A surface layer (4) formed of a composite material is stacked on the surface (3) of a core layer (2) formed of a foam synthetic resin material, and an arrester portion (5) is provided in an interface region between the surface layer (4) and the core layer (2) to prevent the progression of delamination between the surface layer (4) and the core layer (2). Optical fibers (6a, 6b) with grating portions are embedded inside the arrester (5) and along the surface layer (4), and the spectra (A, B) of reflected light from the optical fibers (6a, 6b) are compared to detect the occurrence position of a crack between the surface layer (4) and the core layer (2).
METHOD FOR DETECTING CRACK OCCURRENCE POSITION
VERFAHREN ZUM DETEKTIEREN EINER BRUCHAUFTRITTSPOSITON
PROCÉDÉ DE DÉTECTION DE LA POSITION DE LA PRÉSENCE DE FISSURES
2019-05-15
Patent
Electronic Resource
English
IPC: | G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / B64C AEROPLANES , Flugzeuge / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen |
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