Airplane electrical load statistics and power supply capacity analysis method and system

Abstract

The invention belongs to the technical field of airplane electrical load statistics and power supply capacity analysis. On the one hand, an airplane electrical load statistics and power supply capacity analysis method is provided; the method comprises the steps of acquiring the load information of an airplane and acquiring a total power requirement of the load of the airplane at a set stage according to the load information of the airplane, acquiring the power supply information of the airplane and acquiring a corrected capacity that can be output by the power supply of the airplane at the setstage, and acquiring a residual capacity according to the total power requirement and the corrected capacity; furthermore, whether the power supply capacity accords with a corresponding design specification and whether the power supply capacity can meet the power supply requirement of the electrical load on the airplane can be judged according to the residual capacity. On the other hand, an airplane electrical load statistics and power supply capacity analysis system is provided to implement the abovementioned method, and thus the airplane electrical load statistics and power supply capacityanalysis can be automatically, efficiently and accurately achieved.

Description

technical field [0001] The application belongs to the technical field of aircraft electrical load statistics and power supply capacity analysis, and specifically relates to a method and system for aircraft electrical load statistics and power supply capacity analysis. Background technique [0002] Electrical load statistics and power supply capacity analysis are the basic work in the design stage of the aircraft power supply system, and are also the primary and indispensable technical links in the design of the aircraft power supply system. In the design stage of the aircraft power supply system, the electrical load is counted and the power capacity is analyzed, and the appropriate capacity margin and transient requirements are considered to verify whether the power capacity meets the corresponding design specifications and whether it can meet the requirements of the electrical load on the aircraft. It is of great significance to ensure the safety and reliability of electric...

AI Technical Summary

Problems solved by technology

[0003] At present, there is a lack of a systematic, efficient and automated analysis tool for electrical load statistics and power supply capacity. When performing aircraft electrical load statistics and power supply capacity analysis, it mainly relies on manual statistics and manual calculations by relevant designers. Due to aircraft There are many types of loads and different uses, which makes the manual statistics and manual calculation process complex and cumbersome, and cannot eliminate the influence of subjective and objective factors on its accuracy, consumes a lot of manpower, material resources and experience, and is inefficient. Can adapt to the needs of the rapid development of the current technological level

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