ELECTRICAL SYSTEM WITH COOLING BY HEAT-TRANSFER FLUID, AIRCRAFT COMPRISING SUCH A SYSTEM AND METHOD FOR MANUFACTURING SUCH A SYSTEM

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. Liqui...

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Bibliographische Detailangaben
Hauptverfasser:	GAUTIER, Cyrille, NEHME, Samir, YOUSSEF, Toni, MARTINEAU, Donatien Henri Edouard
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COSMONAUTICS ELECTRIC SOLID STATE DEVICES NOT OTHERWISE PROVIDED FOR ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS SEMICONDUCTOR DEVICES TRANSPORTING
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Beschreibung
Zusammenfassung:	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.