PROBLEM TO BE SOLVED: To provide a distribution device capable of inhibiting abnormality from being generated by an excess current while being capable of utilizing electric power more sufficiently in an aircraft.SOLUTION: An electric power system 1 includes: a remote distribution board 5; an electric type actuator 15a to which electric power is supplied from the remote distribution board 5; and a relay 43. Regenerative electric power generated by the electric type actuator 15a is outputted to a capacitor 27.
【課題】航空機において電力をより効率的に利用することができながら、過大な電流により異常が生じることを抑制できる、配電装置を提供する。【解決手段】電力システム1は、遠隔配電盤5と、遠隔配電盤5から電力を供給される電気式アクチュエータ15aと、継電器43とを有している。電気式アクチュエータ15aで発生した回生電力は、蓄電器27に出力される。【選択図】図2
DISTRIBUTION DEVICE
配電装置
2015-06-18
Patent
Electronic Resource
Japanese
IPC: | H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern |
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