Power management strategies in a local DC Power Distribution System of More Electric Aircraft with the help of hybrid storage and dissipation systems

2009 ◽  
Author(s):  
H. Zhang ◽  
H. Fakham ◽  
C. Saudemont ◽  
B. Robyns
Keyword(s):  
Power Management ◽  
Power Distribution ◽  
Distribution System ◽  
Management Strategies ◽  
Power Distribution System ◽  
Hybrid Storage ◽  
Dc Power ◽  
Electric Aircraft ◽  
More Electric Aircraft

scholarly journals Modeling and Simulation of Power Distribution System in More Electric Aircraft

2015 ◽  
Vol 2015 ◽  
pp. 1-7 ◽  
Author(s):  
Zhangang Yang ◽  
Junchao Qu ◽  
Yingchuan Ma ◽  
Xudong Shi
Keyword(s):  
Power System ◽  
Simulation Model ◽  
Power Distribution ◽  
Distribution System ◽  
Transient State ◽  
Maintenance Cost ◽  
Power Distribution System ◽  
System Integrity ◽  
Electric Aircraft ◽  
More Electric Aircraft

The More Electric Aircraft concept is a fast-developing trend in modern aircraft industry. With this new concept, the performance of the aircraft can be further optimized and meanwhile the operating and maintenance cost will be decreased effectively. In order to optimize the power system integrity and have the ability to investigate the performance of the overall system in any possible situations, one accurate simulation model of the aircraft power system will be very helpful and necessary. This paper mainly introduces a method to build a simulation model for the power distribution system, which is based on detailed component models. The power distribution system model consists of power generation unit, transformer rectifier unit, DC-DC converter unit, and DC-AC inverter unit. In order to optimize the performance of the power distribution system and improve the quality of the distributed power, a feedback control network is designed based on the characteristics of the power distribution system. The simulation result indicates that this new simulation model is well designed and it works accurately. Moreover, steady state performance and transient state performance of the model can fulfill the requirements of aircraft power distribution system in the realistic application.

Load Control for the DC Electrical Power Distribution System of the More Electric Aircraft

2019 ◽  
Vol 34 (4) ◽  
pp. 3937-3947 ◽  
Author(s):  
Sandro Gunter ◽  
Giampaolo Buticchi ◽  
Giovanni De Carne ◽  
Chunyang Gu ◽  
Marco Liserre ◽  
...  
Keyword(s):  
Power Distribution ◽  
Distribution System ◽  
Electrical Power ◽  
Load Control ◽  
Power Distribution System ◽  
Electric Aircraft ◽  
More Electric Aircraft
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