 螺栓、螺钉、螺柱。

SAE MA 3377B-2008 发布之时,引用了标准

* 在 SAE MA 3377B-2008 发布之后有更新,请注意新发布标准的变化。

SAE MA 3377B-2008的历代版本如下:

  • 2008年11月05日 SAE MA 3377B-2008 拉伸强度为1275MPa的米制UNS NO7718镍合金螺栓和螺钉的采购规范

SAE MA 3377B-2008 拉伸强度为1275MPa的米制UNS NO7718镍合金螺栓和螺钉的采购规范 由 SAE MA 3377A-1995 变更而来。

 

 

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标准号
SAE MA 3377B-2008
发布日期
2008年11月05日
实施日期
废止日期
中国标准分类号
V20
国际标准分类号
49.030.20
发布单位
US-SAE
引用标准
ASME B46.1-2002 ASTM D 3951-1998 ASTM E 8M-2004 ASTM E 21-2005 ASTM E 112-1996 ASTM E 139-2006 ASTM E 140-2007 ASTM E 1417-2005 SAE AMS 2700-2000 SAE AMS 2750D-2005 SAE AMS 5662 SAE AS 3062C-1979 SAE AS 3063B-1996 SAE MA 1370-1990 SAE MA 1518 SAE MA 1520-
被代替标准
SAE MA 3377A-1995
适用范围
This document covers metric bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718. The following specification designations and their properties are covered: MA3377 1275 MPa minimum ultimate tensile strength at room temperature; 1000 MPa minimum ultimate tensile strength at 650 °C; 690 MPa stress-rupture strength at 650 °C; 720 MPa tension to 72 MPa tension fatigue at room temperature and MA3377-1 1275 MPa minimum ultimate tensile strength at room temperature; 765 MPa minimum ultimate shear strength at room temperature; 720 MPa tension to 72 MPa tension fatigue at room temperature. Primarily for use in aerospace propulsion systems as follows: a. for use up to approximately 650 °C where elevated temperature tensile strength, stress-rupture strength, and resistance to relaxation are required; and b. for use up to approximately 425 °C where fatigue resistance, tensile strength, and shear strength are required.




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