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MONITORING UNIT AND METHOD FOR DETECTING STRUCTURAL DEFECTS WHICH CAN OCCUR IN AN AIRCRAFT NACELLE DURING USE
MONITORING UNIT AND METHOD FOR DETECTING STRUCTURAL DEFECTS WHICH CAN OCCUR IN AN AIRCRAFT NACELLE DURING USE
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机译:使用过程中在飞机纳赛尔中可能出现的结构缺陷的监测单元和方法
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摘要
The invention relates to a monitoring unit (11) which includes a composite sandwich structure (10) forming a portion of the aircraft nacelle (1), a plurality of sensors (14) for generating signals representative of an amplitude and/or frequency of vibrations. Each sensor (14) transmits said signals via electromagnetic waves, e.g. via radio frequencies. Each sensor (14) is an electromechanical microsystem including a means for converting mechanical energy into electrical energy. A computing unit (15) is suitable for: evaluating the differences between a current transfer function resulting from said signals and a predetermined nominal transfer function; comparing each of said differences with a respective detection threshold; and, from said comparison, estimating or evaluating the size and/or position of said structural defect in the structure (10).
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