Investigation of Reconfigurable Battery Efficiency for an Application in an Electrical Sailplane

被引：0

作者：

Sorokina, Nina ^{[1
]}

Hoegerl, Tobias ^{[1
]}

Wolfgang, Bliemetsrieder ^{[1
]}

Hein, Luca ^{[2
]}

Weyh, Thomas ^{[1
]}

Kuder, Manuel ^{[3
]}

机构：

[1] Univ Bundeswehr Munchen, Dept Elect Engn, Neubiberg, Germany

[2] Univ Bundeswehr Munchen, Chair Flight Mech & Flight Control, Neubiberg, Germany

[3] BAVERTIS GmbH, Munich, Germany

来源：

2023 25TH EUROPEAN CONFERENCE ON POWER ELECTRONICS AND APPLICATIONS, EPE'23 ECCE EUROPE | 2023年

关键词：

Modular Reconfigurable Batteries; MOSFET; 3-Level ANPC; Battery Management Systems (BMS); Electrified aircraft; Power losses; DESIGN;

D O I：

暂无

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

This article examines various concepts for propulsion battery concepts for a glider aircraft. These are distinguished by the type of battery pack and by the DC/AC inverter. The different concepts are a conventional battery with fixed series and parallel configuration connected to a three-level inverter, a variable DC voltage source based on dynamically Reconfigurable Battery System (RBS) as the main energy storage unit connected to the same inverter as in a conventional case. The third one is a multi-level energy system containing separate flexibly configurable battery modules for each phase of the electrical motor. All considerations will be made for a three-phase permanent magnet synchronous motor for the maximum power of 80 kW. For each of the energy storage concepts an analysis of the efficiency of the whole system as well as its sub-components was made.

引用

页数：8

共 30 条

[1] Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches [J].

Brelje, Benjamin J. ;

Martins, Joaquim R. R. A. .

PROGRESS IN AEROSPACE SCIENCES, 2019, 104 :1-19

[2]

Buberger Johannes, 2022, PCIM Europe 2022

[3]

International Exhibition and Conference for Power Electronics, Intelligent Motion, Renewable Energy and Energy Management, P1, DOI 10.30420/565822230

[4] Preliminary Design of a Solar-Powered Hybrid Airship [J].

Buckley, Howard P. ;

Holt, Nick ;

Leinonen, Andrew ;

Fournier, Sebastien ;

Zingg, David W. .

JOURNAL OF AIRCRAFT, 2020, 57 (02) :256-267

[5]

EMRAX Innovative Motors, 2018, US MAN ADV AX FLUX S

[6]

Grupp W., 2023, P 6 INT C SUST EN SC

[7]

Hein L., 2022, Simulation of an Electric Powered Aircraft for Flight &amp

[8]

Mission Performance Evaluation, DOI [10.2514/6.2022-3572, DOI 10.2514/6.2022-3572]

[9] Power management control and delivery module for a hybrid electric aircraft using fuel cell and battery [J].

Hoenicke, Pia ;

Ghosh, Debjani ;

Muhandes, Adel ;

Bhattacharya, Sumantra ;

Bauer, Christiane ;

Kallo, Josef ;

Willich, Caroline .

ENERGY CONVERSION AND MANAGEMENT, 2021, 244

[10]

Infineon Technologies AG, 2022, BSC005N03LS5 MOSFET OptiMOSTM5 PowerTransistor, 30V, P12

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