Aerobridge and control circuit thereof
A technology for controlling circuits and switches, applied to circuit devices, aircraft parts, electrical components, etc., to achieve the effects of low cost, safe take-off, and light weight
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[0021] refer to figure 2 , image 3 , for ease of description, only the parts relevant to the present invention are shown, which are now described in detail as follows: the boarding bridge provided by the embodiment of the present invention is powered by a single-phase UPS power supply 22 when the normal power supply 21 fails, and 201 is the first A control switch, used to control the connection between the boarding bridge and the normal power supply 21, 202 is the first interlock contactor of the first frequency converter 206, used to switch the power supply of the first frequency converter 206, 203 is the first The second interlock contactor of the second frequency converter 207 is used to switch the power supply of the second frequency converter 207. When the normal power supply 21 fails, even if the first control switch 201 is closed, the first and second mutual The coils of the lock contactors 202 and 203 are de-energized, and the inverter is powered by the single-phase...
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