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现行 SAE AS7510B
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Coupling Assembly, Threadless, Flexible, Self-Locking, Fixed Cavity, High Conductivity, Self-Bonding, Part Specification 连接器组件 无螺纹 柔性 自锁 固定腔 高导电性 自粘合 零件规范
发布日期: 2023-12-18
本SAE航空航天标准(AS)定义了无螺纹、柔性、高导电、自结合联轴器组件的要求,当安装在规定的套圈上时,该组件为连接加压流体系统中的管道和部件提供了柔性连接。组装联轴器的设计目的是在合格制造商之间提供零件和部件的互换性,以便在额定工作压力为130 psi、温度为-65至+265°F的条件下使用,并延长飞机系统的使用寿命。FAR23.954、FAR25.603、FAR25.605、FAR25.609、FAR256613、FAR 25.901、FAR25954和FAR25.981认证要求已经确定了对具有高电流能力的柔性流体组装联轴器的需求。联接器组件不需要检查或维护以在飞机的使用寿命内保持电流能力。本规范提供了低- 压力联轴器:组装联轴器的电磁效应/雷电测试,以证明雷电传导电流和静电能力,通过模拟使用寿命测试序列来保持,以满足商用飞机FAR 25.981认证要求。基于尺寸和材料相似性对耦合试样进行分组和目标张贴。组装联轴器的预期应用和用途包括但不限于商用和军用飞机。此处定义并符合性能和法规合规要求的部件将支持其在燃料和其他流体输送系统中的使用。本规范要求制造商符合性能审查机构(PRI)/Nadcap的要求。
This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive, self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system.FAR 23.954, FAR 25.603, FAR 25.605, FAR 25.609, FAR 25.613, FAR 25.901, FAR 25.954, and FAR 25.981 certification requirements have identified the need for high-current capable flexible fluid assembled couplings. The coupling assembly does not require inspection or maintenance to remain current capable for the life of the aircraft.This specification provides two test philosophies necessary for low-pressure couplings:Electromagnetic effects/lightning testing of assembled couplings to demonstrate both lightning conducted current and electrostatic capabilities are retained through simulated service life test sequences to meet commercial airplane FAR 25.981 certification requirements.Grouping and goal posting of coupling test specimens based on size and material similarities.The assembled coupling’s intended application and usage is for, but not limited to, commercial and military aircraft. Components defined herein and qualified to the performance capabilities and regulatory compliance requirements will support their use in fuel and other fluid conveyance systems.This specification requires manufacturers to be qualified and accredited to Performance Review Institute (PRI)/Nadcap requirements.
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