elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

Impact of pulse time uncertainty on synchronous average: Statistical analysis and relevance to rotating machinery diagnosis

Camerini, Valerio und Coppotelli, Giuliano und Bendisch, Stefan und Kiehn, Daniel (2019) Impact of pulse time uncertainty on synchronous average: Statistical analysis and relevance to rotating machinery diagnosis. Mechanical Systems and Signal Processing (MSSP), 129, Seiten 308-336. Elsevier. doi: 10.1016/j.ymssp.2019.04.017. ISSN 0888-3270.

[img] PDF - Postprintversion (akzeptierte Manuskriptversion)
3MB

Offizielle URL: https://www.sciencedirect.com/science/article/pii/S0888327019302481

Kurzfassung

Time synchronous averaging for the extraction of periodic waveforms is a rather common processing method for rotating machinery diagnosis. By synchronizing the signal to the rotational angle of the component of interest, e.g. by using keyphasor reference signal, it is possible to perform the averaging in the angular domain, thus obtaining an anglesynchronous signal. Jittering of the reference signal affects the quality of the synchronous averaging process, resulting in attenuation and uncertain estimation of the extracted synchronous signal, especially in the high frequency band. In this paper, the effects of random uncertainty in the pulse arrival times of the reference signal on the synchronous averaging method are studied, with the objective of assessing the relevance of such a jitter error to the extracted waveform and the indicators derived for monitoring purposes. First, a unified framework for the computed order tracking method is presented, and then a model linking the statistics of the random jitter to the statistics of the waveform extracted through synchronous averaging in angle domain is developed. The theoretical model connects the random jitter distribution, the number of averaged periods and the ratio of the period of interest to the reference trigger period, to the distribution of the amplitudes of the synchronous frequency components in the synchronously averaged signal. Approximate analytical solutions are derived for cases of interest, allowing the prediction of the attenuation bias and variability of the extracted components amplitudes. The model is first verified against numerical simulations in order to assess consistency, and then parametric studies are presented. Experimental validation is performed on both an experimental and an operational data sets involving respectively a helicopter gearbox and a helicopter fleet.

elib-URL des Eintrags:https://elib.dlr.de/125263/
Dokumentart:Zeitschriftenbeitrag
Titel:Impact of pulse time uncertainty on synchronous average: Statistical analysis and relevance to rotating machinery diagnosis
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Camerini, ValerioDepartment of Aerospace Engineering and Astronautics, University of Rome "La Sapienza", 00184 Rome, Italyhttps://orcid.org/0000-0003-1425-3175NICHT SPEZIFIZIERT
Coppotelli, GiulianoDepartment of Aerospace Engineering and Astronautics, University of Rome "La Sapienza", 00184 Rome, Italyhttps://orcid.org/0000-0003-0254-4987NICHT SPEZIFIZIERT
Bendisch, StefanAirbus Helicopters Deutschland, 86609 Donauwörth, GermanyNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Kiehn, DanielDLR Institut für Flugsystemtechnik, 38108 Braunschweighttps://orcid.org/0000-0001-7383-0740NICHT SPEZIFIZIERT
Datum:15 August 2019
Erschienen in:Mechanical Systems and Signal Processing (MSSP)
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:129
DOI:10.1016/j.ymssp.2019.04.017
Seitenbereich:Seiten 308-336
Verlag:Elsevier
ISSN:0888-3270
Status:veröffentlicht
Stichwörter:Health Monitoring, Vibration Monitoring, Synchronous Average, Diagnose
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Hubschrauber
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L RR - Rotorcraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Der robuste Drehflügler (alt), L - Der intelligente Drehflügler (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Flugsystemtechnik > Flugdynamik und Simulation
Hinterlegt von: Kiehn, Daniel
Hinterlegt am:14 Jun 2019 16:19
Letzte Änderung:19 Aug 2021 03:00

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.