A system for managing heat transfer is provided by the present disclosure, which in one form includes a cavity having an inner wall portion, at least one heat-generating component disposed within the cavity, and a plurality of heat conducting members disposed adjacent one another. Each heat conducting member includes a resilient core and an outer shell wrapped around at least a portion of the resilient core. The outer shell is made of a material having a relatively high thermal conductivity, and the plurality of heat conducting members are positioned between the heat-generating component and the inner wall portion of the cavity.
THERMAL MANAGEMENT SYSTEM FOR AN AIRCRAFT AVIONICS BAY
2019-01-10
Patent
Elektronische Ressource
Englisch
IPC: | H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION / H01L Halbleiterbauelemente , SEMICONDUCTOR DEVICES |
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