|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/058; 244/060; 244/0760R; 307/0091|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 47|
Systems and methods for operating aircraft power systems are disclosed. A power system in accordance with one embodiment of the invention includes an aircraft auxiliary power unit and a controller coupled to the aircraft auxiliary power unit, with the controller being configured to automatically stop the auxiliary power unit while the auxiliary power unit is functioning normally. The controller can also be configured to automatically start the auxiliary power unit in-flight when power supplied or expected to be supplied to a subsystem of the aircraft has...
We claim: 1. An aircraft power system, comprising:at least one aircraft primary power source;an aircraft auxiliary power unit;an electrical power circuit coupled to the at least one aircraft primary power source and the aircraft auxiliary power unit;a detection system operatively coupled to the electrical power circuit to provide a first signal corresponding to a load on the electrical power circuit, and a second signal corresponding to the power supplied to the electrical power circuit; anda controller coupled to the detection system and the auxiliary p...