AIRCRAFT TAIL REGION WITH A COOLING SYSTEM INSTALLED IN SAID AIRCRAFT TAIL REGION

An aircraft tail region including a cooling system installed in the aircraft tail region. The cooling system comprises a cooler, which forms a section of an outer skin of the aircraft tail region, and includes coolant channels allowing a flow of ambient air therethrough, and extending from a first s...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: KRAUSE, UDO, WOLLRAB, UWE, MUELLER, CHRISTIAN, STEFES, BRUNO, STOLTE, RALF-HENNING, EILKEN, FLORIAN
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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 KRAUSE, UDO
WOLLRAB, UWE
MUELLER, CHRISTIAN
STEFES, BRUNO
STOLTE, RALF-HENNING
EILKEN, FLORIAN
description An aircraft tail region including a cooling system installed in the aircraft tail region. The cooling system comprises a cooler, which forms a section of an outer skin of the aircraft tail region, and includes coolant channels allowing a flow of ambient air therethrough, and extending from a first surface of the cooler to a second surface of the cooler. The cooling system also includes a fan system, which is adapted to convey ambient air through the coolant channels of the cooler at least in specified operating phases of the cooling system, and a first opening, which is formed in the outer skin of the aircraft tail region, and which allows, in conveying operation of the fan system, ambient air which is supplied through the coolant channels of the cooler into an interior of the aircraft tail region to be discharged back into the aircraft environment.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2688801A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2688801A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2688801A13</originalsourceid><addsrcrecordid>eNrjZAh09AxyDnJ0C1EIcfT0UQhydff091MI9wzxUHBUcPb39_H0c1cIjgwOcfVV8PQLDnH08XF1AbIUgh09XRSwaeZhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAUZmFhYWBoaOhsZEKAEAGwQumw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIRCRAFT TAIL REGION WITH A COOLING SYSTEM INSTALLED IN SAID AIRCRAFT TAIL REGION</title><source>esp@cenet</source><creator>KRAUSE, UDO ; WOLLRAB, UWE ; MUELLER, CHRISTIAN ; STEFES, BRUNO ; STOLTE, RALF-HENNING ; EILKEN, FLORIAN</creator><creatorcontrib>KRAUSE, UDO ; WOLLRAB, UWE ; MUELLER, CHRISTIAN ; STEFES, BRUNO ; STOLTE, RALF-HENNING ; EILKEN, FLORIAN</creatorcontrib><description>An aircraft tail region including a cooling system installed in the aircraft tail region. The cooling system comprises a cooler, which forms a section of an outer skin of the aircraft tail region, and includes coolant channels allowing a flow of ambient air therethrough, and extending from a first surface of the cooler to a second surface of the cooler. The cooling system also includes a fan system, which is adapted to convey ambient air through the coolant channels of the cooler at least in specified operating phases of the cooling system, and a first opening, which is formed in the outer skin of the aircraft tail region, and which allows, in conveying operation of the fan system, ambient air which is supplied through the coolant channels of the cooler into an interior of the aircraft tail region to be discharged back into the aircraft environment.</description><language>eng ; fre ; ger</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>2014</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=20140129&amp;DB=EPODOC&amp;CC=EP&amp;NR=2688801A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20140129&amp;DB=EPODOC&amp;CC=EP&amp;NR=2688801A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRAUSE, UDO</creatorcontrib><creatorcontrib>WOLLRAB, UWE</creatorcontrib><creatorcontrib>MUELLER, CHRISTIAN</creatorcontrib><creatorcontrib>STEFES, BRUNO</creatorcontrib><creatorcontrib>STOLTE, RALF-HENNING</creatorcontrib><creatorcontrib>EILKEN, FLORIAN</creatorcontrib><title>AIRCRAFT TAIL REGION WITH A COOLING SYSTEM INSTALLED IN SAID AIRCRAFT TAIL REGION</title><description>An aircraft tail region including a cooling system installed in the aircraft tail region. The cooling system comprises a cooler, which forms a section of an outer skin of the aircraft tail region, and includes coolant channels allowing a flow of ambient air therethrough, and extending from a first surface of the cooler to a second surface of the cooler. The cooling system also includes a fan system, which is adapted to convey ambient air through the coolant channels of the cooler at least in specified operating phases of the cooling system, and a first opening, which is formed in the outer skin of the aircraft tail region, and which allows, in conveying operation of the fan system, ambient air which is supplied through the coolant channels of the cooler into an interior of the aircraft tail region to be discharged back into the aircraft environment.</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>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAh09AxyDnJ0C1EIcfT0UQhydff091MI9wzxUHBUcPb39_H0c1cIjgwOcfVV8PQLDnH08XF1AbIUgh09XRSwaeZhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAUZmFhYWBoaOhsZEKAEAGwQumw</recordid><startdate>20140129</startdate><enddate>20140129</enddate><creator>KRAUSE, UDO</creator><creator>WOLLRAB, UWE</creator><creator>MUELLER, CHRISTIAN</creator><creator>STEFES, BRUNO</creator><creator>STOLTE, RALF-HENNING</creator><creator>EILKEN, FLORIAN</creator><scope>EVB</scope></search><sort><creationdate>20140129</creationdate><title>AIRCRAFT TAIL REGION WITH A COOLING SYSTEM INSTALLED IN SAID AIRCRAFT TAIL REGION</title><author>KRAUSE, UDO ; WOLLRAB, UWE ; MUELLER, CHRISTIAN ; STEFES, BRUNO ; STOLTE, RALF-HENNING ; EILKEN, FLORIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2688801A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2014</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>KRAUSE, UDO</creatorcontrib><creatorcontrib>WOLLRAB, UWE</creatorcontrib><creatorcontrib>MUELLER, CHRISTIAN</creatorcontrib><creatorcontrib>STEFES, BRUNO</creatorcontrib><creatorcontrib>STOLTE, RALF-HENNING</creatorcontrib><creatorcontrib>EILKEN, FLORIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRAUSE, UDO</au><au>WOLLRAB, UWE</au><au>MUELLER, CHRISTIAN</au><au>STEFES, BRUNO</au><au>STOLTE, RALF-HENNING</au><au>EILKEN, FLORIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT TAIL REGION WITH A COOLING SYSTEM INSTALLED IN SAID AIRCRAFT TAIL REGION</title><date>2014-01-29</date><risdate>2014</risdate><abstract>An aircraft tail region including a cooling system installed in the aircraft tail region. The cooling system comprises a cooler, which forms a section of an outer skin of the aircraft tail region, and includes coolant channels allowing a flow of ambient air therethrough, and extending from a first surface of the cooler to a second surface of the cooler. The cooling system also includes a fan system, which is adapted to convey ambient air through the coolant channels of the cooler at least in specified operating phases of the cooling system, and a first opening, which is formed in the outer skin of the aircraft tail region, and which allows, in conveying operation of the fan system, ambient air which is supplied through the coolant channels of the cooler into an interior of the aircraft tail region to be discharged back into the aircraft environment.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2688801A1
source esp@cenet
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 TAIL REGION WITH A COOLING SYSTEM INSTALLED IN SAID AIRCRAFT TAIL REGION
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T22%3A42%3A19IST&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=KRAUSE,%20UDO&rft.date=2014-01-29&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2688801A1%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