Aircraft battery systems

Aircraft battery systems

An aircraft 10 comprising a battery pack 20 having a plurality of battery cells 200 is provided. Each of the plurality of battery cells 200 is arranged to vent into a venting region 230, 235a, 235b of the battery pack 20. A path 21, 210, 213, 232, 235a, 235b is defined between the venting region 230...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Michael Zagrodnik, István Örökös-Tóth, Vidor Veres-Szekely, Anand Prabhu Mathivanan, Krishnamoorthi Sivalingam, Satyanarayana Reddy Gajjela, Daniel Lorincz
Format: Patent
Sprache:eng
Schlagworte:
BASIC ELECTRIC ELEMENTS
ELECTRICITY
PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Michael Zagrodnik
István Örökös-Tóth
Vidor Veres-Szekely
Anand Prabhu Mathivanan
Krishnamoorthi Sivalingam
Satyanarayana Reddy Gajjela
Daniel Lorincz
description An aircraft 10 comprising a battery pack 20 having a plurality of battery cells 200 is provided. Each of the plurality of battery cells 200 is arranged to vent into a venting region 230, 235a, 235b of the battery pack 20. A path 21, 210, 213, 232, 235a, 235b is defined between the venting region 230, 235a, 235b and an exterior of the aircraft 10, whereby thermal products vented by the cells 200 can exit the aircraft 10 via the path 21, 210, 213, 232, 235a, 235b. In some embodiments, the venting region 230, 235a, 235b is or is in fluid communication with an air channel 21, 210, 213, 235a, 235b through which air flows from an aircraft air inlet 16 to an aircraft air outlet 17. In other embodiments, the path joins the venting region 230 and an opening in an external surface of the aircraft 10.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_GB2607926B</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>GB2607926B</sourcerecordid><originalsourceid>FETCH-epo_espacenet_GB2607926B3</originalsourceid><addsrcrecordid>eNrjZJBwzCxKLkpMK1FISiwpSS2qVCiuLC5JzS3mYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXx7k5GZgbmlkZmTsaEVQAAhfghrA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft battery systems</title><source>esp@cenet</source><creator>Michael Zagrodnik ; István Örökös-Tóth ; Vidor Veres-Szekely ; Anand Prabhu Mathivanan ; Krishnamoorthi Sivalingam ; Satyanarayana Reddy Gajjela ; Daniel Lorincz</creator><creatorcontrib>Michael Zagrodnik ; István Örökös-Tóth ; Vidor Veres-Szekely ; Anand Prabhu Mathivanan ; Krishnamoorthi Sivalingam ; Satyanarayana Reddy Gajjela ; Daniel Lorincz</creatorcontrib><description>An aircraft 10 comprising a battery pack 20 having a plurality of battery cells 200 is provided. Each of the plurality of battery cells 200 is arranged to vent into a venting region 230, 235a, 235b of the battery pack 20. A path 21, 210, 213, 232, 235a, 235b is defined between the venting region 230, 235a, 235b and an exterior of the aircraft 10, whereby thermal products vented by the cells 200 can exit the aircraft 10 via the path 21, 210, 213, 232, 235a, 235b. In some embodiments, the venting region 230, 235a, 235b is or is in fluid communication with an air channel 21, 210, 213, 235a, 235b through which air flows from an aircraft air inlet 16 to an aircraft air outlet 17. In other embodiments, the path joins the venting region 230 and an opening in an external surface of the aircraft 10.</description><language>eng</language><subject>BASIC ELECTRIC ELEMENTS ; ELECTRICITY ; PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</subject><creationdate>2024</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&amp;date=20240403&amp;DB=EPODOC&amp;CC=GB&amp;NR=2607926B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240403&amp;DB=EPODOC&amp;CC=GB&amp;NR=2607926B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Michael Zagrodnik</creatorcontrib><creatorcontrib>István Örökös-Tóth</creatorcontrib><creatorcontrib>Vidor Veres-Szekely</creatorcontrib><creatorcontrib>Anand Prabhu Mathivanan</creatorcontrib><creatorcontrib>Krishnamoorthi Sivalingam</creatorcontrib><creatorcontrib>Satyanarayana Reddy Gajjela</creatorcontrib><creatorcontrib>Daniel Lorincz</creatorcontrib><title>Aircraft battery systems</title><description>An aircraft 10 comprising a battery pack 20 having a plurality of battery cells 200 is provided. Each of the plurality of battery cells 200 is arranged to vent into a venting region 230, 235a, 235b of the battery pack 20. A path 21, 210, 213, 232, 235a, 235b is defined between the venting region 230, 235a, 235b and an exterior of the aircraft 10, whereby thermal products vented by the cells 200 can exit the aircraft 10 via the path 21, 210, 213, 232, 235a, 235b. In some embodiments, the venting region 230, 235a, 235b is or is in fluid communication with an air channel 21, 210, 213, 235a, 235b through which air flows from an aircraft air inlet 16 to an aircraft air outlet 17. In other embodiments, the path joins the venting region 230 and an opening in an external surface of the aircraft 10.</description><subject>BASIC ELECTRIC ELEMENTS</subject><subject>ELECTRICITY</subject><subject>PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBwzCxKLkpMK1FISiwpSS2qVCiuLC5JzS3mYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXx7k5GZgbmlkZmTsaEVQAAhfghrA</recordid><startdate>20240403</startdate><enddate>20240403</enddate><creator>Michael Zagrodnik</creator><creator>István Örökös-Tóth</creator><creator>Vidor Veres-Szekely</creator><creator>Anand Prabhu Mathivanan</creator><creator>Krishnamoorthi Sivalingam</creator><creator>Satyanarayana Reddy Gajjela</creator><creator>Daniel Lorincz</creator><scope>EVB</scope></search><sort><creationdate>20240403</creationdate><title>Aircraft battery systems</title><author>Michael Zagrodnik ; István Örökös-Tóth ; Vidor Veres-Szekely ; Anand Prabhu Mathivanan ; Krishnamoorthi Sivalingam ; Satyanarayana Reddy Gajjela ; Daniel Lorincz</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2607926B3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2024</creationdate><topic>BASIC ELECTRIC ELEMENTS</topic><topic>ELECTRICITY</topic><topic>PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</topic><toplevel>online_resources</toplevel><creatorcontrib>Michael Zagrodnik</creatorcontrib><creatorcontrib>István Örökös-Tóth</creatorcontrib><creatorcontrib>Vidor Veres-Szekely</creatorcontrib><creatorcontrib>Anand Prabhu Mathivanan</creatorcontrib><creatorcontrib>Krishnamoorthi Sivalingam</creatorcontrib><creatorcontrib>Satyanarayana Reddy Gajjela</creatorcontrib><creatorcontrib>Daniel Lorincz</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Michael Zagrodnik</au><au>István Örökös-Tóth</au><au>Vidor Veres-Szekely</au><au>Anand Prabhu Mathivanan</au><au>Krishnamoorthi Sivalingam</au><au>Satyanarayana Reddy Gajjela</au><au>Daniel Lorincz</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft battery systems</title><date>2024-04-03</date><risdate>2024</risdate><abstract>An aircraft 10 comprising a battery pack 20 having a plurality of battery cells 200 is provided. Each of the plurality of battery cells 200 is arranged to vent into a venting region 230, 235a, 235b of the battery pack 20. A path 21, 210, 213, 232, 235a, 235b is defined between the venting region 230, 235a, 235b and an exterior of the aircraft 10, whereby thermal products vented by the cells 200 can exit the aircraft 10 via the path 21, 210, 213, 232, 235a, 235b. In some embodiments, the venting region 230, 235a, 235b is or is in fluid communication with an air channel 21, 210, 213, 235a, 235b through which air flows from an aircraft air inlet 16 to an aircraft air outlet 17. In other embodiments, the path joins the venting region 230 and an opening in an external surface of the aircraft 10.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_GB2607926B
source esp@cenet
subjects BASIC ELECTRIC ELEMENTS
ELECTRICITY
PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY
title Aircraft battery systems
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-23T05%3A27%3A10IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Michael%20Zagrodnik&rft.date=2024-04-03&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EGB2607926B%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true