tsadifference
Difference signal of a time-synchronous averaged signal
Syntax
Description
computes the difference signal Y
= tsadifference(X
,fs
,rpm
,orderList
)Y
of the time-synchronous averaged
(TSA) signal vector X
using sampling rate fs
,
the rotational speed rpm
, and the orders to be filtered
orderList
. Y
is computed by removing the
regular signal, the value of 'NumSidebands
', and their respective
harmonics from X
. For more information on regular signal, see
tsaregular
.
You can use Y
to further extract condition indicators of rotating
machinery for predictive maintenance. For example, extracting the
FM4 indicator from Y
is useful to detect
faults isolated to only a limited number of teeth in a gear mesh.
___ = tsadifference(___)
allows you to
specify additional parameters using one or more name-value pair arguments. You can use
this syntax with any of the previous input and output arguments.
tsadifference(___)
with no output arguments plots the
time-domain and frequency-domain plots of the raw and difference TSA signals.
Examples
Input Arguments
Output Arguments
Algorithms
Difference Signal
The difference signal is computed from the TSA signal by filtering the following from the signal spectrum:
Shaft frequency and its harmonics
Gear meshing frequencies and their harmonics
First-order sidebands at the gear meshing frequencies and their harmonics
Optionally, the sidebands specified in '
NumSidebands
' at the gear meshing frequencies and their harmonics
tsadifference
uses a bandwidth equal to three times the shaft speed and the
value of 'NumSidebands
', around the frequencies of interest, to compute
Y
from the TSA signal.
Amplitude Spectrum
The amplitude spectrum of the difference signal is computed as follows,
Here, Y
is the difference signal.
References
[1] McFadden, P.D. "Examination of a Technique for the Early Detection of Failure in Gears by Signal Processing of the Time Domain Average of the Meshing Vibration." Aero Propulsion Technical Memorandum 434. Melbourne, Australia: Aeronautical Research Laboratories, Apr. 1986.
[2] Večeř, P., Marcel Kreidl, and R. Šmíd. "Condition Indicators for Gearbox Monitoring Systems." Acta Polytechnica 45.6 (2005), pages 35-43.
[3] Zakrajsek, J. J., Townsend, D. P., and Decker, H. J. "An Analysis of Gear Fault Detection Methods as Applied to Pitting Fatigue Failure Data." Technical Memorandum 105950. NASA, Apr. 1993.
[4] Zakrajsek, James J. "An investigation of gear mesh failure prediction techniques." National Aeronautics and Space Administration Cleveland OH Lewis Research Center, 1989. No. NASA-E-5049.
Extended Capabilities
Version History
Introduced in R2018b