| 摘要 |
<p>The invention relates to a system for monitoring the quality of a structural component (1) of an aircraft, comprising: - a device for monitoring an internal structure (10) of the structural component (1) by ultrasound measurement, - a device for monitoring an exterior aspect (20) of a surface of the structural component (1) by optical measurement, - a robotized support (4), supporting both the device for monitoring an internal structure and the device for monitoring an exterior aspect, which is able to scan successively each zone (z1, z2, zn) of the surface of the structural component (1) so as to simultaneously monitor a state of the internal structure and an aspect of the exterior surface of the structural component, and - a device (3) for processing ultrasound data transmitted by the device for monitoring an internal structure (10) and optical data transmitted by the device for monitoring an exterior aspect (20).</p> |
