计算机与网络
計算機與網絡
계산궤여망락
CHINA COMPUTER & NETWORK
2015年
14期
55-58
,共4页
固态功率控制器%配电系统%多电飞机%加电控制单元
固態功率控製器%配電繫統%多電飛機%加電控製單元
고태공솔공제기%배전계통%다전비궤%가전공제단원
solid-state power controller (SSPC)%power distribution system%more electric aircraft%power control unit
以现代多电飞机对新型配电系统的迫切需求为牵引,以新型配电系统核心部件新型执行器件固态功率控制器的应用为手段,系统地阐述了新型执行器件固态功率控制器的设计原理以及电路设计方法.实验通过某型号任务对加电控制单元的要求,利用SSPC加以实现,并与常规器件在重量、可靠性以及电磁兼容性等指标上进行综合比较分析,进而展现SSPC在当前航电任务配电系统中的优异性能.
以現代多電飛機對新型配電繫統的迫切需求為牽引,以新型配電繫統覈心部件新型執行器件固態功率控製器的應用為手段,繫統地闡述瞭新型執行器件固態功率控製器的設計原理以及電路設計方法.實驗通過某型號任務對加電控製單元的要求,利用SSPC加以實現,併與常規器件在重量、可靠性以及電磁兼容性等指標上進行綜閤比較分析,進而展現SSPC在噹前航電任務配電繫統中的優異性能.
이현대다전비궤대신형배전계통적박절수구위견인,이신형배전계통핵심부건신형집행기건고태공솔공제기적응용위수단,계통지천술료신형집행기건고태공솔공제기적설계원리이급전로설계방법.실험통과모형호임무대가전공제단원적요구,이용SSPC가이실현,병여상규기건재중량、가고성이급전자겸용성등지표상진행종합비교분석,진이전현SSPC재당전항전임무배전계통중적우이성능.
This paper systematically describes the design principles and circuit design of new solid-state power controller to perform a device by taking taking the more urgent demand of modern electric aircraft for new power distribution system as traction and with the means of the application of solid-state power controller (SSPC) of new performance device of core component of new distribution system as means. proves excellent performance of SSPC in the current avionics distribution system, In the experiment, the requirements of a certain task for power control unit are satisfied, SSPC is used for implementation and compared with conventional device in terms of weight, reliability, electromagnetic compatibility, etc.. The experiment results show that SSPC has excellent performance in current avionics mission power distribution system.
