IP Library Granted Patent US 9,657,966
Granted Patent B2
US 9,657,966 · App. 12/639,056 · Granted May 23, 2017

Single bi-temperature thermal storage tank for application in solar thermal plant

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Quick Facts
Patent No.
US 9,657,966
App. No.
12/639,056
Granted
May 23, 2017
Kind
B2
Abstract

Thermocline storage tanks for solar power systems are disclosed. A thermocline region is provided between hot and cold storage regions of a fluid within the storage tank cavity. One example storage tank includes spaced apart baffles fixed relative to the tank and arranged within the thermocline region to substantially physically separate the cavity into hot and cold storage regions. In another example, a flexible baffle separated the hot and cold storage regions and deflects as the thermocline region shifts to accommodate changing hot and cold volumes. In yet another example, a controller is configured to move a baffle within the thermocline region in response to flow rates from hot and cold pumps, which are used to pump the fluid.

Claims (21)

1. A tank comprising:

a wall having a portion providing a cavity;

wherein the tank has a horizontal cross-section defining a cross-sectional area, the cross-section accommodating a baffle, the baffle configured to be located in a thermocline region of a fluid within the cavity and vertically separating the cavity into first and second regions, and configured to permit substantially limited flow between the first region and the second region wherein the baffle has a flow area comprising one or more aperture(s), wherein the flow area is configured to permit fluid flow between the first and second regions, the flow area corresponding to less than 1% of the cross-sectional area; and

a skirt attached to the baffle, the skirt having a geometry based at least in part on the portion, the skirt proximate to the portion.

2. The tank of claim 1 , wherein the portion defines at least a majority of a vertical portion of the wall.

3. The tank of claim 1 , wherein the baffle substantially separates the first and second regions respectively into a first volume and a second volume.

4. The tank of claim 3 , wherein a hot fluid is in the first volume and a cold fluid is in the second volume.

5. The tank of claim 4 , wherein a mixing of the hot fluid and the cold fluid is limited by the baffle.

6. The tank of claim 5 , wherein the baffle includes plural apertures configured to permit substantially limited flow between the first volume and the second volume.

7. A tank comprising:

a wall having a portion providing a cavity;

wherein the tank has a horizontal cross-section defining a cross-sectional area, the cross-section accommodating a membrane, the membrane configured to be located in a thermocline region of a fluid within the cavity and vertically separating the cavity into first and second regions, and configured to permit substantially limited flow between the first region and the second region wherein the membrane has a flow area comprising one or more aperture(s), wherein the flow area configured to permit fluid flow between the first and second regions, the flow area corresponding to less than 1% of the cross-sectional area; and

a skirt attached to the membrane, the skirt having a geometry based at least in part on the portion, the skirt proximate to the portion.

8. The tank of claim 7 , wherein the portion is a vertical portion.

9. The tank of claim 7 , wherein the membrane substantially separates the first and second regions respectively into a first volume and a second volume.

10. The tank of claim 9 , wherein a hot fluid is in the first volume and a cold fluid is in the second volume.

11. The tank of claim 10 , wherein a mixing of the hot fluid and the cold fluid is limited by the membrane.

12. The tank of claim 11 , wherein the membrane includes plural apertures configured to permit substantially limited flow between the first volume and the second volume.

13. A tank comprising: a wall having a portion providing a cavity; a baffle configured to be located in a thermocline region of a fluid within the cavity and vertically separating the cavity into first and second regions, and configured to permit substantially limited flow between the first region and the second region; a skirt attached to the baffle, the skirt having a geometry based at least in part on the portion, the skirt proximate to the portion; and wherein the tank has a width and height, and the width is greater than the height; wherein the tank has a horizontal cross-section defining a cross-sectional area, the cross sectional accommodating the baffle, wherein the baffle has a flow area comprising one or more aperture(s), wherein the flow area is configured to permit fluid flow between the first and second regions, the flow area corresponding to less than 1% of the cross-sectional area.

14. A tank comprising: a wall having a portion providing a cavity; a membrane configured to be located in a thermocline region of a fluid within the cavity and vertically separating the cavity into first and second regions, and configured to permit substantially limited flow between the first region and the second region; a skirt attached to the membrane, the skirt having a geometry based at least in part on the portion, the skirt proximate to the portion; and wherein the tank has a width and height, and the width is greater than its height; wherein the tank has a horizontal cross-section defining a cross-sectional area, the cross-section accommodating the membrane, wherein the membrane has a flow area comprising one or more aperture(s), wherein the flow area is configured to permit fluid flow between the first and second regions, the flow area corresponding to less than 1% of the cross-sectional area.

15. The tank of claim 1 configured for use with a fluid at a temperature of at least 288° C.

Assignments (7)
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 →
RELEASE OF SECURITY INTEREST Recorded Sep 23, 2015
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 036666/0103 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2014
From: AEROJET ROCKETDYNE OF DE
To: SOLARRESERVE TECHNOLOGY, LLC
Reel/Frame 034530/0978 →
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 Dec 16, 2009
From: LITWIN, ROBERT ZACHARY; WAIT, DAVID; LANCET, ROBERT T.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 023659/0417 →