Aircraft signal computer system having a plurality of modular signal computer units

Aircraft signal computer system having a plurality of modular signal computer units

The present invention relates to an aircraft signal computer system (10) comprising a plurality of modular signal computer units (12) and a liquid cooling device for cooling the modular signal computer units (12), wherein the liquid cooling device comprises a coolant line (16), which can be connecte...

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1. Verfasser: ROERING SEBASTIAN
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Sprache:chi ; eng
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CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS
ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
ELECTRICITY
MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
PRINTED CIRCUITS
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creator ROERING SEBASTIAN
description The present invention relates to an aircraft signal computer system (10) comprising a plurality of modular signal computer units (12) and a liquid cooling device for cooling the modular signal computer units (12), wherein the liquid cooling device comprises a coolant line (16), which can be connected to a central liquid cooling system of an aircraft in order to feed a liquid coolant medium at a desired low temperature to the liquid cooling device, and wherein the coolant line (16) of the liquid cooling device is in thermal surface contact with the modular signal computer units (12) in order to dissipate heat from the modular signal computer units (12).
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eng</language><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ; ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ; ELECTRICITY ; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS ; PRINTED CIRCUITS</subject><creationdate>2011</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=20110727&amp;DB=EPODOC&amp;CC=CN&amp;NR=102138374A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20110727&amp;DB=EPODOC&amp;CC=CN&amp;NR=102138374A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROERING SEBASTIAN</creatorcontrib><title>Aircraft signal computer system having a plurality of modular signal computer units</title><description>The present invention relates to an aircraft signal computer system (10) comprising a plurality of modular signal computer units (12) and a liquid cooling device for cooling the modular signal computer units (12), wherein the liquid cooling device comprises a coolant line (16), which can be connected to a central liquid cooling system of an aircraft in order to feed a liquid coolant medium at a desired low temperature to the liquid cooling device, and wherein the coolant line (16) of the liquid cooling device is in thermal surface contact with the modular signal computer units (12) in order to dissipate heat from the modular signal computer units (12).</description><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</subject><subject>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</subject><subject>ELECTRICITY</subject><subject>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</subject><subject>PRINTED CIRCUITS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAh2zCxKLkpMK1EozkzPS8xRSM7PLSgtSS1SKK4sLknNVchILMvMS1dIVCjIKS1KzMksqVTIT1PIzU8pzUkswtBUmpdZUszDwJqWmFOcyguluRkU3VxDnD10Uwvy41OLCxKTU_NSS-Kd_QwNjAyNLYzNTRyNiVEDAJ9MOP8</recordid><startdate>20110727</startdate><enddate>20110727</enddate><creator>ROERING SEBASTIAN</creator><scope>EVB</scope></search><sort><creationdate>20110727</creationdate><title>Aircraft signal computer system having a plurality of modular signal computer units</title><author>ROERING SEBASTIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN102138374A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2011</creationdate><topic>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</topic><topic>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</topic><topic>ELECTRICITY</topic><topic>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</topic><topic>PRINTED CIRCUITS</topic><toplevel>online_resources</toplevel><creatorcontrib>ROERING SEBASTIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROERING SEBASTIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft signal computer system having a plurality of modular signal computer units</title><date>2011-07-27</date><risdate>2011</risdate><abstract>The present invention relates to an aircraft signal computer system (10) comprising a plurality of modular signal computer units (12) and a liquid cooling device for cooling the modular signal computer units (12), wherein the liquid cooling device comprises a coolant line (16), which can be connected to a central liquid cooling system of an aircraft in order to feed a liquid coolant medium at a desired low temperature to the liquid cooling device, and wherein the coolant line (16) of the liquid cooling device is in thermal surface contact with the modular signal computer units (12) in order to dissipate heat from the modular signal computer units (12).</abstract><oa>free_for_read</oa></addata></record>
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subjects CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS
ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
ELECTRICITY
MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
PRINTED CIRCUITS
title Aircraft signal computer system having a plurality of modular signal computer units
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