Difference signal of a time-synchronous averaged signal
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.
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.
[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.