標(biāo)準(zhǔn)號：SAE MA 3377B-2008
中文標(biāo)準(zhǔn)名稱：拉伸強(qiáng)度為1275MPa的米制UNS NO7718鎳合金螺栓和螺釘?shù)牟少徱?guī)范
英文標(biāo)準(zhǔn)名稱：Bolts and Screws, Nickel Alloy UNS NO7718, Tensile Strength 1275 MPa Procurement Specification, Metric
標(biāo)準(zhǔn)類型：V20
發(fā)布日期：2008/11/5 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國標(biāo)準(zhǔn)分類號：V20
國際標(biāo)準(zhǔn)分類號：49.030.20
引用標(biāo)準(zhǔn)：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-
適用范圍：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.