SAE AS 1710D-2009
带套圈的螺纹型可变空腔柔性燃料耦合件

Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules


SAE AS 1710D-2009 发布历史

This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.

SAE AS 1710D-2009由美国机动车工程师协会 US-SAE 发布于 2009-02-19。

SAE AS 1710D-2009 在中国标准分类中归属于: V21 管件、卡箍、密封件,在国际标准分类中归属于: 49.050 航空航天发动机和推进系统。

SAE AS 1710D-2009 发布之时,引用了标准

SAE AS 1710D-2009的历代版本如下:

  • 2009年02月19日 SAE AS 1710D-2009 带套圈的螺纹型可变空腔柔性燃料耦合件

SAE AS 1710D-2009 带套圈的螺纹型可变空腔柔性燃料耦合件 由 SAE AS 1710C-2006 变更而来。

 

 

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标准号
SAE AS 1710D-2009
发布日期
2009年02月19日
实施日期
废止日期
中国标准分类号
V21
国际标准分类号
49.050
发布单位
US-SAE
引用标准
ANSI/ASQC Z 1.4-1993 ASME B1.1-2003 ASTM D 473-2007 ASTM D 5118/D 5118M-2005 ASTM D 5486/D 5486M-2006 ASTM D 6251/D 6251M-2007 PD 2001 PD 2101 MIL-STD-810-2008 SAE AMS-R-25988-1998 SAE AMS-WW-T-700/6 SAE ARP 9013-2005 SAE AS 567J-1994 SAE AS 568C-2008 SAE
被代替标准
SAE AS 1710C-2006
适用范围
This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.




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