The utility model belongs to the technical field of
aviation electromechanics, and relates to detection and maintenance equipment of a refueling control device. The equipment adopts a PXI
bus architecture and mainly comprises a control case, a zero slot controller, a power supply
system, a DA output board card, an AD acquisition board card, a
power load, a DIO board card, an RS422 communication board card, an ARINC429 communication board card, a CAN communication board card and an interface
signal adaptation unit. The equipment is mainly used for testing and maintaining the refueling control device. In the testing process, the refueling control device is connected with the equipment through the interface
signal adapter unit, the equipment power supply
system controls connection of a power supply, the zero slot controller controls the DA output board card, the AD acquisition board card, the
power load and the DIO board card to carry out
signal interaction with the refueling control device, and meanwhile the equipment and the refueling control device carry out data interaction through RS422, ARINC429 and CAN communication buses. The interface function and performance
verification of the refueling control device is realized, and meanwhile, ground data maintenance can be performed.