Problems of Structural Health Monitoring of Aircraft Component

Proceedings of 27th Congress of the International Council of the Aeronautical Sciences (ICAS-2010) 2010
Igors Pavelko, Vitālijs Pavelko, Sergejs Kuzņecovs, Ēriks Ozoliņš, Ilmārs Ozoliņš, Helge Pfeiffer, Martine Wevers

The problems of experimental system of SHM are discussed in this article. The elements of ESHM system were designed and mounted in some zones structure and used far-field and near-field damage detection. As the objects of full-scale testing is used the helicopter MI-8 tail beam that is typical example of Al alloy structure. The ultrasonic methods were selected as a sensitive element of SHM system.

Atslēgas vārdi
aircraft, structural health, monitoring

Pavelko, I., Pavelko, V., Kuzņecovs, S., Ozoliņš, Ē., Ozoliņš, I., Pfeiffer, H., Wevers, M. Problems of Structural Health Monitoring of Aircraft Component. No: Proceedings of 27th Congress of the International Council of the Aeronautical Sciences (ICAS-2010), Francija, Nice, 19.-24. septembris, 2010. Nice: International Council of the Aeronautical Sciences, 2010, 1751.-1758.lpp.

Publikācijas valoda
English (en)