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Aircraft Brake Temperature Monitoring 飞机刹车温度监测
发布日期: 2021-10-28
本SAE航空航天推荐规程(ARP)为机载制动温度监测系统(BTMS)的功能、设计、构造和测试提供了建议,有时也称为制动温度指示系统(BTIS)。 注意:此ARP不寻址: 驾驶舱人体工程学和飞机操作程序。 温度感测或读数的各种手持方法,因为这些方法在正常操作期间与运输机无关。 温度敏感涂料,作为指示由于制动器温度超过起落架轴温阈值的手段。
This SAE Aerospace Recommended Practice (ARP) provides recommendations for the function, design, construction, and testing of an on-aircraft Brake Temperature Monitoring System (BTMS), sometimes referred to as a Brake Temperature Indication System (BTIS). NOTE: This ARP does not address: Cockpit ergonomics and Aircraft operating procedures. Various handheld methods of temperature sensing or readouts, as these are not associated with transport aircraft during normal operation. Temperature sensitive paints as a means to indicate exceedance of a landing gear axle temperature threshold due to brake temperature.
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归口单位: AEROC
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