AIRCRAFT WITH A BATTERY COOLING SYSTEM
The invention relates to a device for cooling a component (2) in a vehicle by means of a cooling air flow (4), wherein the device has at least one air inlet (11) and at least one air outlet (12), which are arranged such that the cooling air flow (4) is adjusted from the air inlet (11) to the air out...
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| creator | WETZEL, Wolfgang |
| description | The invention relates to a device for cooling a component (2) in a vehicle by means of a cooling air flow (4), wherein the device has at least one air inlet (11) and at least one air outlet (12), which are arranged such that the cooling air flow (4) is adjusted from the air inlet (11) to the air outlet (12) as a result of a difference in pressure produced during movement of the vehicle as a result of varying high flow velocities of the ambient air. The invention also relates to a method for cooling a component (2) in a vehicle by means of an above-named device. |
| format | Patent |
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The invention also relates to a method for cooling a component (2) in a vehicle by means of an above-named device.</description><language>eng ; hun</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2017</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=20170428&DB=EPODOC&CC=HU&NR=E030310T2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170428&DB=EPODOC&CC=HU&NR=E030310T2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WETZEL, Wolfgang</creatorcontrib><title>AIRCRAFT WITH A BATTERY COOLING SYSTEM</title><description>The invention relates to a device for cooling a component (2) in a vehicle by means of a cooling air flow (4), wherein the device has at least one air inlet (11) and at least one air outlet (12), which are arranged such that the cooling air flow (4) is adjusted from the air inlet (11) to the air outlet (12) as a result of a difference in pressure produced during movement of the vehicle as a result of varying high flow velocities of the ambient air. The invention also relates to a method for cooling a component (2) in a vehicle by means of an above-named device.</description><subject>AEROPLANES</subject><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>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBz9AxyDnJ0C1EI9wzxUHBUcHIMCXENilRw9vf38fRzVwiODA5x9eVhYE1LzClO5YXS3AyKbq4hzh66qQX58anFBYnJqXmpJfEeoa4GxgbGhgYhIUbGxKgBAMhSJAM</recordid><startdate>20170428</startdate><enddate>20170428</enddate><creator>WETZEL, Wolfgang</creator><scope>EVB</scope></search><sort><creationdate>20170428</creationdate><title>AIRCRAFT WITH A BATTERY COOLING SYSTEM</title><author>WETZEL, Wolfgang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_HUE030310TT23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; hun</language><creationdate>2017</creationdate><topic>AEROPLANES</topic><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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>WETZEL, Wolfgang</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WETZEL, Wolfgang</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT WITH A BATTERY COOLING SYSTEM</title><date>2017-04-28</date><risdate>2017</risdate><abstract>The invention relates to a device for cooling a component (2) in a vehicle by means of a cooling air flow (4), wherein the device has at least one air inlet (11) and at least one air outlet (12), which are arranged such that the cooling air flow (4) is adjusted from the air inlet (11) to the air outlet (12) as a result of a difference in pressure produced during movement of the vehicle as a result of varying high flow velocities of the ambient air. The invention also relates to a method for cooling a component (2) in a vehicle by means of an above-named device.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; hun |
| recordid | cdi_epo_espacenet_HUE030310TT2 |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | AIRCRAFT WITH A BATTERY COOLING SYSTEM |
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