N. Takeda, N. Tajima, T. Sakurai

The Japanese Smart Material/Structure System Project started in 1998 with four research groups, such as (1) structural health monitoring, (2) smart manufacturing, (3) active/adaptive structures, and ( 4) actuator material/device development. Based on the above research accomplishment, two Demonstrators were fabricated and tested in late 2002. This paper presents a summary of test results obtained in the damage detection and suppression composite fuselage demonstrator program where novel developed monitoring techniques such as small-diameter optical fiber sensors were implemented in the composite structure. This damage detection and suppression composite fuselage demonstrator provided the solid foundation for more practical applications of structural health monitoring technology in advanced large-size composite structures.

23rd ICAF Symposium of the international Committee on Aeronautical Fatique, 2005, Hamburg

Conference Paper

englisch

A5, 10 Seiten

DGLR-Bericht, 2005, 2005-03, 23rd ICAF Symposium of the international Committee on Aeronautical Fatique - Proceedings; S.209-218; 2005; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

composite structures, structural health monitoring, damage detection, optical fibers, sensors

Bestellbar

2005