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Tray-adapted support power supply for electronic aviation equipment

机译:适用于托盘的电子航空设备支持电源

摘要

Invention Patent: "SUPPORT ENERGY SUPPLY ADAPTED IN TRAY FOR ELECTRONIC AVIATION EQUIPMENT". A support power supply for electronic aviation equipment that can be installed in existing electronic aviation equipment trays without having to restart the aircraft. According to a preferred embodiment of the invention (described for illustrative purposes in the context of providing a supporting power supply for a cabin voice recorder (CVR)), the power supply / CVR combination is retrofitted on a CVR rack existing. The energy supply is, according to the preferred modality mentioned above, modular; removable / replaceable; and is "independent" with respect to the main power source and aircraft connection. The power supply / CVR combination is designed to fit into a conventional CVR tray; and the CVR is designed to fit the modular power supply. In addition, according to a preferred mode, the power supply is "plug compatible" with the electrical connector on the CVR tray and includes a circuit that allows the power supply and CVR to be tested using the test button CVR in the cab; and to report the deficiencies of each unit using existing aircraft connections. In addition, the power supply includes a circuit that automatically disconnects electrically from the CVR and the exposed pins when the power supply is removed from the CVR tray. The CVR and the power supply of the preferred modality of the invention, being modular, are easy to install, do not require cables, occupy approximately the same space previously occupied by the existing CVR, and have the same center of gravity as the existing CVR. Integrated aviation electronics / support power supply units are also considered by the invention where the units are designed to fit into existing equipment trays to eliminate and / or minimize the need to restart the aircraft.
机译:发明专利:“托盘中为电子航空设备提供的支持能源”。用于电子航空设备的辅助电源,可以将其安装在现有的电子航空设备托盘中,而不必重启飞机。根据本发明的优选实施例(在为机舱语音记录器(CVR)提供辅助电源的情况下出于说明目的而描述),电源/ CVR组合被改装在现有的CVR机架上。根据上面提到的优选方式,能量供应是模块化的。可移动/可更换;并且在主电源和飞机连接方面是“独立的”。电源/ CVR组合设计为可放入常规CVR托盘中; CVR设计为适合模块化电源。另外,根据优选模式,电源与CVR托盘上的电连接器“插头兼容”,并且包括允许使用驾驶室中的测试按钮CVR对电源和CVR进行测试的电路。并使用现有的飞机连接报告每个单元的缺陷。另外,电源设备包括一个电路,当从CVR托盘中卸下电源设备时,该电路会自动自动与CVR和裸露的引脚断开电连接。本发明的优选方式的CVR和电源是模块化的,易于安装,不需要电缆,占用现有CVR先前占据的大致相同的空间,并且具有与现有CVR相同的重心。本发明还考虑了集成的航空电子/辅助电源单元,其中该单元被设计成可安装到现有设备托盘中,以消除和/或最小化重新启动飞机的需要。

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