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SAE AS 5392:2002-12-12

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SAE AS 5392:2002-12-12

Health and Usage Monitoring System, Rotational System Indexing Sensor Specification

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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.
Author SAE
Editor SAE
Document type Standard
Format File
Number of pages 11
Set AEROPAKS10U-10
Year 2002
Country USA
Keyword SAE 5392;SAE AS5392;SAE AS5392;SAE AS 5392