发明名称 TRANSDUCER MOUNTING STRUCTURE FOR A VERTICAL TAIL OF AN AIRCRAFT
摘要 <p>A transducer mounting structure for a vertical tail of an aircraft comprises a mounting bracket (6) which comprises a transducer rod mounting bracket (6) which comprises a transducer rod mounting portion (61) extending outwardly from a body of the mounting bracket, the transducer rod mounting portion being pivotally connected to a rod (41) of a transducer (4); and a mounting flange (62) extending outwardly form the body of the mounting bracket (6), the mounting flange (620 being secured to a fitting (5) of the vertical tail; wherein said mounting flange (62) extends outwardly in an approximately vertical direction, and is secured to a side surface of a stiffener (53) of the fitting (5). With the vertical mounting configuration, no intervention will occur during the process of drilling holes and mounting the transducer, thus the productivity is improved greatly.</p>
申请公布号 WO2012024838(A1) 申请公布日期 2012.03.01
申请号 WO2010CN76384 申请日期 2010.08.26
申请人 AIRBUS SAS;LI, YUPING 发明人 LI, YUPING
分类号 B64D45/00;G01B21/22 主分类号 B64D45/00
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