发明名称 SAFETY SYSTEM FOR AN AIRCRAFT
摘要 In a safety system (S) for an aircraft (1) for storing flight (FD) and voice data (SD) relevant for reconstructing crashes, comprising a data collection device (6) which is connected to sensors (4, 5) of the aircraft (1) and by means of which relevant flight data (FD) and voice data (SD) of the aircraft (1) can be collected and stored by means of a black box-terra (7) which is substantially inseparably attached to the aircraft (1), the black box-terra (7) being accommodated in an impact-proof and fireproof housing, a data splitter (9, 15) is provided by means of which the flight (FD) and voice data (SD) to be stored in the black box-terra (7) can be delivered in parallel to a black box-water (8; 8.1 to 8.9), and it is furthermore provided that the black box-water (8; 8.1 to 8.9) is likewise designed for storing the collected flight (FD) and voice data (SD), wherein the black box-water (8; 8.1 to 8.9) comprises a floating body or is designed to be self-floating and is designed to emit an alarm signal locatable by a satellite, immediately before, during or after a crash of the aircraft, after having been separated from the aircraft (1) and upon an automatic or manual activation.
申请公布号 US2012232746(A1) 申请公布日期 2012.09.13
申请号 US201013513193 申请日期 2010.12.02
申请人 WIEDERWOHL KURT O.;BDP SICHERHEITSTECHNOLOGIEN GMBH 发明人 WIEDERWOHL KURT O.
分类号 G07C5/08;B64D25/00;B64D45/00 主分类号 G07C5/08
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