The invention belongs to the technical field of aircraft power supply systems, and particularly relates to an aircraft single-phase emergency
alternating current power supply
system and a switching method. Comprising an
AC power distribution box, an emergency
AC power control box, a DC power distribution box, a
power control and display module and a static converter. The
alternating current power distribution box is used for connecting an onboard main
alternating current power supply or an auxiliary alternating current power supply or a static converter power supply, supplying power to alternating
current electric equipment and transmitting a single-phase normal alternating current
bus bar power supply to the emergency alternating current power supply control box; the emergency
AC power supply control box is used for carrying out real-time
power loss monitoring on a single-phase normal AC
bus bar in the AC power
supply distribution box, connecting the single-phase normal AC
bus bar in the AC power
supply distribution box with a single-phase emergency AC bus bar when
power loss is monitored, and connecting the single-phase emergency AC bus bar with the single-phase normal AC bus bar in the AC power
supply distribution box when
power loss is monitored. The static converter is connected with the single-phase emergency AC bus bar, and self state information and output power information of the static converter are fed back to the
power control and display module; the direct-current power supply distribution box is used for accessing an
airplane direct-current power supply, providing an emergency direct-current power supply for the power supply control and display module and the static converter, and realizing power supply
input control and short-
circuit protection of the static converter; and the static converter is used for converting the emergency direct-current power supply output by the direct-current power supply distribution box into a single-phase alternating-current power supply and feeding back state information of the static converter to the power supply control and display module. The problem of reliable and automatic conversion of the single-phase emergency alternating current power supply under the condition that the
airplane loses a main power supply
system and an auxiliary power supply
system and a normal alternating current bus bar loses power is solved.