IP Library Patent Application 13224414
Patent Application
App. No. 13/224,414

COOLING STRUCTURE

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Quick Facts
Patent No.
US None
App. No.
13/224,414
Abstract

A heat exchanger structure includes a monolithic extrusion and a plurality of headers. The extrusion includes a first end; a second end; a first, smooth side; and a second side with a plurality of smooth portions alternating with a plurality of raised portions defining a plurality of parallel flow passages extending from the first end to the second end; and a plurality of headers connecting the plurality of flow passages to form a flow path.

Claims (31)

1 . A heat exchanger structure comprising:

a monolithic extrusion comprising:

a first end;

a second end;

a first, smooth side; and

a second side with a plurality of smooth portions alternating with a plurality of raised portions defining a plurality of parallel flow passages extending from the first end to the second end; and

a plurality of headers connecting the plurality of flow passages to form a flow path through the plurality of passages.

2 . The structure of claim 1 , wherein the extrusion is aluminum.

3 . The structure of claim 1 , wherein the plurality of flow passages have a cross section with a first surface parallel to the first side of the extrusion.

4 . The structure of claim 3 , wherein the width of the cross section is semi-circular.

5 . The structure of claim 1 , wherein the plurality of flow passages have an inner diameter of about 0.25 inches (6.35 mm) to about 1.1 inches (27.94 mm).

6 . The structure of claim 1 , wherein the headers connect alternating pairs of the plurality of flow passages.

7 . The structure of claim 1 , wherein the extrusion is a curved segment.

8 . The structure of claim 1 , wherein the flow path through the plurality of flow passages is serpentine.

9 . A method of forming a heat exchanger structure comprising:

forming an extrusion as a monolithic part with a first end, a second end, a first, smooth side and a second side with a plurality of smooth portions alternating with a plurality of raised portions defining a plurality of elongated flow passages extending from the first end to the second end; and

joining the plurality of flow passages with a plurality of headers to form a flow path through the plurality of flow passages.

10 . The method of claim 9 , wherein the headers connect alternating pairs of the plurality of flow passages.

11 . The method of claim 9 , wherein the plurality of flow passages have a cross section with a first surface parallel to the first side of the structure.

12 . The method of claim 11 , wherein the cross section of the flow passages is a semi-circle.

13 . The method of claim 9 , wherein the structure is extruded as a curved segment.

14 . The method of claim 13 , and further comprising:

connecting multiple modular segments to form a full cylinder radiator.

15 . The method of claim 13 , wherein the plurality of flow passages have an inner diameter of about 0.25 inches (6.35 mm) to about 1.1 inches (27.94 mm).

16 . A method of cooling comprising:

placing a cooling structure in thermal contact with a heat producing source, wherein the structure is formed by forming an extrusion as a monolithic part with a first end, a second end, a first, smooth side and a second side with a plurality of smooth portions alternating with a plurality of raised portions defining a plurality of flow passages extending from the first end to the second end; and

flowing a coolant through the plurality of flow passages, wherein the plurality of flow passages are joined at either end by a plurality of headers connecting pairs of flow passages to form a flow path.

17 . The method of claim 16 , wherein the extrusion is aluminum.

18 . The method of claim 16 , wherein the plurality of flow passages have a cross section that is a semi-circle.

19 . The method of claim 18 , wherein the each of the plurality of flow passages is parallel to the other flow passages.

20 . The method of claim 16 , wherein plurality of headers join alternating pairs of flow passages to form a serpentine flow path.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
CHANGE OF NAME Recorded Jul 30, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 030902/0313 →
SECURITY AGREEMENT Recorded Jun 21, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0615 →
SECURITY AGREEMENT Recorded Jun 17, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0408 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 14, 2013
From: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 030612/0506 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 8, 2012
From: HAMILTON SUNDSTRAND CORPORATION
To: PRATT & WHITNEY, ROCKETDYNE, INC.
Reel/Frame 029293/0682 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 6, 2011
From: HAMILTON SUNDSTRAND CORPORATION
To: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.
Reel/Frame 027026/0467 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 2, 2011
From: BROMBERG, MARCELO; LU, CHENG-YI
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 026849/0236 →