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 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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