基于能量宏观表征的直升机混合动力系统能量管理方法

D. Bienaimé, N. Devillers, M. Péra, F. Gustin, A. Berthon, M. Grojo
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引用次数: 12

摘要

该项目基于嵌入直升机的电网设计。电网为飞机提供辅助设备。它由涡轮交流发电机提供动力,并与其他电源混合使用,以满足辅助设备的需求,并限制主电源的消耗。本文研究的混合系统由主电源(汽轮机和交流发电机)、次电源(蓄电池和超级电容器)和负载(辅机)组成。利用能量宏观表示(EMR)组织了该电网络的模型。根据EMR模型的反演规则确定最大控制结构(MCS)。定义了一种能源管理策略,以共享每个电源提供的电力。这个份额取决于负载的动态。给出了Matlab Simulink™软件的仿真结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Energetic Macroscopic Representation as an efficient tool for energy management in a hybrid electrical system embedded in a helicopter
The project is based on the design of an electric network embedded in a helicopter. The electric network supplies the aircraft auxiliaries. It is powered by a turbo alternator and hybridized with other electric sources in order to fulfil the demand of the auxiliaries and to limit the consumption on the main source. In this paper, the studied hybrid system is composed of the main source (the turbine and the alternator), the secondary source (batteries and supercapacitors) and the load representing the auxiliaries. The model of this electric network is organized by using the Energetic Macroscopic Representation (EMR). A Maximal Control Structure (MCS) is determined by inversion rules of the EMR model. An energy management strategy is defined to share the power supplied by each of the electrical sources. This share depends on the dynamic of the load. Simulation results, using Matlab Simulink™ software, are presented.
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