Condition monitoring diagnosis methods of helicopter units

L. M. Gelman, D. A. Kripak, V. V. Fedorov, L. N. Udovenko

Research output: Contribution to journalArticle

13 Citations (Scopus)

Abstract

A non-demountable adaptive automatic method of passive low-frequency (0-25 kHz) vibroacoustical diagnostics of gear cracks is presented. The method is based on signal processing of own vibro and acoustic noise of helicopter engine. The method is promising because it follows to prevent the cracks by ascertaining the causes of the high level of vibration excitation.

Original languageEnglish
Pages (from-to)613-624
Number of pages12
JournalMechanical Systems and Signal Processing
Volume14
Issue number4
DOIs
Publication statusPublished - Jul 2000
Externally publishedYes

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