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Abstrakty
Traditionally helicopter gearbox failure analysis has been achieved in a number of ways, including the recording of the oil temperature and oil pressure of critical components within the transmission system. Vibration monitoring techniques provide a sufficient level of detail such that all drive train components can be monitored throughout flight. Each indicator relates to specific faults, such as shaft misalignment, gear tooth cracking, bearing inner-race damage, and lubrication problems.
Rocznik
Tom
Strony
54--57
Opis fizyczny
Bibliogr. 5 poz., rys.
Twórcy
autor
- Faculty of Aeronautics of Technical University of Košice, Department of aviation engineering, Košice, Slovak Republic
autor
- Faculty of Aeronautics of Technical University of Košice, Department of avionics, Košice, Slovak Republic
autor
- Faculty of Aeronautics of Technical University of Košice, Department of avionics, Košice, Slovak Republic
Bibliografia
- [1] Choy, F. K., Huang, S. J., Zakrajsek, J., Handschuh, R. F., Townsend, D. P.: Vibration Signature Analysis of a Faulted Gear Transmission System. NASA/TM-2008-215262.
- [2] Dempsey, P. J., Keller, J. A., Wade, D.R.: Glenn Research Center, Signal Detection Theory Applied to Helicopter Transmission Diagnostic Thresholds.
- [3] Tumer, I. Y., Huff, E. M.: Analysis of Triaxial Vibration Data for Health Monitoring of Helicopter Gearboxes, Computational Sciences Division, NASA Ames Research Center, Moffett Field, CA 94035, 2003.
- [4] Pil'a, J., Sloboda, A. ml.: Niektorè možnosti využitie diagnostických parametrov pre proaktivnu udržbu lietadiel. In: DIS 2004, Košice, 2004, 4 str. ISBN 80-232-0237-5.
- [5] Neštrák, D., Pil'a, J.: Aerodynamika, konstrukce a systémy vrtulniků: Učebni texty dle nařízeni komise (ES) 2042/2003 Part 66: Studijni modul 12.1. Akademické nakladatelství CERM, Brno, 2006. 454 str. ISBN 80-7204-484-2.
Typ dokumentu
Bibliografia
Identyfikator YADDA
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