Intelligent Power Distribution for Aircraft - Load Management

The Electrical Load Management Center is used for intelligent management of model electrical loads. It organically combines SSPC modules with intelligent and network functions through data processing units, and implements various logical switching functions based on instructions issued by the upper computer system. It plays a role as a connecting link within the system and is a new application technology for data acquisition, overload protection, data integration, and fault recording of control parameters, greatly improving the reliability, maintainability, and scalability of the system. At the same time, it uses intelligent modules to replace the operation of drivers for automatic control and load management, which can greatly reduce the workload of drivers

Electrical Load Management Center

Used for intelligent management of model electrical loads, it organically combines SSPC modules with intelligent and network functions through a data processing unit, and implements various logical switching functions based on instructions issued by the upper computer system. It plays a role as a connecting link within the system and is a new application technology for data acquisition, overload protection, data integration, and fault recording of control parameters, greatly improving the reliability, maintainability, and scalability of the system. At the same time, it uses intelligent modules to replace the operation of drivers for automatic control and load management, which can greatly reduce the burden on drivers and improve existing power distribution and load management methods. Main performance indicators:

Main performance indicators:

Working voltage: 27Vd. c./120Vd. c./270Vd. c. Working temperature: -40~85 ℃

Load power characteristics: ≤ 100A/Ch, customizable number of channels Control mode: switch control/bus control

Control mode: Three modes (remote control, local control, and emergency control) Environmental adaptability: meets the relevant requirements of GJB1032-1990 and GJB150A-2009 Electromagnetic compatibility: meets the relevant electromagnetic environment requirements of GJB151A-1997

Communication interfaces: RS485, RS422, CAN, Ethernet, MIL-STD-1553B and other bus interfaces Electrical interfaces: connectors, busbars or terminals

Structural form: Standard chassis or customized chassis Average time between failures: up to 20000 hours

Service Hotline: 18576510868



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