Aircraft system including dual power supply structure and method for controlling method thereof
The present invention relates to an aircraft system and, more specifically, to an aircraft system including a dual power supply structure. In the aircraft system including a dual power supply structure and a method for controlling the same according to the present invention, a high-voltage battery p...
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| creator | CHAE SANGHYUN PARK POOMIN CHOI INHO KIM DEOG KWAN |
| description | The present invention relates to an aircraft system and, more specifically, to an aircraft system including a dual power supply structure. In the aircraft system including a dual power supply structure and a method for controlling the same according to the present invention, a high-voltage battery provided to a motor or a motor controller and a low-voltage battery provided to a control module and communication equipment are provided separately, such that even if the voltage requirement of the motor increases, power can be efficiently supplied to the control module and the communication equipment. In addition, by allowing a control unit to control the power supply, when a problem occurs in any one battery, auxiliary power can be provided through a battery with no problem, thereby inducing safe landing of an aircraft.
본 발명은 항공기 시스템에 관한 것으로, 보다 상세하게는 이중 전력구조를 포함하는 항공기 시스템에 관한 것이다. 본 발명의 이중 전력공급구조를 포함하는 항공기 시스템 및 이를 제어하는 방법은 모터나 모터 제어기에 제공하는 고전압 배터리와, 제어모듈 및 통신장비에 제공하는 저전압 배터리를 분리하여 구비함으로써, 모터의 전압요구량이 증가하더라도 제어모듈 및 통신장비에 전력을 효율적으로 공급할 수 있고, 제어부가 전력 공급을 제어할 수 있도록 함으로써, 어느 하나의 배터리에 이상이 발생한 경우, 이상이 발생하지 않은 배터리를 통해 보조적으로 전력을 제공할 수 있도록 하여 안정적으로 항공기의 착륙을 유도할 수 있는 효과가 있다. |
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본 발명은 항공기 시스템에 관한 것으로, 보다 상세하게는 이중 전력구조를 포함하는 항공기 시스템에 관한 것이다. 본 발명의 이중 전력공급구조를 포함하는 항공기 시스템 및 이를 제어하는 방법은 모터나 모터 제어기에 제공하는 고전압 배터리와, 제어모듈 및 통신장비에 제공하는 저전압 배터리를 분리하여 구비함으로써, 모터의 전압요구량이 증가하더라도 제어모듈 및 통신장비에 전력을 효율적으로 공급할 수 있고, 제어부가 전력 공급을 제어할 수 있도록 함으로써, 어느 하나의 배터리에 이상이 발생한 경우, 이상이 발생하지 않은 배터리를 통해 보조적으로 전력을 제공할 수 있도록 하여 안정적으로 항공기의 착륙을 유도할 수 있는 효과가 있다.</description><language>eng ; kor</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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=20230510&DB=EPODOC&CC=KR&NR=20230064127A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230510&DB=EPODOC&CC=KR&NR=20230064127A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CHAE SANGHYUN</creatorcontrib><creatorcontrib>PARK POOMIN</creatorcontrib><creatorcontrib>CHOI INHO</creatorcontrib><creatorcontrib>KIM DEOG KWAN</creatorcontrib><title>Aircraft system including dual power supply structure and method for controlling method thereof</title><description>The present invention relates to an aircraft system and, more specifically, to an aircraft system including a dual power supply structure. In the aircraft system including a dual power supply structure and a method for controlling the same according to the present invention, a high-voltage battery provided to a motor or a motor controller and a low-voltage battery provided to a control module and communication equipment are provided separately, such that even if the voltage requirement of the motor increases, power can be efficiently supplied to the control module and the communication equipment. In addition, by allowing a control unit to control the power supply, when a problem occurs in any one battery, auxiliary power can be provided through a battery with no problem, thereby inducing safe landing of an aircraft.
본 발명은 항공기 시스템에 관한 것으로, 보다 상세하게는 이중 전력구조를 포함하는 항공기 시스템에 관한 것이다. 본 발명의 이중 전력공급구조를 포함하는 항공기 시스템 및 이를 제어하는 방법은 모터나 모터 제어기에 제공하는 고전압 배터리와, 제어모듈 및 통신장비에 제공하는 저전압 배터리를 분리하여 구비함으로써, 모터의 전압요구량이 증가하더라도 제어모듈 및 통신장비에 전력을 효율적으로 공급할 수 있고, 제어부가 전력 공급을 제어할 수 있도록 함으로써, 어느 하나의 배터리에 이상이 발생한 경우, 이상이 발생하지 않은 배터리를 통해 보조적으로 전력을 제공할 수 있도록 하여 안정적으로 항공기의 착륙을 유도할 수 있는 효과가 있다.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNi0EKwjAQAHvxIOofFjwLsRV7LqII3sR7CMnGBtJs2GyQ_l6EPsDTwDCzbvQQ2LLxAmUughOEZGN1Ib3BVRMh0wcZSs05zlCEq5XKCCY5mFBGcuCJwVISphh_26JlREby22blTSy4W7hp9rfr63I_YCaNJRuLCUU_nq1qO6XOp2PbD91_1Rfvvj6r</recordid><startdate>20230510</startdate><enddate>20230510</enddate><creator>CHAE SANGHYUN</creator><creator>PARK POOMIN</creator><creator>CHOI INHO</creator><creator>KIM DEOG KWAN</creator><scope>EVB</scope></search><sort><creationdate>20230510</creationdate><title>Aircraft system including dual power supply structure and method for controlling method thereof</title><author>CHAE SANGHYUN ; PARK POOMIN ; CHOI INHO ; KIM DEOG KWAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR20230064127A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>CHAE SANGHYUN</creatorcontrib><creatorcontrib>PARK POOMIN</creatorcontrib><creatorcontrib>CHOI INHO</creatorcontrib><creatorcontrib>KIM DEOG KWAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHAE SANGHYUN</au><au>PARK POOMIN</au><au>CHOI INHO</au><au>KIM DEOG KWAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft system including dual power supply structure and method for controlling method thereof</title><date>2023-05-10</date><risdate>2023</risdate><abstract>The present invention relates to an aircraft system and, more specifically, to an aircraft system including a dual power supply structure. In the aircraft system including a dual power supply structure and a method for controlling the same according to the present invention, a high-voltage battery provided to a motor or a motor controller and a low-voltage battery provided to a control module and communication equipment are provided separately, such that even if the voltage requirement of the motor increases, power can be efficiently supplied to the control module and the communication equipment. In addition, by allowing a control unit to control the power supply, when a problem occurs in any one battery, auxiliary power can be provided through a battery with no problem, thereby inducing safe landing of an aircraft.
본 발명은 항공기 시스템에 관한 것으로, 보다 상세하게는 이중 전력구조를 포함하는 항공기 시스템에 관한 것이다. 본 발명의 이중 전력공급구조를 포함하는 항공기 시스템 및 이를 제어하는 방법은 모터나 모터 제어기에 제공하는 고전압 배터리와, 제어모듈 및 통신장비에 제공하는 저전압 배터리를 분리하여 구비함으로써, 모터의 전압요구량이 증가하더라도 제어모듈 및 통신장비에 전력을 효율적으로 공급할 수 있고, 제어부가 전력 공급을 제어할 수 있도록 함으로써, 어느 하나의 배터리에 이상이 발생한 경우, 이상이 발생하지 않은 배터리를 통해 보조적으로 전력을 제공할 수 있도록 하여 안정적으로 항공기의 착륙을 유도할 수 있는 효과가 있다.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Aircraft system including dual power supply structure and method for controlling method thereof |
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