|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||322/022 ; 307/019|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 41 인용 특허 : 17|
A power conversion system allows for redundant starting and generating functions together with fault tolerant operation through the multiple use of power conversion equipment.
[ What is claimed is:] [12.] A power conversion system for an aircraft, comprising:first and second aircraft engines;an auxiliary power unit (APU);first and second pairs of generators coupled to the first and second aircraft engines, respectively, and a third pair of generators coupled to the APU;a first load bus coupled to an electrically driven hydraulic pump;a second, variable frequency bus;a first switch matrix coupled to the generators;first through sixth power converter units coupled to the first switch matrix;a second switch matrix coupled between...