US2019285363A1PendingUtilityA1
Integral heat exchanger core reinforcement
Est. expiryMar 16, 2038(~11.6 yrs left)· nominal 20-yr term from priority
F28F 2260/02F28F 9/0075F28F 3/025F28D 2021/0021F28D 9/0062B33Y 10/00B23P 15/26B33Y 80/00F28F 2225/04
48
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Claims
Abstract
An embodiment of a heat exchanger core includes a plurality of walls defining a plurality of layers in at least one heat exchange relationship. At least one of the layers of the core having a first load-bearing portion aligned with and adjacent to a first mount location on a perimeter of the core, and a first non-load-bearing portion distal from the non-load-bearing portion. A topology of the first load-bearing portion has a load bearing capacity greater than a load bearing capacity of the non-load-bearing portion.
Claims
exact text as granted — not AI-modified1 . A heat exchanger core comprising:
a plurality of walls defining a plurality of layers in at least one heat exchange relationship, at least one of the layers of the core having a first load-bearing portion aligned with and adjacent to a first mount location on a perimeter of the core, and a first non-load-bearing portion distal from the non-load-bearing portion; wherein a topology of the first load-bearing portion has a load bearing capacity greater than a load bearing capacity of the non-load-bearing portion.
2 . The core of claim 1 , wherein the heat exchanger comprises a plate-and-fin heat exchanger or a micro-channel heat exchanger.
3 . The core of claim 2 , wherein the heat exchanger includes a plurality of corrugated fins.
4 . The core of claim 3 , wherein a pitch of the plurality of corrugated fins in the first load-bearing portion is less than a pitch of the plurality of corrugated fins in the same layer in the non-load-bearing portion.
5 . The core of claim 3 , wherein a thickness of the plurality of corrugated fins in the first load-bearing portion is greater than a thickness of the plurality of corrugated fins in the same layer in the non-load-bearing portion.
6 . The core of claim 3 , wherein a thickness of a plurality of plates separating the plurality of corrugated fins in the first load-bearing portion is greater than a thickness of the plurality of plates in the same layer in the non-load-bearing portion.
7 . The core of claim 1 , wherein the at least one of the layers of the core also includes a transition region between the load-bearing portion and the non-load-bearing portion.
8 . The core of claim 1 , wherein a mount portion of the core is integrally formed with at least one of a mount pad and an end plate of the heat exchanger core.
9 . A heat exchanger assembly comprising:
a mount for supporting a heat exchanger in a system; and a heat exchanger core comprising:
a plurality of walls defining a plurality of layers in at least one heat exchange relationship, at least one of the layers of the core having a first load-bearing portion aligned with and adjacent to a first mount location on a perimeter of the core, and a first non-load-bearing portion distal from the non-load-bearing portion;
wherein a topology of the first load-bearing portion has a load bearing capacity greater than load bearing capacity of the non-load-bearing portion.
10 . The assembly of claim 9 , wherein the heat exchanger assembly is a plate-and-fin heat exchanger or a micro-channel heat exchanger.
11 . The assembly of claim 10 , wherein the plate-and-fin heat exchanger includes a plurality of fins, and wherein a pitch of the plurality of fins in the first load-bearing portion of a first layer is less than a pitch of the plurality of fins in the non-load-bearing portion of the same first layer.
12 . The assembly of claim 10 , wherein the plate-and-fin heat exchanger includes a plurality of fins, and wherein a thickness of the plurality of fins in the first load-bearing portion of a first layer is greater than a thickness of the plurality of fins in the non-load-bearing portion of the same first layer.
13 . The assembly of claim 10 , wherein a thickness of a plurality of plates separating a plurality of fins in the first load-bearing portion is greater than a thickness of the plurality of plates in the same layer in the non-load-bearing portion.
14 . The assembly of claim 9 , wherein the heat exchanger is a shell-and-tube heat exchanger.
15 . The assembly of claim 14 , wherein the mount includes at least one clevis leg or bar integrally supporting at least one tube of the shell-and-tube heat exchanger.
16 . A method of making a heat exchanger, the method comprising:
forming a housing for a heat exchanger core; forming a first mount portion; additively manufacturing the heat exchanger core, the step comprising:
forming a first load-bearing region in connection with the joint/mount; and
forming a first non-load bearing region outward of the non-load bearing region.
17 . The method of claim 16 , wherein the core includes a different topology in the first load-bearing region than in the first non-load-bearing region.
18 . The method of claim 16 , wherein the first load-bearing region is aligned with the at least one integrally formed joint such that a load path includes both the first load-bearing region and the at least one integrally formed joint.
19 . The method of claim 16 , further comprising:
forming a mount for a heat exchanger assembly; and integrally forming the mount with at least one core wall or at least one manifold wall of the heat exchanger assembly via one or more of a casting process or an additive manufacturing process.
20 . The method of claim 19 , wherein the mount is integrally formed with at least one of a mount pad and an end plate of the heat exchanger core.Join the waitlist — get patent alerts
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