IP Library Granted Patent US 10,458,283
Granted Patent B2
US 10,458,283 · App. 15/440,295 · Granted Oct 29, 2019

Varying compression ratios in energy storage and retrieval systems

Inventors: Robert B. Laughlin (Mountain View, CA); Philippe Larochelle (Mountain View, CA); Nicholas Cizek (Mountain View, CA)
Assignee: Malta Inc.
F01K3/00F01K3/12F01K3/185F01K3/20F02C1/10F02C6/14F24S60/00F28D15/00F28D20/00F05D2250/90Y02E20/14Y02E20/16Y02E60/14
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Quick Facts
Patent No.
US 10,458,283
App. No.
15/440,295
Granted
Oct 29, 2019
Kind
B2
Abstract

In the present disclosure, an example method is provided. The example method may comprise operating a pumped thermal system in a charging cycle at a first compression ratio, wherein the pumped thermal system comprises a working fluid circulating through, in sequence, a compressor system, a hot side heat exchanger, a turbine system, and a cold side heat exchanger, wherein the working fluid is in thermal contact with a hot thermal storage (“HTS”) medium in the hot side heat exchanger and the working fluid is in thermal contact with a cold thermal storage (“CTS”) medium in the cold side heat exchanger. The example method may also comprise operating the pumped thermal system in a discharging cycle at a second compression ratio different than the first compression ratio.

Claims (87)

1. A method comprising:

operating a pumped thermal system in a charging cycle at a first compression ratio, wherein the pumped thermal system comprises a working fluid circulating through, in sequence, a compressor system, a hot side heat exchanger, a turbine system, and a cold side heat exchanger, wherein the working fluid is in thermal contact with a hot thermal storage (“HTS”) medium in the hot side heat exchanger and the working fluid is in thermal contact with a cold thermal storage (“CTS”) medium in the cold side heat exchanger; and

operating the pumped thermal system in a discharging cycle at a second compression ratio different than the first compression ratio,

wherein the pumped thermal system is configured to circulate the working fluid through, in sequence and in the same direction, the compressor system, the hot side heat exchanger, the turbine system, and the cold side heat exchanger when the pumped thermal system operates in the charging cycle and when the pumped thermal system operates in the discharging cycle.

2. The method of claim 1 , wherein the compressor system comprises at least a first compressor and a second compressor.

3. The method of claim 2 , wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first compressor and the second compressor in parallel, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first compressor and the second compressor in series.

4. The method of claim 2 , wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first compressor and not the second compressor, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the second compressor and not the first compressor.

5. The method of claim 2 , wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first compressor and not the second compressor, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first compressor and the second compressor.

6. The method of claim 1 , wherein the turbine system comprises at least a first turbine and a second turbine.

7. The method of claim 6 , wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first turbine and the second turbine in parallel, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first turbine and the second turbine in series.

8. The method of claim 6 , wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first turbine and not the second turbine, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the second turbine and not the first turbine.

9. The method of claim 6 , wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first turbine and the second turbine, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first turbine and not the second turbine.

10. The method of claim 1 , wherein the compressor system comprises a compressor, wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises operating the compressor at a first rotation speed, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises operating the compressor at a second rotation speed different than the first rotation speed.

11. The method of claim 1 , wherein the turbine system comprises a turbine, wherein operating the pumped thermal system in the charging cycle at the first compression ratio further comprises operating the turbine at a first rotation speed, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio further comprises operating the turbine at a second rotation speed different than the first rotation speed.

12. The method of claim 1 , wherein the compressor system comprises at least a first compressor and a second compressor, wherein the turbine system comprises at least a first turbine and a second turbine, wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first compressor and the first turbine and not circulating the working fluid through the second compressor and the second turbine, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the second compressor and the second turbine and not circulating the working fluid through the first compressor and the first turbine.

13. The method of claim 1 , wherein the compressor system comprises a compressor comprising a variable pressure stator, wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises tuning the variable pressure stator to operate the compressor at a third compression ratio across the compressor, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises tuning the variable pressure stator to operate the compressor at a fourth compression ratio across the compressor.

14. The method of claim 1 , wherein the turbine system comprises a turbine comprising a variable pressure stator, wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises tuning the variable pressure stator to operate the turbine at a third compression ratio across the turbine, and wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises tuning the variable pressure stator to operate the turbine at a fourth compression ratio across the turbine.

15. The method of claim 1 , wherein the first compression ratio is a value such that

T

1

+

T

1

=

ψ

C

1

/

η

cp

,

wherein η cp is a polytropic efficiency associated with the compressor system, T 1 is a temperature at which the working fluid enters the compressor system, T 1 + is a temperature at which the working fluid exits the compressor system, and

ψ

C

=

r

γ

-

1

γ

,

where r is the first compression ratio and γ is a ratio of specific heats of the working fluid.

16. The method of claim 1 , wherein the second compression ratio is a value such that

T

1

+

T

1

=

ψ

D

η

tp

,

wherein η tp is a polytropic efficiency associated with the compressor system, T 1 is a temperature at which the working fluid enters the compressor system, T 1 + is a temperature at which the working fluid exits the compressor system, and

ψ

D

=

r

γ

-

1

γ

,

where r is the second compression ratio and γ is a ratio of specific heats of the working fluid.

17. The method of claim 1 , wherein the second compression ratio is greater than the first compression ratio.

18. The method of claim 17 , wherein the first compression ratio is less than 3 and the second compression ratio is greater than 3.

19. The method of claim 1 , wherein the first compression ratio varies based at least in part on a temperature of the working fluid.

20. The method of claim 1 , wherein the second compression ratio varies based at least in part on a temperature of the working fluid.

21. A method comprising:

operating a pumped thermal system in a charging cycle at a first compression ratio, wherein the pumped thermal system comprises a working fluid circulating through, in sequence, a compressor system, a hot side heat exchanger, a turbine system, and a cold side heat exchanger, wherein the working fluid is in thermal contact with a hot thermal storage (“HTS”) medium in the hot side heat exchanger and the working fluid is in thermal contact with a cold thermal storage (“CTS”) medium in the cold side heat exchanger; and

operating the pumped thermal system in a discharging cycle at a second compression ratio different than the first compression ratio,

wherein the compressor system comprises at least a first compressor and a second compressor,

wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first compressor and the second compressor in parallel, and

wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first compressor and the second compressor in series.

22. A method comprising:

operating a pumped thermal system in a charging cycle at a first compression ratio, wherein the pumped thermal system comprises a working fluid circulating through, in sequence, a compressor system, a hot side heat exchanger, a turbine system, and a cold side heat exchanger, wherein the working fluid is in thermal contact with a hot thermal storage (“HTS”) medium in the hot side heat exchanger and the working fluid is in thermal contact with a cold thermal storage (“CTS”) medium in the cold side heat exchanger; and

operating the pumped thermal system in a discharging cycle at a second compression ratio different than the first compression ratio,

wherein the compressor system comprises at least a first compressor and a second compressor,

wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first compressor and not the second compressor, and

wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first compressor and the second compressor.

23. A method comprising:

operating a pumped thermal system in a charging cycle at a first compression ratio, wherein the pumped thermal system comprises a working fluid circulating through, in sequence, a compressor system, a hot side heat exchanger, a turbine system, and a cold side heat exchanger, wherein the working fluid is in thermal contact with a hot thermal storage (“HTS”) medium in the hot side heat exchanger and the working fluid is in thermal contact with a cold thermal storage (“CTS”) medium in the cold side heat exchanger; and

operating the pumped thermal system in a discharging cycle at a second compression ratio different than the first compression ratio,

wherein the turbine system comprises at least a first turbine and a second turbine,

wherein operating the pumped thermal system in the charging cycle at the first compression ratio comprises circulating the working fluid through the first turbine and the second turbine, and

wherein operating the pumped thermal system in the discharging cycle at the second compression ratio comprises circulating the working fluid through the first turbine and not the second turbine.

Assignments (8)
CORRECTIVE ASSIGNMENT TO CORRECT THE SPELLING OF INVENTORS NAME PREVIOUSLY RECORDED AT REEL: 044104 FRAME: 0185. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Mar 6, 2019
From: LAROCHELLE, PHILIPPE; LAUGHLIN, ROBERT B.; CIZEK, NICHOLAS
To: GIGAWATT DAY STORAGE SYSTEMS, INC.
Reel/Frame 048516/0565 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 4, 2019
From: X DEVELOPMENT LLC
To: GOOGLE LLC
Reel/Frame 047905/0128 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 4, 2019
From: GOOGLE LLC
To: MALTA INC.
Reel/Frame 047905/0168 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 7, 2018
From: LAUGHLIN, ROBERT B.; CIZEK, NICHOLAS; LAROCHELLE, PHILIPPE
To: GIGAWATT DAY STORAGE SYSTEMS, INC.
Reel/Frame 046575/0403 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 7, 2018
From: LAUGHLIN, ROBERT B.; LAROCHELLE, PHILIPPE; CIZEK, NICHOLAS
To: GIGAWATT DAY STORAGE SYSTEMS, INC.
Reel/Frame 046575/0607 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 27, 2017
From: GOOGLE INC.
To: X DEVELOPMENT LLC
Reel/Frame 044511/0347 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 13, 2017
From: GIGAWATT DAY STORAGE SYSTEMS
To: GOOGLE INC.
Reel/Frame 044104/0200 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 13, 2017
From: LAROCHELLE, PHILIPPE; LAUGHLIN, ROBERT B.; CIZAK, NICHOLAS
To: GIGAWATT DAY STORAGE SYSTEMS, INC.
Reel/Frame 044104/0185 →
Continuity (6)
Continuation 14668610 · Mar 25, 2015
Continuation PCTUS2013062469 · Sep 27, 2013
Provisional Application 61868070 · Aug 20, 2013
Provisional Application 61706337 · Sep 27, 2012
Related Publication 20170159496A1 · Jun 8, 2017
Related Publication 20190153901A9 · May 23, 2019
Cited By (1)
US 12,348,669