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Energy feedback type aircraft electrical load simulation method and device

An electrical load and simulation device technology, applied in the field of aviation electrical systems, can solve the problems of time-consuming, labor-intensive, expensive, and difficult to implement, and achieve the effects of saving space, reducing noise pollution, and saving energy.

Active Publication Date: 2016-08-10
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

The starting system and power distribution system on the aircraft need to be tested with load in the early stage of laboratory demonstration, but using real load in the laboratory demonstration stage is not only time-consuming, laborious, expensive, and often difficult to achieve

Method used

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  • Energy feedback type aircraft electrical load simulation method and device
  • Energy feedback type aircraft electrical load simulation method and device
  • Energy feedback type aircraft electrical load simulation method and device

Examples

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Embodiment

[0046] Figure 4 In order to simulate the steps of the starter generator as an example, first build the simulink simulation model according to the parameters of the starter generator used by the aircraft, and then import the simulation model into the real-time simulation platform of the load characteristic controller, and then run the real-time simulation to achieve the simulation The purpose of the electrical load of the starter generator, according to the subsequent needs, such as if the stator resistance and inductance parameters of the starter generator change, can modify and adjust the parameters of the starter generator to simulate the starter generator under different parameters.

[0047] Figure 5 , Figure 6 , Figure 7 It is a simulation realization process taking starter generator as an example, Figure 6 M represents the starter generator simulation model in the load characteristic controller, Figure 7 where TC represents the transformer simulation model in th...

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Abstract

The invention belongs to the field of aviation electrical systems, and especially relates to an energy feedback type aircraft electrical load simulation method and device, wherein a load simulator and a grid connected inverter are comprised. The simulation device comprises an isolation transformer which is used for providing right voltage or current for an integrated power supply and physically isolating a power grid and the simulation device, the integrated power supply used for providing a voltage source of an electrical load, and an electrical load simulation device which is used for simulating the electrical load. According to the invention, a power electronic converter technology is used to simulate the aircraft electrical load; on the basis that the preliminary laboratory demonstration phase load test of a start system, a distribution system and the like on an aircraft is completed, energy output by an electrical simulation load is recycled; energy is saved; a lot of heat can be avoided; the space of a cooling device is saved; noise pollution is greatly reduced; the cost is saved; and technology and research foundations are provided for developing existing wide body aircrafts and future green environment-friendly all-electric aircrafts.

Description

technical field [0001] The invention belongs to the field of aviation electrical systems, and in particular relates to an energy feedback type aircraft electrical load simulation method and device including a load simulator and a grid-connected inverter. Background technique [0002] At present, one type of aircraft electrical analog load is a resistive load, which is not only inconvenient to adjust, but also difficult to control accurately. The size and parameters of the load will change with the change of the load and the ambient temperature, and cause a large amount of electrical energy to be converted into heat and lost. Coupled with the required cooling equipment, it not only requires extra space, but also requires additional operating costs, and will cause noise pollution to the environment. With the advancement of research on wide-body aircraft and more electric aircraft, the number and types of aircraft electrical loads have increased by an order of magnitude compare...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/00G09B25/02
CPCG09B9/00G09B25/02
Inventor 康元丽回彦年王春成马跃
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC
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