Baffled thermoclines in thermodynamic cycle systems

Patent metadata

Field	Value
Publication number	US-11053847-B2
Application number	US-201615392542-A
Country	US
Kind code	B2
Filing date	Dec 28, 2016
Priority date	Dec 28, 2016
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

Solid-state thermoclines with internal baffle structures are used in place of heat exchangers in a closed thermodynamic cycle power generation or energy storage system, such as a closed Brayton cycle system. The baffles limit the conductive and/or radiative transfer of heat between a solid thermal medium within different zones defined by the baffle structures.

First claim

What is claimed is:

1. A thermal system comprising:
a motor;
a compressor;
a first thermocline vessel comprising a first plurality of zones of a first solid thermal medium defined by first baffle structures in the interior of the first thermocline vessel, wherein each baffle structure of the first baffle structures is configured to limit direct transfer of heat between the first solid thermal medium in different zones of the first plurality of zones;
a second thermocline vessel comprising a second plurality of zones of a second solid thermal medium defined by second baffle structures in the interior of the second thermocline vessel, wherein each baffle structure of the second baffle structures is configured to limit direct transfer of heat between the second solid thermal medium in different zones of the second plurality of zones;
a turbine; and
a working fluid circulating, in a charge mode of the thermal system, through a closed cycle fluid path comprising, in order, (i) the compressor, (ii) the first thermocline vessel and the first solid thermal medium in the interior of the first thermocline vessel, (iii) the turbine, and (iv) the second thermocline vessel and the second solid thermal medium in the interior of the second thermocline vessel,
wherein the first solid thermal medium within a first zone proximate to an inlet of the working fluid to the first thermocline vessel is at a first temperature, and wherein the first solid thermal medium within a second zone proximate to an outlet of the working fluid from the first thermocline vessel is at a second temperature higher than the first temperature,
wherein the second solid thermal medium within a third zone proximate to an inlet of the working fluid to the second thermocline vessel is at a third temperature, and wherein the second solid thermal medium within a fourth zone proximate to an outlet of the working fluid from the second thermocline vessel is at a fourth temperature lower than the third temperature,
wherein the motor is coupled to the compressor, and
wherein the motor is configured to facilitate operation of the thermal system in the charge mode by operating the compressor using electricity.

2. The thermal system of claim 1 , wherein the working fluid within the first thermocline vessel is at a pressure greater than atmospheric pressure.

3. The thermal system of claim 1 further comprising a recuperative heat exchanger configured to thermally contact the working fluid exiting the compressor with the working fluid exiting the turbine, wherein the working fluid circulates through the closed cycle fluid path comprising, in order, (i) the compressor, (ii) the recuperative heat exchanger, (iii) the first thermocline vessel and the first solid thermal medium in the interior of the first thermocline vessel, (iv) the turbine, (v) the recuperative heat exchanger, and (vi) the second thermocline vessel and the second solid thermal medium in the interior of the second thermocline vessel.

4. The thermal system of claim 3 further comprising a heat rejection device configured to eject from the thermal system heat carried by the working fluid, wherein the working fluid circulates through the closed cycle fluid path comprising, in order, (i) the compressor, (ii) the recuperative heat exchanger, (iii) the first thermocline vessel and the first solid thermal medium in the interior of the first thermocline vessel, (iv) the turbine, (v) the recuperative heat exchanger, (vi) the heat rejection device, and (vii) the second thermocline vessel and the second solid thermal medium in the interior of the second thermocline vessel.

Assignees

• Malta Inc

Inventors

• Apte Raj
• Larochelle Philippe

Classifications

• Y02E60/14

  Thermal energy storage · CPC title

• F02C1/04

  the working fluid being heated indirectly {(in a fluidised-bed combustor F02C3/205)} · CPC title

• F28D2020/0086

  Partitions · CPC title

• F02C6/14 Primary

  Gas-turbine plants having means for storing energy, e.g. for meeting peak loads · CPC title

• F02C1/10

  Closed cycles · CPC title