|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||307/064; 244/0070A; 290/0010C; 307/080|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 30 인용 특허 : 3|
A DC electrical power generation system for aircraft having primary and emergency generation systems is disclosed. The system includes a transmission driven power generator, a dedicated generator control unit and a distribution network for providing sufficient capacity to all electrical loads on the aircraft. The emergency power system includes at least one engine driven starter generators, with an associated controller unit and associated distribution network for providing sufficient backup capacity to electrical loads assigned thereto.
1. A redundant DC electrical power system for an aircraft having at least two rotors mechanically driven by a common main driveshaft, comprising:a primary power system including a power generator driven by said common main driveshaft, a dedicated generator control unit and an isolated distribution network that further includes electrical busses for providing sufficient capacity to electrical loads on the aircraft; and an emergency power system including at least one engine driven starter generator with an associated controller unit and associated distrib...