US2019045655A1PendingUtilityA1
Phase change material heat sink using additive manufacturing and method
Est. expiryOct 28, 2035(~9.2 yrs left)· nominal 20-yr term from priority
H10W 40/735H05K 7/2029H01L 23/4275B23P 2700/10B23P 15/26
44
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Claims
Abstract
A heat sink includes a lower shell, an upper shell, and an internal matrix having a space. The space is configured to receive a phase change material. The lower shell, the upper shell and the internal matrix are formed as a single component using additive manufacturing techniques. The upper shell can include a fill port and a vent port. The fill port can be configured to provide a path into the space of the internal matrix for the phase change material. The fill port and the vent port can each be configured to receive a seal plug, such as an expansion plug.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A heat sink comprising:
a lower shell; an upper shell; and an internal matrix comprising a space, wherein the space is configured to receive a phase change material; wherein the lower shell, the upper shell, and the internal matrix are formed as a single component using additive manufacturing techniques.
2 . The heat sink of claim 1 , wherein the upper shell comprises a fill port and a vent port.
3 . The heat sink of claim 2 , wherein the fill port is configured to provide a path into the space of the internal matrix for the phase change material.
4 . The heat sink of claim 2 , wherein the fill port and the vent port are each configured to receive a seal plug.
5 . The heat sink of claim 4 , wherein each seal plug comprises an expansion plug.
6 . The heat sink of claim 1 , wherein:
the lower shell, the upper shell, and the internal matrix comprise a thermally-conductive material; and the internal matrix is designed to optimize heat transfer into the phase change material.
7 . A phase change material (PCM) heat sink comprising:
a phase change material; a lower shell; an upper shell; and an internal matrix comprising a space, wherein the space is configured to receive the phase change material; wherein the lower shell, the upper shell, and the internal matrix are formed as a single component using additive manufacturing techniques.
8 . The PCM heat sink of claim 7 , wherein the upper shell comprises a fill port and a vent port.
9 . The PCM heat sink of claim 8 , wherein the fill port is configured to provide a path into the space of the internal matrix for the phase change material.
10 . The PCM heat sink of claim 8 , wherein the fill port and the vent port are each configured to receive a seal plug.
11 . The PCM heat sink of claim 8 , further comprising:
a first seal plug configured to seal the fill port; and a second seal plug configured to seal the vent port.
12 . The PCM heat sink of claim 11 , wherein each seal plug comprises an expansion plug.
13 . The PCM heat sink of claim 7 , wherein:
the lower shell, the upper shell, and the internal matrix comprise a thermally-conductive material; and the internal matrix is designed to optimize heat transfer into the phase change material.
14 . An apparatus comprising:
a structural component; and a heat sink comprising a lower shell, an internal matrix configured to receive a phase change material, and an upper shell, the internal matrix comprising a plurality of parallel pins or plates; wherein the lower shell, the internal matrix, and the upper shell of the heat sink comprise a single-structure component that is incorporated into the structural component such that the heat sink and the structural component are integral.
15 . The apparatus of claim 14 , wherein:
the upper shell comprises a fill port and a vent port; and the fill port is configured to provide a path into the space of the internal matrix for the phase change material.
16 . The apparatus of claim 15 , further comprising:
a first seal plug configured to seal the fill port; and a second seal plug configured to seal the vent port.
17 . The apparatus of claim 16 , wherein each seal plug comprises an expansion plug.
18 . The apparatus of claim 14 , wherein:
the internal matrix comprises the plurality of parallel pins; and the parallel pins comprise hour-glass shaped pins.
19 . The apparatus of claim 14 , wherein the internal matrix comprises:
the plurality of parallel plates; and a second plurality of parallel plates perpendicular to the plurality of parallel plates.
20 . The apparatus of claim 14 , wherein the structural component comprises an airframe or a bulkhead.Join the waitlist — get patent alerts
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