Health and Usage Monitoring System Accelerometer Interface Specification
|
Product Code: AS5391
Date Published: 2002-12-12
Issuing Committee:
E-32 Aerospace Propulsion Systems Health Management
Scope
Accelerometers are transducers, or sensors, that convert acceleration into an electrical signal which can be used for vibration monitoring and analysis.
This document defines interface requirements for accelerometers and associated interfacing electronics for use in a helicopter Health and Usage Monitoring System (HUMS). The purpose is to standardize the accelerometer-to-electronics interface with the intent of increasing interchangeability among HUMS sensors/systems and reducing the cost of HUMS accelerometers. Although this interface was specified with an internally amplified piezoelectric accelerometer in mind, this does not preclude the use of any other sensor technology that meets the requirements given in this specification.
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.
Product Status: In Stock
File Size:
482K
Purchase more aerospace standards and aerospace material specifications and save!
AeroPaks offers a customized subscription plan that lets you pay
for just the documents that you need, when you need them.
Learn more >
| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| AS5391 |
2002-12-12 |
Issued |
|
Related Content
Collections
Papers
Books
Standards
|
