SAE AS5392
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Health and Usage Monitoring System, Rotational System Indexing Sensor Specification
Hardcopy , PDF
08-04-2020
English
12-12-2002
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1 Scope
1.1 Classification
1.2 Specification terminology
2 References
3 Definitions
4 Requirements and recommendations
4.1 Self-powered sensor interface
4.2 Externally powered sensor interface
5 Notes
5.1 Comments to sensor subsystem designer
5.2 Principles of operation - different sensor technologies
Figures
Specifies requirements for the interface between a rotational system indexing sensor and its interface electronics.
| DocumentType |
Standard
|
| Pages |
11
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
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.
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| SAE AS5393 | Health and Usage Monitoring System, Blade Tracker Interface Specification |
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