Condition monitoring diagnosis methods of helicopter units

Mechanical Systems and Signal Processing

Volumn 14, Issue 4, 2000, Pages 613-624

  Gelman, L M ^a   Kripak, D A ^a   Fedorov, V V ^a   Udovenko, L N ^a  

^a NATIONAL TECHNICAL UNIVERSITY OF UKRAINE   (Ukraine)

Author keywords

[No Author keywords available]

Indexed keywords

CRACKS; FATIGUE OF MATERIALS; MACHINE VIBRATIONS; PARAMETER ESTIMATION; PREVENTIVE MAINTENANCE; PROBABILITY;

AERODYNAMICAL EXCITATION; CONDITION MONITORING DIAGNOSIS METHODS; MECHANICAL EXCITATION; VIBROACOUSTICAL DIAGNOSTICS;

HELICOPTER ROTORS;

EID: 0034215808     PISSN: 08883270     EISSN: None     Source Type: Journal    
DOI: 10.1006/mssp.2000.1295     Document Type: Article

References (4)

1. L. M. GELMAN, Y. V. BURAU and V. I. KRYTSYN 1995 Proceedings of the International Symposium of Nondestructive Testing in Civil Engineering, Berlin, Germany, 1311-1317. Automatic adaptive method for nondestructive testing in civil engineering.
2. S. P. YAO and P. D. MCFADDEN 1998 Proceedings of the 3rd International Conference on Acoustical and Vibratory Surveillance Methods and Diagnostic Technique, Senlis, France, 555-564. Study of modelling of monitoring of gearbox vibration.
3. L. M. GELMAN 1995 Telecommunication and Radio Engineering 49, 70-73. Optimization of the carrier frequency for receiving a modulated signal.
4. M. HORSEY 1993 Westland Helicopter Ltd, Mechanical Research Report MRR 20168, Issue 1. WHL vibration analysis results from H46 AFT gearbox testing.