SYSTEME ELECTRIQUE A REFROIDISSEMENT PAR FLUIDE CALOPORTEUR, AERONEF COMPORTANT UN TEL SYSTEME ET PROCEDE DE FABRICATION D'UN TEL SYSTEME

Le système électrique (100) comporte : - un module électrique de puissance (102) comportant un radiateur (112) muni de saillies (114) de dissipation thermique ; et - une plaque froide (120) d'une boîte à fluide caloporteur (118), présentant des cavités (126) complémentaires des saillies (114) p...

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Hauptverfasser:	GAUTIER,, Cyrille, MARTINEAU,, Donatien Henri Edouard, YOUSSEF,, Toni, NEHME,, Samir
Format:	Patent
Sprache:	fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS BLASTING CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COOLING OF INTERNAL-COMBUSTION ENGINES COOLING OF MACHINES OR ENGINES IN GENERAL COSMONAUTICS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY STEAM ENGINES TRANSPORTING WEAPONS
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creator	GAUTIER,, Cyrille MARTINEAU,, Donatien Henri Edouard YOUSSEF,, Toni NEHME,, Samir
description	Le système électrique (100) comporte : - un module électrique de puissance (102) comportant un radiateur (112) muni de saillies (114) de dissipation thermique ; et - une plaque froide (120) d'une boîte à fluide caloporteur (118), présentant des cavités (126) complémentaires des saillies (114) pour recevoir ces dernières. Figure pour l'abrégé : Fig. 1 An electrical system includes an electrical power module with a heat sink provided with heat-dissipating projections. The system further includes a cold plate of a heat-transfer fluid box. The cold plate has cavities which are complementary to the projections so as to receive said projections. Liquid metal is inserted between the heat sink and the cold plate, at least between the projections and the cavities.
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Figure pour l'abrégé : Fig. 1 An electrical system includes an electrical power module with a heat sink provided with heat-dissipating projections. The system further includes a cold plate of a heat-transfer fluid box. The cold plate has cavities which are complementary to the projections so as to receive said projections. Liquid metal is inserted between the heat sink and the cold plate, at least between the projections and the cavities.</description><language>fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BASIC ELECTRIC ELEMENTS ; BLASTING ; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COOLING OF INTERNAL-COMBUSTION ENGINES ; COOLING OF MACHINES OR ENGINES IN GENERAL ; COSMONAUTICS ; ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ; ELECTRICITY ; ENGINE PLANTS IN GENERAL ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; PRINTED CIRCUITS ; PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2023</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=20230512&DB=EPODOC&CC=FR&NR=3128941A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230512&DB=EPODOC&CC=FR&NR=3128941A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GAUTIER,, Cyrille</creatorcontrib><creatorcontrib>MARTINEAU,, Donatien Henri Edouard</creatorcontrib><creatorcontrib>YOUSSEF,, Toni</creatorcontrib><creatorcontrib>NEHME,, Samir</creatorcontrib><title>SYSTEME ELECTRIQUE A REFROIDISSEMENT PAR FLUIDE CALOPORTEUR, AERONEF COMPORTANT UN TEL SYSTEME ET PROCEDE DE FABRICATION D'UN TEL SYSTEME</title><description>Le système électrique (100) comporte : - un module électrique de puissance (102) comportant un radiateur (112) muni de saillies (114) de dissipation thermique ; et - une plaque froide (120) d'une boîte à fluide caloporteur (118), présentant des cavités (126) complémentaires des saillies (114) pour recevoir ces dernières. Figure pour l'abrégé : Fig. 1 An electrical system includes an electrical power module with a heat sink provided with heat-dissipating projections. The system further includes a cold plate of a heat-transfer fluid box. The cold plate has cavities which are complementary to the projections so as to receive said projections. Liquid metal is inserted between the heat sink and the cold plate, at least between the projections and the cavities.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>BLASTING</subject><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COOLING OF INTERNAL-COMBUSTION ENGINES</subject><subject>COOLING OF MACHINES OR ENGINES IN GENERAL</subject><subject>COSMONAUTICS</subject><subject>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</subject><subject>ELECTRICITY</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PRINTED CIRCUITS</subject><subject>PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjLEKAjEQRK-xEPUftrPR4jwLLdfcBgO5RDebwuo4JFaiB-dP-NdGEMFOGBiYeTPj4hlOQaghIEtK2BwjAQKTZm9qE0KunMABGbSNpiZQaP3Bs1DkBSCxd6RB-eadYUajAyEL39s8Zq8oL7M07tgoFOMd1PNfdFqMLt11SLOPTwrQJGq_TP29TUPfndMtPVrNVbnabNclltUfyAtCZj5b</recordid><startdate>20230512</startdate><enddate>20230512</enddate><creator>GAUTIER,, Cyrille</creator><creator>MARTINEAU,, Donatien Henri Edouard</creator><creator>YOUSSEF,, Toni</creator><creator>NEHME,, Samir</creator><scope>EVB</scope></search><sort><creationdate>20230512</creationdate><title>SYSTEME ELECTRIQUE A REFROIDISSEMENT PAR FLUIDE CALOPORTEUR, AERONEF COMPORTANT UN TEL SYSTEME ET PROCEDE DE FABRICATION D'UN TEL SYSTEME</title><author>GAUTIER,, Cyrille ; MARTINEAU,, Donatien Henri Edouard ; YOUSSEF,, Toni ; NEHME,, Samir</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR3128941A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2023</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>BLASTING</topic><topic>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COOLING OF INTERNAL-COMBUSTION ENGINES</topic><topic>COOLING OF MACHINES OR ENGINES IN GENERAL</topic><topic>COSMONAUTICS</topic><topic>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</topic><topic>ELECTRICITY</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PRINTED CIRCUITS</topic><topic>PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GAUTIER,, Cyrille</creatorcontrib><creatorcontrib>MARTINEAU,, Donatien Henri Edouard</creatorcontrib><creatorcontrib>YOUSSEF,, Toni</creatorcontrib><creatorcontrib>NEHME,, Samir</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GAUTIER,, Cyrille</au><au>MARTINEAU,, Donatien Henri Edouard</au><au>YOUSSEF,, Toni</au><au>NEHME,, Samir</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEME ELECTRIQUE A REFROIDISSEMENT PAR FLUIDE CALOPORTEUR, AERONEF COMPORTANT UN TEL SYSTEME ET PROCEDE DE FABRICATION D'UN TEL SYSTEME</title><date>2023-05-12</date><risdate>2023</risdate><abstract>Le système électrique (100) comporte : - un module électrique de puissance (102) comportant un radiateur (112) muni de saillies (114) de dissipation thermique ; et - une plaque froide (120) d'une boîte à fluide caloporteur (118), présentant des cavités (126) complémentaires des saillies (114) pour recevoir ces dernières. Figure pour l'abrégé : Fig. 1 An electrical system includes an electrical power module with a heat sink provided with heat-dissipating projections. The system further includes a cold plate of a heat-transfer fluid box. The cold plate has cavities which are complementary to the projections so as to receive said projections. Liquid metal is inserted between the heat sink and the cold plate, at least between the projections and the cavities.</abstract><oa>free_for_read</oa></addata></record>
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subjects	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS BLASTING CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COOLING OF INTERNAL-COMBUSTION ENGINES COOLING OF MACHINES OR ENGINES IN GENERAL COSMONAUTICS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY STEAM ENGINES TRANSPORTING WEAPONS
title	SYSTEME ELECTRIQUE A REFROIDISSEMENT PAR FLUIDE CALOPORTEUR, AERONEF COMPORTANT UN TEL SYSTEME ET PROCEDE DE FABRICATION D'UN TEL SYSTEME
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