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Identyfikatory
Warianty tytułu
Języki publikacji
Abstrakty
The research presented in this paper focuses on the investigation of helicopter composite blade. The object of tests is a blade from main rotor of the IS-2 helicopter. The author describes briefly basic elements of composite blade manufactured at the Institute of Aviation in Warsaw. The composite blade was investigated by the Experimental Modal Analysis (EMA) to evaluate dynamic properties of tested structure. Based on the experimental data collection, dynamic properties of a research object were estimated. The modal parameters have been estimated using PolyMAX - module of LMS Test.Lab software.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
101--104
Opis fizyczny
Bibliogr. 8 poz., Rys.
Twórcy
autor
- Center of New Technologies, Institute of Aviation, Warszawa, pawel.skalski@ilot.edu.pl
Bibliografia
- 1. Ewins D. J. (2000), Modal testing: theory, practise, and application, Baldock, Research Studies Press, pp. xiii, 562.
- 2. Heylen W., Lammens S., Sas P.theory and testing, Katholieke Universiteit Leueven, Deparment Werktuigkunde.
- 3. Kaczmarczyk J., Rojek M., Wróbel G., Stabik J.A model of heat transfer in composites subjected to thermgraphic testing, Archives of Materials Science and Engineeing, Vol. 31, Isssue 2, 105-108.
- 4. LMS Company – marketing materials.
- 5. Luczak M., Dziedziech K., Vivolo M., Desmet W., Peters B. (2010), Contact versus nontor composite blade, AIP Conf.
- 6. Meinlschmidt P., Aderhold J.spection of rotor blades, ECNDT
- 7. Świderski W. (2009), Nondestructive testing methods and techniques of composite materials by IR thermography, Problemy Techniki Uzbrojenia
- 8. Świderski W., Vavilov V. (2010), Characterization of defects in composite materials by IR thermography nontesting methods, Problemy Techniki Z. 114, nr 4, 33-56.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPB2-0062-0014