Power system and flying device
The embodiment of the invention discloses a power system and a flying device. The system comprises M battery packs, M flying driving module groups, M busbars and a traveling driving module group; the M busbars are sequentially connected in series, and a first protection unit is arranged between ever...
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| creator | LIANG HUI ZHAO DELI TAN WEI HOU CONG HUANG BAOXIAN |
| description | The embodiment of the invention discloses a power system and a flying device. The system comprises M battery packs, M flying driving module groups, M busbars and a traveling driving module group; the M busbars are sequentially connected in series, and a first protection unit is arranged between every two adjacent busbars; the first protection unit is used for being in a conducting state when the connected busbars are not short-circuited, so that the M battery packs connected in parallel jointly supply power to the M flying driving module groups or the travel driving module group through the connected busbars; and the first protection unit is also used for being in a fusing state when the connected busbars are short-circuited, so that the battery packs connected with other busbars and the flying driving module groups or the traveling driving module group connected with other busbars can normally operate. By adopting the power system, the control strategy is simple, and the utilization rate of the battery packs |
| format | Patent |
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The system comprises M battery packs, M flying driving module groups, M busbars and a traveling driving module group; the M busbars are sequentially connected in series, and a first protection unit is arranged between every two adjacent busbars; the first protection unit is used for being in a conducting state when the connected busbars are not short-circuited, so that the M battery packs connected in parallel jointly supply power to the M flying driving module groups or the travel driving module group through the connected busbars; and the first protection unit is also used for being in a fusing state when the connected busbars are short-circuited, so that the battery packs connected with other busbars and the flying driving module groups or the traveling driving module group connected with other busbars can normally operate. By adopting the power system, the control strategy is simple, and the utilization rate of the battery packs</description><language>chi ; eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BASIC ELECTRIC ELEMENTS ; COSMONAUTICS ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY ; TRANSPORTING</subject><creationdate>2022</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=20220128&DB=EPODOC&CC=CN&NR=113991263A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220128&DB=EPODOC&CC=CN&NR=113991263A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LIANG HUI</creatorcontrib><creatorcontrib>ZHAO DELI</creatorcontrib><creatorcontrib>TAN WEI</creatorcontrib><creatorcontrib>HOU CONG</creatorcontrib><creatorcontrib>HUANG BAOXIAN</creatorcontrib><title>Power system and flying device</title><description>The embodiment of the invention discloses a power system and a flying device. The system comprises M battery packs, M flying driving module groups, M busbars and a traveling driving module group; the M busbars are sequentially connected in series, and a first protection unit is arranged between every two adjacent busbars; the first protection unit is used for being in a conducting state when the connected busbars are not short-circuited, so that the M battery packs connected in parallel jointly supply power to the M flying driving module groups or the travel driving module group through the connected busbars; and the first protection unit is also used for being in a fusing state when the connected busbars are short-circuited, so that the battery packs connected with other busbars and the flying driving module groups or the traveling driving module group connected with other busbars can normally operate. By adopting the power system, the control strategy is simple, and the utilization rate of the battery packs</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>COSMONAUTICS</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJALyC9PLVIoriwuSc1VSMxLUUjLqczMS1dISS3LTE7lYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhsaWloZGZsaOxsSoAQDvfSRp</recordid><startdate>20220128</startdate><enddate>20220128</enddate><creator>LIANG HUI</creator><creator>ZHAO DELI</creator><creator>TAN WEI</creator><creator>HOU CONG</creator><creator>HUANG BAOXIAN</creator><scope>EVB</scope></search><sort><creationdate>20220128</creationdate><title>Power system and flying device</title><author>LIANG HUI ; ZHAO DELI ; TAN WEI ; HOU CONG ; HUANG BAOXIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN113991263A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>COSMONAUTICS</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LIANG HUI</creatorcontrib><creatorcontrib>ZHAO DELI</creatorcontrib><creatorcontrib>TAN WEI</creatorcontrib><creatorcontrib>HOU CONG</creatorcontrib><creatorcontrib>HUANG BAOXIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LIANG HUI</au><au>ZHAO DELI</au><au>TAN WEI</au><au>HOU CONG</au><au>HUANG BAOXIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Power system and flying device</title><date>2022-01-28</date><risdate>2022</risdate><abstract>The embodiment of the invention discloses a power system and a flying device. The system comprises M battery packs, M flying driving module groups, M busbars and a traveling driving module group; the M busbars are sequentially connected in series, and a first protection unit is arranged between every two adjacent busbars; the first protection unit is used for being in a conducting state when the connected busbars are not short-circuited, so that the M battery packs connected in parallel jointly supply power to the M flying driving module groups or the travel driving module group through the connected busbars; and the first protection unit is also used for being in a fusing state when the connected busbars are short-circuited, so that the battery packs connected with other busbars and the flying driving module groups or the traveling driving module group connected with other busbars can normally operate. By adopting the power system, the control strategy is simple, and the utilization rate of the battery packs</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY TRANSPORTING |
| title | Power system and flying device |
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