THERMAL MANAGEMENT SYSTEM FOR AN AIRCRAFT AVIONICS BAY

摘要

A system for managing heat transfer is provided by the present disclosure, which in one form includes a cavity (16) having an inner wall portion (24), at least one heat-generating component (20) disposed within the cavity, and a plurality of heat conducting members (30) disposed adjacent one another. Each heat conducting member includes a resilient core (32) and an outer shell (34) 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.