Aircraft hybrid bus system

Abstract

The invention discloses an aircraft hybrid bus system, which comprises an intelligent control unit, a cluster management module and a basic power supply assembly, and is characterized in that the intelligent control unit is used as upper computer control software to realize the program control management of the running state of an aircraft; receiving and displaying aircraft working state program control information transmitted by the cluster management module through a network through a real-time Ethernet, generating and sending an airborne equipment operation program control instruction to the cluster management module, and controlling the operation state of the aircraft; the cluster management module is connected with the plurality of basic power supply assemblies through a network interface, and controls the plurality of basic power supply assemblies to work through a power supply and distribution strategy; the power supply and distribution strategy comprises the following steps: after receiving a program control instruction sent by the intelligent control unit, the cluster management module generates a power distribution control instruction to the basic power supply assembly to control the basic power supply assembly to operate or stop; the basic power supply assembly is used for supplying power to airborne equipment and has a power storage function; and the basic power supply assembly performs energy scheduling according to the power distribution control instruction.

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