Start control system for aircraft engine
An aircraft engine, starting control technology, applied in the direction of engine starting, machine/engine, engine ignition, etc., can solve the problems of short life and large volume, and achieve the effect of long life, small size and light weight
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[0013] As shown in the figure, the starting control system includes computer printed board (A1), interface printed board (A2), power supply printed board (A3), output processing printed board (A4), transfer printed board (A5) , the chassis, the transfer printed board (A5) is connected to all printed boards through connectors and installed in the chassis, the computer printed board (A1) includes 1394B processing circuit (A1-1), CPU circuit (A1 -2), RS422 and network port circuit (A1-3), CPU circuit (A1-2) includes MPC processor and system logic unit FPGA through local bus communication, the PCI bus of MPC processor expands out 3 roads 1394 interfaces, Connect with 1394B processing circuit (A1-1); expand 2 RS422 serial ports and 1 debugging network port to connect with RS422 and network port circuit (A1-3), 1394 processing circuit (A1-1) connects with external The aircraft computer (UCP) is connected, the RS422 and the network port circuit (A1-3) are connected with the debugging...
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