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

A technology of power supply capacity and electrical load, which is applied in the field of aircraft electrical load statistics and power supply capacity analysis methods and systems, can solve the problems of complicated and cumbersome manual calculation process, inability to adapt, and low efficiency, and achieves efficient and accurate aircraft electrical load statistics and systems. Effects of Power Capacity Analysis

Inactive Publication Date: 2019-04-05
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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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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  • Airplane electrical load statistics and power supply capacity analysis method and system
  • Airplane electrical load statistics and power supply capacity analysis method and system
  • Airplane electrical load statistics and power supply capacity analysis method and system

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[0043] The application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the related application, not to limit the application. In addition, it should be noted that, for ease of description, only parts relevant to the present application are shown in the drawings.

[0044] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and embodiments.

[0045] It should be noted that in the description of this application, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The terms of the indicated direction or positional relationship are based on the direction or positional ...

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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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/40
CPCG01R31/40
Inventor 郭彦峰刘亮铁诚
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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