IWSHM-2011
Описание
This paper presents the design of a self-powered impact sensor dedicated to Structural Health Monitoring for aeronautic applications. The purpose of this work is to identify and implement technological solutions that meet specific requirements for on-ground operation. A prototype featuring thermal energy harvesting, super-capacitor-based energy storage and 3D-accelerometry is demonstrated.
Содержание
|
Регламенты
25 декабря 2013
09 января 2014
|