本SAE航空航天标准（AS）规定了旋转系统分度传感器与其接口电子设备之间的接口要求。这些传感器为被监测轴的每转产生一个或多个电脉冲。这些脉冲可用于确定健康和使用情况监测系统（HUMS）中使用的实际轴转速和/或位置。分度传感器用于飞机上的以下HUMS区域:（a）转子轨道和平衡，（b）发动机振动监测和诊断，（c）传动系振动监测和诊断。这项标准化工作的目标是能够获取任何兼容的索引传感器，并将其连接到任何兼容的接口电子设备。这些SAE HUMS接口规范包括与符合旋翼机工业技术协会（RITA）的HUMS互操作性的最低接口和性能要求。 在更全面的采购和设备规范中，可以参考这些接口规范的合规性。

This SAE Aerospace Standard (AS) specifies requirements for the interface between a rotational system indexing sensor and its interface electronics. These sensors generate one or more electrical pulses for each revolution of the shaft being monitored. These pulses can be used to determine the actual shaft rotational speed and/or position for use in a Health and Usage Monitoring System (HUMS). Indexing sensors are used in the following HUMS areas on the aircraft: (a) rotor track and balance, (b) engine vibration monitoring and diagnostics, (c) drive train vibration monitoring and diagnostics. The goal of this standardization effort is to be able to take any compliant indexing sensor and connect it to any compliant interface electronics.These SAE HUMS Interface Specifications include the minimal interface and performance requirements for interoperability with the Rotorcraft Industry Technology Association (RITA) compliant HUMS. Compliance with these Interface Specifications can be referenced in more comprehensive procurement and device specifications.