Your shopping cart is empty!
SAE International, 03/02/2022
Publisher: SAE
File Format: PDF
$57.00$114.00
Published:02/03/2022
File Size:1 file , 360 KB
Note:This product is unavailable in Ukraine, Russia, Belarus
Accelerometers are transducers, or sensors, that convert acceleration into an electrical signal that can be used for airframe, drive, and propulsion system vibration monitoring and analysis within vehicle health and usage monitoring systems.
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 for Airframe and Drive Train accelerometers, this does not preclude the use of piezoelectric accelerometer with remote charge amplifier or any other sensor technology that meets the requirements given in this specification.
This SAE HUMS Accelerometer Interface Specification includes the minimal interface and performance requirements for commonality. Compliance with this Interface Specifications can be referenced in more comprehensive procurement and device specifications.
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, DOUBLE, SERIES I
$24.00 $48.00
Test Procedures for Non-SAE Hydraulic Hoses (Stabilized: Apr 2021)
$30.00 $60.00
Fittings, 37 Degree Internal Flare, Fluid Connection, Procurement Specification
$55.00 $110.00
Gland Design Criteria and Dimensions for Dynamic Radial O-Ring Seal Applications Specifically for Engine and Engine Control Systems Operating at 1500 psi Max