|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||H02J-003/14 H02J-003/12 B64D-041/00 B64C-019/00|
|미국특허분류(USC)||307/032; 244/058; 244/075.1|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 7 인용 특허 : 14|
An Auxiliary Power System includes an APU controller and an aircraft load controller which include an APU load capacity algorithm which provides an uncomplicated and robust method of APU load control. The APU load capacity algorithm defines three load zones: a continuous APU load capacity zone (zone A); a time controlled zone (zone B); and a fault zone (zone C). Each zone is related to altitude to the service ceiling of the APU to provides consistent APU load capacity that addresses APU performance variation and deterioration effects to an end of the APU...
What is claimed is: 1. A power distribution system for an aircraft comprising: a gas turbine engine; a controller in communication with said gas turbine engine; and an aircraft load controller in communication with said gas turbine engine controller and a multitude of loads, one of said gas turbine engine controller and said aircraft load controller including an instruction set with a power source load capacity algorithm operable to selectively shed one or more of said loads, said power source load capacity algorithm defines a multitude of zones, said m...