Electric Power Supply Device And Flying Machine Using The Electric Power Supply Device
An electric power supply apparatus includes a first power supply unit, a second power supply unit, diodes, detection units, and an electric power control unit. The first power supply unit and the second power supply unit supply electric power to a thruster which is a load. The diodes are provided in...
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| creator | YOSHIKAWA, Satoru MITSUDA, Tetsuji ANDOU, Shinji |
| description | An electric power supply apparatus includes a first power supply unit, a second power supply unit, diodes, detection units, and an electric power control unit. The first power supply unit and the second power supply unit supply electric power to a thruster which is a load. The diodes are provided in the first power supply unit and the second power supply unit, respectively, to restrict reverse flow of currents to the power supply units. The detection units are provided between the first power supply unit and the thruster and between the second power supply unit and the thruster, respectively, to detect at least one of a voltage and a current. The electric power control unit controls electric power transmission between the first power supply unit and the second power supply unit based on detection values of the detection units. |
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The first power supply unit and the second power supply unit supply electric power to a thruster which is a load. The diodes are provided in the first power supply unit and the second power supply unit, respectively, to restrict reverse flow of currents to the power supply units. The detection units are provided between the first power supply unit and the thruster and between the second power supply unit and the thruster, respectively, to detect at least one of a voltage and a current. The electric power control unit controls electric power transmission between the first power supply unit and the second power supply unit based on detection values of the detection units.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER ; CONTROLLING ; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ; COSMONAUTICS ; ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ; ELECTRICITY ; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL ; GENERATION ; HELICOPTERS ; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; SYSTEMS FOR STORING ELECTRIC ENERGY ; TRANSPORTING ; VEHICLES IN GENERAL</subject><creationdate>2019</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190926&DB=EPODOC&CC=US&NR=2019291599A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190926&DB=EPODOC&CC=US&NR=2019291599A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YOSHIKAWA, Satoru</creatorcontrib><creatorcontrib>MITSUDA, Tetsuji</creatorcontrib><creatorcontrib>ANDOU, Shinji</creatorcontrib><title>Electric Power Supply Device And Flying Machine Using The Electric Power Supply Device</title><description>An electric power supply apparatus includes a first power supply unit, a second power supply unit, diodes, detection units, and an electric power control unit. The first power supply unit and the second power supply unit supply electric power to a thruster which is a load. The diodes are provided in the first power supply unit and the second power supply unit, respectively, to restrict reverse flow of currents to the power supply units. The detection units are provided between the first power supply unit and the thruster and between the second power supply unit and the thruster, respectively, to detect at least one of a voltage and a current. 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The first power supply unit and the second power supply unit supply electric power to a thruster which is a load. The diodes are provided in the first power supply unit and the second power supply unit, respectively, to restrict reverse flow of currents to the power supply units. The detection units are provided between the first power supply unit and the thruster and between the second power supply unit and the thruster, respectively, to detect at least one of a voltage and a current. The electric power control unit controls electric power transmission between the first power supply unit and the second power supply unit based on detection values of the detection units.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONTROLLING CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL GENERATION HELICOPTERS MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING VEHICLES IN GENERAL |
| title | Electric Power Supply Device And Flying Machine Using The Electric Power Supply Device |
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