Regular signal of a time-synchronous averaged signal
computes the regular signalY
= tsaregular(X
,fs
,rpm
,orderList
)Y
of the time-synchronous averaged (TSA) signal vectorX
using sampling ratefs
, the rotational speedrpm
, and the orders to be retainedorderList
.Y
is computed by retaining the primary frequency, the components inorderList
, and their respective harmonics fromX
. You can useY
to further extract condition indicators of rotating machinery for predictive maintenance. For example, extracting theFM0indicator fromY
is useful in identifying major changes such as gear tooth breakage or heavy wear in a gear box.
___= tsaregular(___,
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.Name,Value
)
tsaregular(___)
with no output arguments plots the time-domain and frequency-domain plots of the raw and regular TSA signals.
Regular Signal
The regular signal is computed from the TSA signal by retaining the following from the signal spectrum:
Shaft frequency and its harmonics
Gear meshing frequencies and their harmonics
Optionally, the sidebands specified in 'NumSidebands
' at the gear meshing frequencies and their harmonics
tsaregular
uses a bandwidth equal to the shaft speed times the value of 'NumSidebands
', around the frequencies of interest, to computeY
from the TSA signal. The regular signal is related to the residual signal through the equation
. If the first-order sidebands are retained in the regular signal, then,
.
Amplitude Spectrum
The amplitude spectrum of the regular signal is computed as follows,
Here,Y
is the regular 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 Polytechnica45.6 (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.