Structural battery for an aircraft vehicle

Structural battery for an aircraft vehicle

In one embodiment, systems and methods include using a battery (110) to provide electrical charge to a vehicle (100). The battery (110) comprises a first half of a housing (200) coupled comprising one or more air vents (206) and an anode (204) disposed at least partially within the first half of the...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ELLER, MICHAEL R, BREWER, ROGER A
Format: Patent
Sprache:chi ; 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 ELLER, MICHAEL R
BREWER, ROGER A
description In one embodiment, systems and methods include using a battery (110) to provide electrical charge to a vehicle (100). The battery (110) comprises a first half of a housing (200) coupled comprising one or more air vents (206) and an anode (204) disposed at least partially within the first half of the housing (200). The battery (110) further comprises a second half of the housing (200) comprising one or more air vents (206), wherein the anode (204) extends from the first half of the housing (200) and into the second half of the housing (200). The battery (110) further comprises a pair of cathodes (302) disposed within the second half of the housing (200), wherein the pair of cathodes (302) extends from the second half of the housing (200) and into the first half of the housing (200), wherein the anode (204) is disposed between the pair of cathodes (302), wherein there is a gap (212) between the anode (204) and each one of the pair of cathodes (302).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_TWI843155BB</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>TWI843155BB</sourcerecordid><originalsourceid>FETCH-epo_espacenet_TWI843155BB3</originalsourceid><addsrcrecordid>eNrjZNAKLikqTS4pLUrMUUhKLClJLapUSMsvUkjMU0jMLEouSkwrUShLzchMzknlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxIeGeFibGhqamTk7GRCgBAAIHKUU</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Structural battery for an aircraft vehicle</title><source>esp@cenet</source><creator>ELLER, MICHAEL R ; BREWER, ROGER A</creator><creatorcontrib>ELLER, MICHAEL R ; BREWER, ROGER A</creatorcontrib><description>In one embodiment, systems and methods include using a battery (110) to provide electrical charge to a vehicle (100). The battery (110) comprises a first half of a housing (200) coupled comprising one or more air vents (206) and an anode (204) disposed at least partially within the first half of the housing (200). The battery (110) further comprises a second half of the housing (200) comprising one or more air vents (206), wherein the anode (204) extends from the first half of the housing (200) and into the second half of the housing (200). The battery (110) further comprises a pair of cathodes (302) disposed within the second half of the housing (200), wherein the pair of cathodes (302) extends from the second half of the housing (200) and into the first half of the housing (200), wherein the anode (204) is disposed between the pair of cathodes (302), wherein there is a gap (212) between the anode (204) and each one of the pair of cathodes (302).</description><language>chi ; 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=20240521&amp;DB=EPODOC&amp;CC=TW&amp;NR=I843155B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240521&amp;DB=EPODOC&amp;CC=TW&amp;NR=I843155B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ELLER, MICHAEL R</creatorcontrib><creatorcontrib>BREWER, ROGER A</creatorcontrib><title>Structural battery for an aircraft vehicle</title><description>In one embodiment, systems and methods include using a battery (110) to provide electrical charge to a vehicle (100). The battery (110) comprises a first half of a housing (200) coupled comprising one or more air vents (206) and an anode (204) disposed at least partially within the first half of the housing (200). The battery (110) further comprises a second half of the housing (200) comprising one or more air vents (206), wherein the anode (204) extends from the first half of the housing (200) and into the second half of the housing (200). The battery (110) further comprises a pair of cathodes (302) disposed within the second half of the housing (200), wherein the pair of cathodes (302) extends from the second half of the housing (200) and into the first half of the housing (200), wherein the anode (204) is disposed between the pair of cathodes (302), wherein there is a gap (212) between the anode (204) and each one of the pair of cathodes (302).</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>eNrjZNAKLikqTS4pLUrMUUhKLClJLapUSMsvUkjMU0jMLEouSkwrUShLzchMzknlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxIeGeFibGhqamTk7GRCgBAAIHKUU</recordid><startdate>20240521</startdate><enddate>20240521</enddate><creator>ELLER, MICHAEL R</creator><creator>BREWER, ROGER A</creator><scope>EVB</scope></search><sort><creationdate>20240521</creationdate><title>Structural battery for an aircraft vehicle</title><author>ELLER, MICHAEL R ; BREWER, ROGER A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_TWI843155BB3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; 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>ELLER, MICHAEL R</creatorcontrib><creatorcontrib>BREWER, ROGER A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ELLER, MICHAEL R</au><au>BREWER, ROGER A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Structural battery for an aircraft vehicle</title><date>2024-05-21</date><risdate>2024</risdate><abstract>In one embodiment, systems and methods include using a battery (110) to provide electrical charge to a vehicle (100). The battery (110) comprises a first half of a housing (200) coupled comprising one or more air vents (206) and an anode (204) disposed at least partially within the first half of the housing (200). The battery (110) further comprises a second half of the housing (200) comprising one or more air vents (206), wherein the anode (204) extends from the first half of the housing (200) and into the second half of the housing (200). The battery (110) further comprises a pair of cathodes (302) disposed within the second half of the housing (200), wherein the pair of cathodes (302) extends from the second half of the housing (200) and into the first half of the housing (200), wherein the anode (204) is disposed between the pair of cathodes (302), wherein there is a gap (212) between the anode (204) and each one of the pair of cathodes (302).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_TWI843155BB
source esp@cenet
subjects BASIC ELECTRIC ELEMENTS
ELECTRICITY
PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY
title Structural battery for an aircraft vehicle
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-26T17%3A21%3A25IST&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=ELLER,%20MICHAEL%20R&rft.date=2024-05-21&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ETWI843155BB%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