发明名称 Bus system for an aircraft
摘要 The present invention relates to a bus system for transmitting a data packet between multiple devices in an aircraft, which is based on the CAN data bus system, but has an expanded identification field, in which a fixed region is designed for identification of the manifold aircraft systems, through which each aircraft system may be addressed uniquely. According to an exemplary embodiment, the data packet may be sent with different priorities, through which "important" data packets have priority on the transmission medium.
申请公布号 US7433354(B2) 申请公布日期 2008.10.07
申请号 US20040014284 申请日期 2004.12.16
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 SCHERER THOMAS;VON DOEHLEN VOLKER
分类号 H04L12/28;H04L12/413;H04L12/56 主分类号 H04L12/28
代理机构 代理人
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