发明名称 Method for controlled installation of blind fastener for fixing two parts of structure of aircraft to each other, involves presenting defective character of installation process when calculated energy is lower than threshold value
摘要 <p>The method involves converting acoustic signals into electrical signals, and filtering the electrical signals to identify that the electrical signals are associated with a rupture of a rupture element. The filtered electrical signals are processed to calculate energy of the electrical signals during breaking-out of the rupture element. The calculated energy is compared with a predetermined threshold value. A defective character of an installation process is presented when the calculated energy is lower than the predetermined threshold value. An independent claim is also included for a device for controlled installation of a blind fastener for fixing two parts of an aircraft structure to each other.</p>
申请公布号 FR2999707(A1) 申请公布日期 2014.06.20
申请号 FR20120062098 申请日期 2012.12.14
申请人 AIRBUS OPERATIONS 发明人 TUERY JEAN-BAPTISTE;CHIROL CLEMENT
分类号 G01L5/00;B21J15/04;B21J15/38;F16B19/10 主分类号 G01L5/00
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