Design and Verification of Aircraft Electrical Power System

被引:1
|
作者
Sagirkaya, Huseyin [1 ]
机构
[1] Avion & Elect Engn Turkish Aerosp, Ankara, Turkiye
关键词
Test design; functional test; simulation; electrical system test; load banks;
D O I
10.1109/ESARS-ITEC57127.2023.10114894
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Electrical power system generates, regulates and distributes electrical power throughout the A/C. Aircraft electrical system includes power generation and power distribution system. Distribution of aircraft has contactors, which are located in the plates outside of the power distribution system, to provide control of the system. It is the main system energizing all the equipment on the aircraft. Verification of the system on the laboratory is a critical testing activity to achieve a safe system design. Functional checks, performance and compatibility with the related standards are needed to be tested before aircraft ground and flight tests.
引用
收藏
页数:6
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