|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B60L-001/00 B60L-003/00 H02G-003/00|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 7|
The present example provides aircraft integrated aircraft utility management and power distribution systems. Included are three exemplary implementations of aircraft power management systems (a DC power distribution system, a utility management system, and a combined system) that may utilize the like architecture, technologies, and components advantageously. A DC power distribution system can include two parts: primary DC power distribution and secondary DC power distribution systems. The utility management system integrates aircraft sub functions and ut...
1. An aircraft utilities and DC power distribution system comprising: a primary power distribution unit coupled between a plurality of sources and two power feeders; anda secondary power distribution unit coupled to the primary power distribution unit through both of the two power feeders, and including: a power module;an I/O module; anda computing modulewhereby DC power from the plurality of sources may be applied to a plurality of aircraft power loads through the primary power distribution unit and the secondary power distribution unit. 2. The aircraft...