发明名称 Adaptable boom for in-flight refuelling system
摘要 <p>Boom refuelling system (1) operating between a tanker aircraft (2) and a receiver aircraft (3), comprising a rigid mast (4) and a telescopic tube (5), the system (1) also comprising a first articulation element (10) at its root and a second articulation element (20) at its tip, the boom system (1) further comprising a third articulation element (30) with at least one rotational degree of freedom, located between the first and the second articulation, for allowing the rotation of a part (61, 72) of the boom with respect to the other part (62,71), said articulation element being actuated by at least one actuation means.</p>
申请公布号 EP2447160(B1) 申请公布日期 2013.07.31
申请号 EP20100382282 申请日期 2010.10.27
申请人 EADS CONSTRUCCIONES AERONAUTICAS, S.A. 发明人 MARTINEZ VAZQUEZ, BRUNO;FLORES GIRALDO, SANTIAGO
分类号 B64D39/04 主分类号 B64D39/04
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