发明名称 Separable distress beacon for rotorcraft
摘要 <p>The beacon (10) has a detection and control unit (18) connected to a switch (20) and controlling delivery of signals from a transmitter (16) to an aerial (13) exterior to a case (11) or integrated aerial (19) i.e. slot aerial, based on a state of an electromagnetic power sensitive unit (21). The unit (18) is programmed to examine the state at regular time intervals after detection of an incident e.g. shock. The unit (21) measures a standing-wave or voltage standing-wave ratio in a transmission line connecting an output of the switch to a connector (12) that connects the beacon to the aerial.</p>
申请公布号 EP2015100(A1) 申请公布日期 2009.01.14
申请号 EP20080012230 申请日期 2008.07.07
申请人 EUROCOPTER 发明人 DUTRUC, HERVE
分类号 G01S1/68;G01S5/02;H01Q21/28 主分类号 G01S1/68
代理机构 代理人
主权项
地址