Thermal management system for an aircraft avionics bay
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United States of America Patent
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Sep 5, 2017
Issued Date -
N/A
app pub date -
Aug 29, 2011
filing date -
Aug 29, 2011
priority date (Note) -
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Abstract
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.
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