A/E37T-32 Dynamic Vibration Analyzer Track Balance Test VATS Instruments AE37T

Description

A/E37T-32 Dynamic Vibration Analyzer Track Balance Test VATS Instruments AE37T
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Dynamic Instruments A/E 37T-32 digital vibration analysis - track and balance Test Set. A/E3T-32
This auction is for the Computer Indicator case which includes the control panel, display, keyboard, and connector panel. It would make a great Extra/replacement unit.
T
he A/E 37T-32 Vibration Analysis Test Set (VATS)
.
The VATS is a multi-function instrumentation system used for vibration analysis, propeller balancing, and helicopter rotor tracking and balancing. The VATS is also used for fault isolation in aircraft drive systems, flight controls, and airframe components, supporting both rotary and fixed wing aircraft.
SYSTEM DESCRIPTION
1. Operational Uses. The A/E 37T-32 VATS is used on Navy and Marine Corps aircraft by organizational and depot maintenance personnel to track and balance rotors, propellers, and turbofans, and to monitor the vibration of aircraft and aircraft dynamic components under field conditions. The VATS is capable of measuring the vibration frequency and magnitude for engines, transmissions, gear boxes, dynamic drive systems, and airframes. The VATS is used to fault isolate vibration discrepancies and monitor the health of dynamic components and the airframe through vibration trend analysis tracking.
Vibration Analysis (VA) is a means of determining mechanical system faults such as imbalance, misalignment, mechanical looseness, gear tooth defects, bearing defects, and structural and component resonance. The VATS is used as a VA failure isolation and prediction tool. This results in increased readiness due to a reduced vibration discrepancy maintenance workload.
VA tasks which the VATS is intended to accomplish are:
H-53 main and tail rotor track and balance, transmission, gearbox, drive shafts, and airframe monitoring
H-3 main and tail rotor track and balance, transmission, gearbox, drive system, and airframe monitoring
H-60 main and tail rotor track and balance, transmission, gearbox, drive system, airframe monitoring, and vibration absorber tuning
H-1 main and tail rotor track and balance, transmission, gearbox, drive system, airframe monitoring, and vibration absorber tuning
E-2 and C-2 on-aircraft propeller balancing and airframe monitoring
S
-3 fan rotor assembly balancing
Other aircraft utilize several different types of equipment for Vibration Analysis and are not mentioned
here
for that reason.
Foreign Military Sales. Not Applicable (NA)
Description:
Functional Description
. The VATS is used on Navy aircraft by organizational and depot level maintenance and flight crew personnel. It is capable of being placed in the aircraft for in-flight troubleshooting and VA without degrading aircraft operation. The VATS is comprised of the following six subsystems, in three portable instrument cases.
Fast Fourier Transformer Analyzer.
The Fast Fourier Transformer Analyzer is used to record real-time frequency analysis of the input signal.
Magnetic Media Input-Output Module
. The Magnetic Media Input-Output Module is used to record digital information data appearing on the visual display or machine.
Sensors
. The Sensors consist of the optical tachometer and the accelerometers. A line-scan camera provides data to the optical tachometer and the analyzer.
Flat Panel Display.
The Flat Panel Display is an operator visual display unit with
a
lphanumeric and graphic capabilities.
Machine Transcribed Record (Hard Copy)
. This is a device capable of producing hard copy records of both the alphanumeric and graphic data that appear on the Flat Panel Display.
Integrated Operator Interface
. The Integrated Operator Interface enables the operator to select tests or functions, enter data, and communicate with the test unit.
Physical Description
. The dimensions of the three portable instrument cases containing VATS are 15.5" x 18.5" x 11.5", weighing between 35 and 43 pounds.
Instrument case one contains the Computer Indicator Power Supply which includes the control panel, display, keyboard, and connector panel.
Instrument case two contains the remote control and optical sensing units (rotary wing configuration only), five triaxial accelerometers, three single axis accelerometers, two rotor blade tachometer pickups, various brackets and blocks used for mounting the sensors to the airframe, and accessory cables.
Instrument case three contains the printer disk drive and accessory cables.
Only case number one is included in this auction.(the Computer Indicator)
The power supply and cable are not included.
Item is in overall good physical condition with a small dent in the case and some light rust on the case exterior in spots.
Item is untested.
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