Airborne power distribution system for general aviation aircrafts
A technology for power distribution systems, aircraft, used in aerospace
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0018] Such as figure 1 Shown is a structural connection block diagram of a general aviation aircraft onboard power distribution system of the present invention. In the figure, it includes avionics equipment, power system, environmental control system, power supply module, and airborne electrical equipment; the key points of its structure are: the avionics equipment, power system, and environmental control system are connected with a communication module through the CAN bus, The communication module is connected to the CPU module, and the CPU module is connected with a data acquisition module, a state monitoring module, an FPGA module, and a drive control module, and the drive control module is connected with a contactor module; the FPGA module is connected with an expansion interface, The expansion interface is connected with an SSPC device, and the SSPC device is connected with the airborne electrical equipment; the power supply module is a communication module, a CPU module...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


