US20140238634A1

US20140238634A1 - Reversible metal hydride thermal energy storage systems, devices, and process for high temperature applications

Info

Publication number: US20140238634A1
Application number: US14/189,942
Authority: US
Inventors: Ewa Carin Ellinor Ronnebro; Greg A. Whyatt; Michael R. Powell
Original assignee: Battelle Memorial Institute Inc
Current assignee: Battelle Memorial Institute Inc
Priority date: 2013-02-26
Filing date: 2014-02-25
Publication date: 2014-08-28
Also published as: WO2014134186A1

Abstract

High-temperature thermal energy storage and retrieval systems, devices, and processes are described that reversibly store high-temperature heat in metal hydride beds composed of titanium-containing metals or transition metal alloy that reversibly form metal hydrides at high temperatures above about 600° C. and at low temperatures at or below 100° C. The present invention provides exergetic efficiency up to 96% or better.

Description

CROSS REFERENCE TO RELATED APPLICATION

This is a Non-Provisional application that claims priority from U.S. Provisional Application No. 61/769,628 entitled “Reversible Metal Hydride Thermal Energy Storage System and Process for High Temperature Power Generation”, filed 26 Feb. 2013, which reference is incorporated in its entirety herein.

STATEMENT REGARDING RIGHTS TO INVENTION MADE UNDER FEDERALLY-SPONSORED RESEARCH AND DEVELOPMENT

This invention was made with Government support under Contract DE-ACO5-76RL01830 awarded by the U.S. Department of Energy. The Government has certain rights in the invention.

BACKGROUND OF THE INVENTION

Currently, no commercial high-temperature thermal energy storage systems (TES) are available that operate above 600° C. for applications such as power generation. Some conventional thermal energy storage (TES) systems employ molten salts reported to operate at mid-level temperatures up to 500° C. However, energy density for these systems is only about 153 kJ/kg. Thus, large quantities of salts are required to operate. Medium temperature systems that employ magnesium hydride (MgH₂) are reported to operate at temperatures between 250° C. and 500° C. and hydrogen pressures between 20 bar and 40 bar. However, at higher temperatures, magnesium hydride requires significantly increased pressures. For example, at a temperature of 520° C., a pressure of 132 bar is required. Elevated pressures significantly increase costs as containers must withstand the added pressures. Further, at a pressure of ≈250 bar (25 MPa), storage as a hydride is not possible above a temperature of 566° C. due to a problematic phase transition from Mg+β(MgH₂) to a mixture of Mg and H₂. Another system based on molten CaH₂is reported that operates continuously at temperatures between 1000° C. and 1200° C. However, to withstand these temperatures, reactor tanks must be constructed of costly nickel-based alloys. Accordingly, new systems, devices, and processes are needed that increase energy density, exergetics, and provide suitable commercial operation costs. The present invention addresses these needs.

SUMMARY OF THE INVENTION

The present invention includes a Reversible Metal Hydride (RMH) Thermochemical (RMHT) energy storage and retrieval system. The system may include at least one HT reservoir and at least one LT reservoir. The HT and LT reservoirs may each include a metal hydride bed. The HT metal hydride bed may include a titanium-containing metal in the presence of hydrogen gas that reversibly forms a metal hydride at a temperature at or above about 600° C. The LT metal hydride bed may include a transition metal alloy that reversibly forms a metal hydride in the presence of hydrogen gas at a temperature at or below about 100° C. The system may include a hydrogen transfer device that is configured to transfer hydrogen gas between the metal hydride bed of the HT reservoir and the metal hydride bed of the LT reservoir or vice versa that maintains an ambient or near-ambient hydrogen pressure in the respective reservoirs during a thermal cycle operation.
The present invention may also include a reversible thermal energy storage and retrieval device. The device may a container constructed of a corrosion-resistant metal or metal alloy with an internal compartment that includes a selected density of adjacent conducting metal disks. The metal disks may be positioned a selected distance apart and span at least a portion of the length or internal volume of the internal compartment. The separation distance between the metal disks provides a gap or space that may receive a titanium-containing metal or a transition metal alloy. The metal or metal alloy with introduced into the container charges the metal hydride bed for operation and reversibly forms a metal hydride during operation at a temperature at or above 600° C. or at or below 100° C. The metal disks enhance thermal conductivity through the metal hydride in the metal hydride bed in at least a radial direction during a thermal cycle. The separation distance between the conducting metal disks may be between about 0.25 inches (0.64 cm) and about 12 inches (30.5 cm).
The present invention may also include a process for performing reversible thermal energy storage and retrieval. The process may include delivering heat from a high-temperature heat source into a HT metal hydride bed of a HT reservoir at a temperature of at least about 600° C. to release hydrogen from the metal hydride in the metal hydride bed. Released hydrogen may be delivered into the metal hydride bed of the LT reservoir for absorption therein that stores the high-temperature heat. When heat is required, LT reservoir may release hydrogen from the LT metal hydride bed within the LT reservoir, which may be delivered back to the HT metal hydride bed within the HT reservoir. When absorbed in the HT reservoir, hydrogen releases heat that can be sent to a power block to drive a Rankine stream cycle that produces electricity.
The process may include matching the hydrogen flow rate between the HT reservoir and the LT reservoir during operation.
The process may include recovering high-temperature heat from the hydrogen gas released from the HT metal hydride bed in a recuperation system to recuperate the heat that may be used to preheat feed water into a Rankine steam cycle.
The process may include maintaining a hydrogen gas pressure within the metal hydride beds of the HT reservoir and the LT reservoir between about 0.1 MPa and about 1 MPa during operation.
The process may include introducing the titanium-containing metal or the transition metal-containing metal alloy into the metal hydride beds of the HT and LT reservoirs between adjacent conducting metal disks within the storage containers.
The metal hydride beds of the respective HT and LT reservoirs may include one or more storage containers with an internal compartment comprising a selected density of adjacent conducting metal disks that are positioned a selected distance apart. The conducting metal disks may span at least a portion of the length or internal volume of the internal compartment. The separation distance between the conducting metal disks may be filled with a titanium-containing metal or a transition metal alloy that reversibly form metal hydrides during thermal cycle operation. The metal disks enhance thermal conductivity in at least a radial direction through the metal hydride beds of the HT and LT reservoirs during a thermal cycle operation. The density of conducting metal disks is between 2% and 10% of the volume of the HT or LT reservoir, respectively.
The gas transfer device may be a sintered porous metal conduit with an inner bore of a selected dimension positioned within the metal hydride beds configured to deliver hydrogen into the metal hydride bed for formation of the metal hydride or to recover hydrogen released from the metal hydride bed during operation. The gas transfer device may include a selected metal or metal alloy such as stainless steel. The gas transfer device may couple to conducting metal disks positioned within the metal hydride beds of the HT and LT reservoirs. The sintered porous conduit maintains a hydrogen gas pressure in the metal hydride beds of the HT and LT reservoirs between about 0.1 MPa and about 1 MPa during a thermal cycle operation.
The HT and LT reservoirs may each include a fluid transfer device configured to deliver a heat transfer fluid that delivers heat into or retrieves heat from the HT metal hydride bed and the LT metal hydride bed within respective reservoirs.
Heat transfer fluids for the HT bed may include sodium metal, lead-bismuth, and tin-antimony. Heat transfer fluids for the LT bed may include water, propylene glycol, ethylene glycol, or mixtures of these fluids.
The metal positioned within the HT metal hydride bed may include titanium metal and the metal alloy within the LT metal hydride bed may include one or more metals selected from: Ti, Fe, Ni, Mn, or combinations. The titanium-containing metal reversibly forms a titanium metal hydride at a high temperature between about 600° C. and about 800° C. The transition metal alloy may be a titanium-containing metal alloy that reversibly forms a metal hydride at a low temperature between about 20° C. and about 100° C. The titanium-containing metal and transition metal alloy may be in the form of compressed powder disks in the one or more HT and LT reservoirs, respectively.
The HT and LT metal hydride beds of the HT reservoir and the LT reservoirs may further include a conducting metal foam with a density of open pores of at least about 8% by weight or at least about 10 pores per inch (20.5 pores per cm) into which the metal or transition metal alloy powder may be dispersed. The metal foam may be a copper metal foam or an aluminum metal foam.
The system may provide an energy density of at least about 750 kJ/kg and a volumetric energy density of at least about 3,000 kWh/m³. The system may provide a heat flux of at least about 3,000 W/m²during operation. The system may provide an exergetic efficiency of up to about 95% or better. The system may include a recuperation system that recuperates sensible heat for steam generation.
Various advantages and novel features of the present invention are described herein and will become further readily apparent to those of ordinary skill in the art from the following detailed description. Additional advantages and novel features of the present invention will be set forth as follows and will be readily apparent from the descriptions and demonstrations set forth herein. As will be realized, the invention is capable of modification in various respects without departing from the invention. Accordingly, the drawings and description of the preferred embodiment set forth hereafter are to be regarded as illustrative in nature, and not as restrictive.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a thermal energy storage (TES) and retrieval system of a bench-scale design according to one embodiment of the present invention.

FIG. 2 shows a single metal hydride storage reservoir for one embodiment of the present invention.

FIG. 3 shows a thermal energy storage (TES) and retrieval system of an industrial-scale design according to another embodiment of the present invention.

FIG. 4 shows an exemplary metal hydride storage tank of one embodiment that includes one or more metal hydride storage reservoirs for high-temperature or low-temperature operation.

FIG. 5 shows a single metal hydride storage reservoir of the present invention used in HT and LT storage reservoirs.

FIGS. 6A-6B show exemplary system configurations for recuperation of heat used to desorb hydrogen from the low temperature hydride bed during thermal cycling.

FIG. 7 shows outer wall temperatures of the high-temperature and low-temperature metal hydride storage reservoirs obtained during thermal cycling.

FIG. 8 shows model absorption and desorption curves obtained from an embodiment of the present invention.

FIG. 9 shows experimental absorption and desorption curves obtained during thermal cycling of an embodiment of the present invention.

DETAILED DESCRIPTION

The present invention includes a new High Temperature Metal Hydride Thermochemical Storage system that stores high-temperature heat including, e.g., solar energy or waste heat for high-temperature energy production applications. The following description includes preferred embodiments of the invention that illustrate the best mode contemplated for carrying out the invention. It will be clear from this description of the invention that the invention is not limited to these illustrated embodiments but that the invention also includes a variety of modifications and embodiments thereto. Therefore the present description should be seen as illustrative and not limiting. Because the invention is susceptible of various modifications and alternative constructions, it should be understood that there is no intention to limit the invention to the specific form disclosed, but, on the contrary, the invention is to cover all modifications, alternative constructions, and equivalents falling within the spirit and scope of the invention as defined in the claims.
FIG. 1 shows a cross-sectional view of a thermal energy storage (TES) and retrieval system 100 of a bench-scale design according to one embodiment of the present invention. System 100 may include a HT metal hydride storage tank (reservoir) 2 and a LT metal hydride storage tank (reservoir) 4. HT storage reservoir 2 and LT storage reservoir 4 may be constructed of corrosion-resistant metals or metal alloys including, e.g., stainless steel alloys or Inconel alloys. In the instant embodiment, reservoirs 2 and 4 may be of a single-wall design with both an outer (exterior) surface and an inner surface. Dimensions of the HT reservoir and the LT reservoir are not limited. In the exemplary embodiment, HT reservoir 2 may include a diameter dimension of about 5 inches (12.7 cm) with an I.D. of 5.1 inches and O.D. of 5.6 inches, and a length of from 22.5 inches (57.9 cm) to 24 inches (60.9 cm). LT reservoir 4 may include a diameter of 5 inches (12.7 cm) or less and a length of 22.5 inches (57.9 cm) to 24 inches (60.9 cm) or less. Dimensions are exemplary only, and other dimensions may be employed. No limitations are intended.
HT metal hydride storage reservoir 2 may include a HT metal hydride bed 6 composed of a metal foam 8 such as copper foam (e.g., DUOCEL® copper foam, ERG Materials and Aerospace Corp., Oakland, Calif., USA) into which a selected titanium-containing metal 10 powder is introduced that reversibly absorbs hydrogen and forms a metal hydride at high temperatures. LT metal hydride storage reservoir 4 may include a LT metal hydride bed 12 composed of a metal foam 8 such as copper foam into which a selected transition metal or metal alloy 14 is introduced that reversibly absorbs hydrogen and forms a metal hydride at LT. In some embodiments, metal foam 8 may include a density of 8% with 10 pores per inch. Pores of foam 8 create interstitial spaces that may be filled with the metal hydride powder. Metal hydride powders loosely packed within the open cells (pores) of the copper foam enhances thermal conductivity or transfer of heat in both the radial and axial directions.
In some embodiments, titanium metal and transition metal alloy powders introduced into respective reservoirs may have a mesh size of about 60, but particle size is not intended to be limited.
Thermal energy is stored in the chemical bonds between the metal or metal alloy and hydrogen of the metal hydride in the selected reservoirs. Hydrogen acts as the energy carrier that may be released when needed. Thermal cycling between the HT metal hydride 10 formed in HT bed 6 of HT storage reservoir 2 and LT metal hydride 14 formed in LT bed 12 of LT storage reservoir 4 during operation are driven by gas-solid chemical reactions accompanied by heats of reaction that provide maximum exergetic efficiency.
Reservoirs may be operated at selected temperatures and ambient hydrogen pressures detailed herein. For example, the dual bed system of the present invention may employ selected metal hydrides that permit a wide range of temperatures and pressures to be used. In some embodiments, the high-temperature (HT) metal hydride may be a titanium-containing hydride. Titanium hydride is capable of forming hydrides over a range of [H:Ti] ratios from 0 to 2 or more. In the exemplary embodiment, heat storage may be accomplished with [H:Ti] ratios of from 1.0 to 1.5 where the phase diagram shows both β and δ phases present. Operation in this region allows a swing in hydrogen loading of about 1 wt % with only small changes in temperature at a constant pressure. In some embodiments, formation of the high-temperature (HT) metal hydride operates reversibly at temperatures exceeding 600° C. and pressures of at least about 1 bar. In some embodiments, formation of the HT metal hydride operates reversibly at a temperature of 640° C. and a hydrogen pressure of 1 bar. In some embodiments, HT metal hydride operates reversibly at a temperature from about 650° C. to about 700° C. In some embodiments, formation of the HT metal hydride operates reversibly over temperatures in the range from about 450° C. to about 900° C. and is safe to handle at ambient temperature. Decomposition begins above 400° C.
In some embodiments, the low-temperature metal hydride may be titanium iron hydride or another transition metal alloy. The LT metal hydride stores hydrogen until heat is needed. In some embodiments, formation of the LT metal hydride operates reversibly at a temperature between about 20° C. and about 100° C.
HT reservoir 2 and LT storage reservoir 4 may each include a hydrogen gas transfer conduit 16 comprised of a sintered, porous metal positioned, e.g., at the centerline of HT metal hydride bed 6 of HT reservoir 2 and LT metal hydride bed 12 of LT storage reservoir 4. Transfer conduit 16 delivers and collects hydrogen gas to and from respective beds 6 and 12 during operation. In the exemplary embodiment, transfer conduit 16 includes a dimension (O.D.) of about ½ inch (1.3 cm), but dimensions are not intended to be limited. In the figure, transfer conduit 16 connects metal hydride bed 6 of HT storage reservoir 2 to metal hydride bed 12 of LT storage reservoir 4. In some embodiments, HT reservoir 2 and LT storage reservoir 4 may be connected via interconnecting tubes with valves that connect the two metal hydride beds.
HT reservoir 2 and LT storage reservoir 4 may further include retention screens 18 or another retention device constructed of suitable materials including, e.g., metals or metal alloys with a mesh size sufficiently small to ensure retention of metal hydride particles. Retention screens 18 may be positioned at respective ends of HT reservoir 2 and LT storage reservoir 4 to retain metal hydride powders within the reservoirs. Screen mesh sizes are not limited. Screens 18 may be mounted to, e.g., metal support disks 20 that include a center perforation that permits mounting to hydrogen transfer conduit 16 at respective ends of metal hydride beds 6 and 12 within HT reservoir 2 and LT storage reservoir 4.
HT reservoir 2 and LT storage reservoir 4 may include metal end caps 22 positioned at respective ends of the reservoirs that enclose the metal hydride beds 6 and 12 with their respective metal hydride powders 10 and 14 in the copper foam 8 within the respective reservoirs. During operation, metal end caps 12 may be filled with hydrogen gas at the reservoir operation pressure. Metal caps 22 may be secured to reservoirs 2 and 4 to form a leak tight seal. Hydrogen in end caps 22 is in communication with hydrogen in contact with or that otherwise surrounds metal hydride particles in hydride beds 6 and 12 of HT storage reservoir 2 and LT storage reservoir 4, respectively.
HT reservoir 2 may be wrapped with a metal sheet 24 of a selected thickness composed of a conducting metal such as copper to increase thermal conductivity of the outside surface of HT reservoir 2 along the longitudinal direction.
An optional heater 26 may be employed to test performance of HT reservoir 2 for operation by coupling HT reservoir 2 to heater 26. Heater 26 delivers heat into HT metal hydride bed 6 through the outer wall of HT reservoir 2 and tests release of hydrogen from the metal hydride bed. Heater 26 be constructed, e.g., of electrical heating wire [e.g., nickel-chrome (Ni-80/Cr-20), Pelican Wire Co., Naples, Fl, USA] that is insulated with, e.g., interlocking ceramic beads [e.g., salamander beads (0.2 in.×0.094 in.×0.21 in.), Mor Electric Heating Assoc., Inc., Comstock, Mich., USA] that circumvolve the outer wall of HT reservoir 2 and form an insulation layer 28 around HT reservoir 2. Insulation 30 composed of a selected high-quality material may also be positioned at respective ends of HT reservoir 2 around metal caps 22. Need for insulation depends in part on the scale and components of the system. For industrial-scale systems and applications, for example, need for insulation decreases because heaters are not employed. In the instant embodiment, once testing is complete, heater 26 may be exchanged with an external heat source and heat transfer fluids described further herein. No limitations are intended.
For performance testing, LT reservoir 4 may also be introduced into an optional temperature-controlled water bath 32 or other temperature-controlled environment. Temperatures of reservoirs 2 and 4 in system 100 may be controlled with a thermal adjustment device 34 such as a temperature controller that maintains low temperatures in LT reservoir 4 and high temperatures in HT reservoir 2. For industrial-scale operation, temperatures may be maintained with heat sources and recuperation systems described further herein. All system components as will be selected by those of ordinary skill in the art in view of the disclosure are within the scope of the present invention. Thus, no limitations are intended.
In the instant embodiment, HT reservoir 2 and LT reservoir 4 each include a volumetric energy-storage density greater than 25 kWh/m³. The present invention works at high exergetic efficiencies up to about 95% at operation temperatures between about 600° C. and about 800° C.
FIG. 2 shows a cut-away view of HT storage reservoir 2 of the system described previously in reference to FIG. 1. Reservoir 2 may include a metal hydride bed 6 filled with a metal foam (not shown). A metal hydride powder may be dispersed uniformly through the metal foam as described previously. Choice of metal powder configures the reservoir for either HT or LT operation. Reservoir 2 may include a hydrogen transfer conduit composed of a sintered metal positioned, e.g., at the center of the reservoir 2 to transfer and collect hydrogen gas released from or delivered to the HT metal hydride bed 6 of HT reservoir 2. The LT reservoir (FIG. 1) may be constructed similarly with the introduction of a metal alloy into the metal hydride bed.
FIG. 3 shows a reversible, high-temperature thermal energy storage (TES) system 200 of an industrial-scale thermochemical energy storage (TCES) design for high-temperature applications. System 200 may be integrated with, e.g., a solar-driven supercritical steam plant that provides electricity generation. System 200 may include one or more high-temperature (HT) storage reservoirs 40 and one or more low-temperature (LT) storage reservoirs 50. Storage reservoirs and may each include metal hydride beds 42 and 52 constructed of one or more metal hydride storage containers detailed further in reference to FIG. 5. Metal hydride storage containers may be filled with selected metals or metal alloys during assembly that form metal hydrides during thermal cycling for storage and retrieval of energy.
In the figure, a high-temperature heat source 44 or receiver including, e.g., solar collectors (e.g., 100 kW 16-facet solar dishes and 50 kW thermal dishes), advanced composite glass mirrors, heat generators, and other high-temperature thermal generators and heat sources may be used to heat a high-temperature heat transfer fluid 46. Exemplary HT heat transfer fluids include, but are not limited to, e.g., sodium metal, lead-bismuth, and tin-antimony. Heat transfer fluid 46 delivers heat into the metal hydride bed 42 which releases high-temperature hydrogen 48 from HT metal hydride bed 42. HT storage containers (FIG. 5) discharge and collect hydrogen efficiently and effectively at high temperatures selected between about 600° C. and about 900° C. High-temperature hydrogen 48 released from HT storage reservoir 40 may be delivered to and passed through power block 54 (e.g., a Rankine cycle steam power) where sensible heat carried by hydrogen 48 may be used to raise temperature that preheats feed water delivered into a steam cycle in power block 54 before hydrogen 48 is stored in LT storage reservoir 50. “Sensible heat” is heat that causes a direct increase in temperature of an object when introduced and a direct decrease in temperature of an object when heat is removed. Preheating feed water can reduce the quantity of high-temperature heat required generate steam needed to drive turbines that generate power in power block 54. Sensible heat is a low duty heat (<10% of exergy) compared to high quality heat delivered by hot HTF 46, which allows sensible heat to be effectively used. As an example, feed water may be preheated to a temperature of, e.g., 291° C. before going to a boiler where steam is generated at a temperature of, e.g., 593° C. In this scenario, about 30% (⅓) of the heat duty may be used to preheat feed water, mostly from steam taken from turbines. Sensible heat delivered from high-temperature hydrogen 48 may be about 8% of the total exergy delivered to steam block 54.
Hydrogen 48 passing from power block 54 may then be introduced into LT metal hydride bed 52 of LT storage reservoir 50. The transition metal in LT hydride bed 52 absorbs hydrogen 48 forming a transition metal hydride that stores heat during. LT metal hydride storage containers (FIG. 5) that make up LT hydride bed 52 discharge and collect hydrogen efficiently and effectively at low temperatures between about 20° C. and about 100° C. LT heat transfer fluids (not shown) circulated through LT bed 52 maintain the temperatures. LT heat transfer fluids include, but are not limited to, e.g., water, propylene glycol, ethylene glycol, mixtures of these fluids, and like media.
When heat is needed, hydrogen 56 released from LT hydride bed 52 may be delivered from LT storage reservoir 50 back to HT storage reservoir 40 where it is adsorbed back into HT hydride bed 42 in an exothermic reaction that releases heat during thermal cycling. Hydrogen 56 returned to HT hydride bed 42 may flow directly from LT bed 52. The hydrogen flow stream may be controlled by valves (not shown). Reversible chemical reactions in LT reservoir 50 are similar to those in HT reservoir 40.
HTF 46 may transfer heat between HT storage bed 42 and power block 54. For example, HTF 46 may deliver high temperature heat at a first (e.g., T1) high temperature of, e.g., ˜650° C. from HT hydride bed 42 to power block 54 where water may be heated into supercritical steam to drive power turbines (not shown) that generate power 58. A pump 60 (e.g., an electrodynamic pump) may set the circulation rate for HTF 46 to bring the high temperature of HTF 46 to the first temperature. In exemplary tests, a high-temperature heat transfer fluid may deliver 30 kW of heat with a flow of about 36.5 liters per minute (Ipm) or about ˜9.7 gallons per minute (gpm). Pump 60 may also be set at a flow rate that provides a predetermined temperature drop for the HTF 46 that generates steam within power block 54 at a desired rate. For example, if flow of heat into steam block 54 is less than the flow of heat from solar collector 44 into HT reservoir 40, inlet temperature (T1) at steam block 54 may increase above the temperature of HT bed 42. Maximum temperature drop for HTF 46 through power block 54 may be also selected such that the HTF is returned at a lowest operation temperature (e.g., T3) as a low-temperature flow 62 to solar collector 44 for reheating. In various embodiments, maximum temperature drop may be up to about 50° C. At the upper limit, the HTF may be returned to solar collector 44 at a temperature (T3) of about 600° C. However, no limitations are intended.
Heat transfer fluids may be selected that have selected freezing points suitable for high temperature operation. For example, when power is not produced, pump 60 may maintain a sufficient flow of HTF 46 to prevent freezing of the HTF. For example, liquid sodium as an HTF becomes a solid metal (i.e., freezes) below 98° C.
When heat is neither stored nor retrieved, HTF 46 does not flow through HT storage reservoir 40. When heat is stored, a pump 64 may be positioned to produce a flow of HTF 46 through HT storage reservoir 40 and then back to heat source 44. Here, as liquid sodium HTF 46 passes through HT bed 42, HTF 46 heats the reservoir walls of the one or more HT metal hydride containers (FIG. 5) to a temperature (e.g., T2) that is at or near the temperature of the HTF. Heat from HTF 46 passes through the walls of the containers into the metal hydride bed 42.
The HTF leaves HT bed 42, e.g., at the bottom of HT storage reservoir 40 as a flow 66 that is at the temperature (T2) near the wall temperature of the storage containers back to heat source 44. Over the heat loading cycle, wall temperature of metal hydride bed 42 may increase, e.g., from about 660° C. to about 703° C.
HTF 46 delivered from HT-bed storage reservoir 40 at temperature (T1), e.g., at the top of HT bed 42, closely matches the wall temperature of the storage reservoir. Temperature drop of HTF 46 from HT-bed 42 may be too fast or too large to maintain the HTF temperature entering steam block 54. In the figure, pump 64 (e.g., an electrodynamic pump) may pump HTF 46 in an upward direction to restore temperature of HTF 46 entering steam block 54. Flow to solar collector 44 may then be reduced to allow HTF 46 to maintain a desired temperature at a lower flow rate. Then, pump 60 may be set to deliver steam through power block 54 at a desired rate and a predetermined temperature.
When there is no solar input, pump 60 may be set to provide HTF 46 at a flow rate that is, e.g., ˜10% higher than the flow through pump 64 so that some flow is provided through solar collector 44 to prevent freezing of HTF 46. Pump 64 may also drive primary circulation of HTF 46 through HT bed 42 to power block 54.
Pump 64 may also be operated to produce a flow rate for HTF 46 that maintains HTF 46 at a temperature ˜10° C. above the temperature of HT storage bed 42. For example, hot HTF 46 may flow down through HT storage reservoir 40 to allow HTF 46 to give up heat to HT bed 42 in storage reservoir 40. Temperature differentials affect pumping costs. For example, if temperature of HTF 46 is too close to the temperature of HT bed 42, more energy may be required to pump the fluid compared with the quantity of heat stored on a per unit basis. As will be appreciated by those of ordinary skill in the art, temperature differentials selected between HTF 46 and HT storage bed 42 are not limited. Temperature differentials are selected that optimize performance. Thus, no limitations are intended.
Modeled results indicate temperature of HT storage bed 42 may fall from about 691° C. to about 653° C. during retrieval of heat, but is not intended to be limiting.
When there is a shortage of heat delivered from solar collector 44, a portion of HTF 46 returning to solar collector 44 may be withdrawn and pumped through HT bed 42 to provide sufficient heat to HTF 46 to permit it to be joined with the flow of HTF 46 sent to power block 54. As heat is extracted from HT bed 42, hydrogen from LT bed 52 may be delivered back to HT bed 42 to maintain hydrogen pressure in both HT bed 42 and in LT bed 52. Hydrogen does not flow to power block 54 when heat is being retrieved. Hydrogen flows to power block 54 only when heat is introduced to HT bed 42.
In the instant embodiment, H₂gas may be stored in LT reservoir 50 which is advantageous. For example, practical storage volumes for the LT reservoir are lower than gas storage tanks by a factor of about 350 times compared with storage of H₂at atmospheric pressure. LT bed 52 forms a metal hydride reversibly within a range of temperatures between about 20° C. and about 55° C. of the ambient temperature depending on selected operating conditions. Heat of reaction for formation of the metal hydride in LT bed 52 is in the range from about 25 KJ/mol to about 30 kJ/mol. Composition of the LT hydride bed may be tuned based on the choice of metal alloys so that hydrogen release rates and hydrogen diffusion rates match those of HT metal hydride bed 42. As will be appreciated by those of ordinary skill in the art, temperatures and heats of reaction may vary depending on the choices of metal hydrides and selected conditions. Thus, no limitations are intended.
In some embodiments, LT metal hydride bed 52 may be filled with a Ti—Mn—Fe metal alloy configured to operate near ambient temperatures with hydrogen pressures that match the operating pressures of HT hydride bed 40. During storage of hydrogen, low-grade (low-duty) heat may be rejected to atmosphere. The term “low grade heat” refers to heat with a sufficiently low temperature that is unusable to perform work. Heat at or below a temperature of about 100° C. is considered low-grade heat. The term “high grade heat” refers to heat that is capable of doing work, e.g., to generate electrical power. Heat typically above a temperature above 100° C. can perform work.
During retrieval of hydrogen, cooling can occur in LT reservoir 50 as a side effect. Temperature in LT storage bed 52 may be maintained using heat (e.g., waste heat) dissipated, e.g., by a condenser (e.g., a Rankine cycle condenser) (not shown) in power block 54.
In some embodiments, as an alternative to storing hydrogen in a LT hydride bed, H₂gas released from the HT storage reservoir may be stored in a gas storage tank (not shown). In these embodiments, use of a gas storage tank for low-temperature storage presumes energy requirements for compression and storage of hydrogen are favorable.
The invention provides a thermal energy storage capacity defined by an energy density between about 700 kJ/kg and 800 kJ/kg or a volumetric energy density of between about 3000 kJ/m³and about 4000 kJ/m³. Energy density values are a factor of ten times greater than those achieved with conventional molten salt systems known in the art. System 200 provides superior energy densities that provide operation costs below conventional systems. In various embodiments, operation costs may be below about $30/kWh. System 200 with its selection of titanium powders is also scalable. For example, titanium powders may be produced in scalable quantities up to ton quantities or greater at selected impurity levels. For example, at a higher impurity levels, if performance metrics can be maintained, operation costs may be reduced accordingly.
FIG. 4 shows a HT storage reservoir 40 of an exemplary design used in the TES system described previously in reference to FIG. 3. Storage reservoir 40 may be of a cylindrical design constructed of a corrosion-resistant metal or metal alloy such as stainless steel or another suitable structural material. However, shapes are not intended to be limited. HT storage reservoir 40 may include an internal metal hydride bed 42 that includes one or more metal hydride storage containers 72 of a selected design each filled with one or more selected metal hydrides, described further in reference to FIG. 5. In one exemplary configuration, metal hydride bed 42 may include 31 metal hydride containers 72, but number is not intended to be limited. Each metal hydride container 72 may be mounted into a top support plate 74 and a bottom support plate 76. Plates 74 and 76 are preferably in a horizontal position within storage reservoir 40, but orientation is not intended to be limited. Top plate 74 and bottom plate 76 may each include fluid flow channels or holes 78 positioned around each metal hydride reservoir 72 that allow a heat transfer fluid (not shown) when introduced into reservoir 40 to fill and surround hydride storage containers 72 of metal hydride bed 42. Fluid flow channels or holes 78 further allow heat transfer fluid to drain from HT reservoir 40 when reservoir 40 is emptied.
Storage reservoir 40 may include an HTF inlet 80 for introduction of heat transfer fluid and a second HTF outlet 82 for release of heat transfer fluid from storage reservoir 40 during operation. Inlet 80 (or outlet) and outlet 82 (or inlet) are reversible depending on the direction of flow of HTF into reservoir 40. Thus, no limitations are intended. In the figure, baffles 84 may be placed at selected locations along the inside wall of storage reservoir 40 to prevent pooling of HTF introduced into storage reservoir 40. As HTF enters HTF inlet 80, a corresponding quantity of HTF may exit from HTF outlet 82 or vice versa. Flow of HTF through reservoir 40 may be controlled to maintain temperature differences within storage reservoir 40. For example, during heat storage, HTF may be flowed in a downward direction through storage reservoir 40 and in an upward direction during heat retrieval. However, flows of HTF are not intended to be limited.
Hydride storage containers 72 may each include a porous hydrogen gas transfer conduit 16 that is constructed of a sintered metal or metal alloy that introduces and collects hydrogen gas from the metal hydride contained with the storage containers. Gas transfer conduits 16 couple to manifold (header) 86 positioned, e.g., at the top of storage reservoir 40 to distribute or collect hydrogen gas uniformly into or from transfer conduits 16 during operation. Hydrogen gas may enter or return through a hydrogen inlet/outlet 88 through manifold (header) 86 into and from each metal hydride container 72 within storage reservoir 40 at selected temperatures during operation.
HT metal hydride storage containers 72 that configure reservoir 40 for operation may each be filled with a metal hydride that operates reversibly at high temperatures. In some embodiments, the metal selected for HT operation may be titanium metal that forms TiH at temperatures greater than 600° C. In various embodiments, metal hydride storage containers 72 of the HT bed may operate at temperatures selected above 600° C. and at hydrogen gas pressures at or above 1 bar. In some embodiments, the HT bed may operate at a temperature between about 600° C. and about 750° C. In some embodiments, the HT bed may operate at 640° C. In some embodiments, the HT bed may operate at temperatures between about 600° C. and about 800° C.
LT reservoir (FIG. 3) may include a configuration similar to that described here for the HT reservoir. Differences between the respective reservoirs may include the number of metal hydride containers, different metal hydride(s), and different heat transfer fluids described herein. All other components may be identical. No limitations are intended. For example, LT reservoir may include one or more metal hydride storage containers that configure the LT bed for operation. Each LT storage container may be filled with a selected metal alloy containing a transition metal configured to form a metal hydride at a low temperature.
In some embodiments, the metal alloy may be a titanium-containing alloy. In some embodiments, the metal alloy may be a metal TiFeNi alloy. In some embodiments, the LT metal alloy may be a TiFeMn alloy.
In some embodiments, the LT metal hydride bed X may operate at a temperature near ambient temperature to store H₂desorbed from the HT bed. In some embodiments, the low temperature containers of the LT metal hydride bed may be configured to operate at temperatures above about 20° C. In some embodiments, the low temperature containers of the LT metal hydride bed may be configured to operate at temperatures between about 20° C. and about 100° C. In various embodiments, the LT bed may operate at a temperature selected above 20° C. and at hydrogen pressures at or above 1 bar. In some embodiments, the LT bed may operate at a temperature between about 20° C. and about 100° C. at hydrogen pressures at or above 1 bar.
HT reservoirs and LT reservoirs when coupled may store thermal energy for a time greater than about 8 hours on average. HT reservoirs can be charged for operation in a time of less than about 6 hours on average.
In operation, HT reservoirs and LT reservoirs provide an energy density of between about 700 kJ/kg and 800 kJ/kg, or a volumetric energy density between about 3000 kJ/m³and about 4000 kJ/m³.
FIG. 5 shows a HT metal hydride container 72 of an exemplary design that configures the HT metal hydride bed of the HT storage reservoir (FIG. 4) for operation. Differences between the components of the HT metal hydride container and the LT metal hydride container may include the metal hydride selected for use in the container and selected operation temperatures.
In the figure, metal hydride container 72 may be constructed of a corrosion-resistant metal or metal alloy such as stainless steel. In the figure, container 72 may include a cylindrical design. Container 72 may include an internal compartment 90 and a container lid 92 that seals container 72. Inner compartment 90 may include a selected quantity or density of adjacent conducting metal disks 94 that span at least a portion of the length within the container. Conducting metal disks 94 may be constructed of copper or aluminum or another conducting metal to increase thermal conductivity within the container and enhance transfer of heat from the inside of the container wall to the metal hydride within the container. Metal disks 94 may be positioned a selected distance apart within the container. Separation distances between adjacent metal disks may be selected that allow a metal or metal alloy powder to be inserted between the metal disks in the container.
In some embodiments, metal or metal alloys may be in the form of a powder introduced or inserted between adjacent conducting metal disks in the HT container 72 that charge the container for operation. In some embodiments, the powder may be in the form of a compressed powder disk or disks (not shown) that allow for convenient and rapid exchange. Metal or metal alloy powders may be compacted, e.g., with a press. In some embodiments, powder disks may each include a diameter selected to maximize the packing density in the HT container. Compressed powder disks and metal disks 94 may be stacked in the thickness dimension to fill the container.
In various embodiments, spacing between adjacent conducting metal disks 94 may be selected between about 0.25 inches (0.64 cm) and about 5 inches (12.7 cm). Spacing depends in part on the distribution of heat into the metal or metal alloys positioned within the container and ease of exchange for compressed metal or metal alloy powders.
Conducting metal disks 94 enhance thermal heat conductivity in both radial direction and the axial direction through the metal hydride powder in the container. Conducting metal disks may displace a within inner compartment 90 at or below about 10% on average. However, densities are not intended to be limited. For example, higher densities may be employed when increased thermal cycling is desired. No limitations are intended.
Diameter of conducting metal disks 94 and powder disks may each match or be below the inside diameter of storage container 72. In some embodiments, diameter of conducting metal disks and powder disks may be selected between about 3 inches (7.6 cm) and about 12 inches (30.5 cm). In some embodiments, diameter of conducting metal disks and powder disks may be about 5 inches (12.7 cm) or greater. Diameter of conducting metal disks and powder disks may also be selected to maximize contact between the metal disks and the powder disks to maximize thermal conductivity in the container.
HT container 72 may further include indexing slits 96 introduced at selected locations along the length of the inner wall of container 72 and/or container lid 92. Indexing slits 96 serve to secure conducting metal disks 94 when the container lid is closed and secured for operation at selected temperatures and pressures. In some embodiments, metal disks and compressed powder disks may be alternatively stacked within the container without a need of indexing slots within the container. In other embodiments, metal or metal alloys may be in a compressed form in the form of a single disk that may be introduced as a single unit into the container.
Metals and metal alloys may include a particle size selected to provide optimum cycle life, capacity, and flat plateau pressures during operation. In some embodiments, metal or metal alloy powder may include a particle size of about 60 mesh, but mesh size is not intended to be limited. Particle size can be expected to change during thermal cycling due to the change in volume during formation of the metal hydride during operation.
Systems of the present invention achieve a (net) exergetic efficiency (e.g., in a round trip thermal cycle) of up to about 96% in operation based on an enthalpy for the HT metal hydride (operating at temperatures in the HT reservoir between about 600° C. to about 800° C.) of about 150 kJ/mol and an enthalpy for the LT metal hydride (operating at temperatures in the LT reservoir of about room temperature or above) of about 25 kJ/mol. Such efficiencies lower costs of operation. For example, as heat is withdrawn from storage, high exergetic efficiency is achieved because the temperature at which heat is removed from the reservoir is maintained at a high temperature by the hydride reaction and does not fall as would the temperature of a sensible heat storage medium. Heat withdrawn from the HT storage reservoir thus allows each Watt of extracted heat to do a sustained level of work in contrast with sensible heat in which a falling temperature reduces the work that can be done. The present invention also extracts sensible heat from high-temperature hydrogen leaving the HT storage reservoir during heat storage may be delivered to the steam power block to assist in the production of electricity. An exemplary system for recovery of sensible heat from hydrogen released from the HT metal hydride bed will now be described.
FIG. 6A shows an exemplary system 300 for recovery of sensible heat during heat storage mode. At the start of the heat storage cycle, working hydrogen capacity resides in HT bed 42. Recovery system 300 may employ three different heat transfer fluids or media, including, but not limited to, e.g., carbonate salts 114, nitrate salts 122, and mineral oil 130. At the start of the storage cycle, heat transfer fluids 114, 122, and 130 reside in their respective low temperature (cool) temperature reservoirs 116, 124, and 132. In the figure, high-temperature heat 110 may be added to HT hydride bed 42 at ˜700° C. Heat absorbed by the HT hydride bed results in endothermic decomposition of some fraction of the metal hydride in the bed, which results in release of hydrogen 48. Released hydrogen 48 may be delivered through a recuperator 112 (e.g., a counter-current recuperator) where sensible heat may be transferred from the hydrogen to a heat transfer medium composed of or including, e.g., a carbonate salt 114. The carbonate salt may be drawn from a cool reservoir 116 and passed through recuperator 112 where heat from the hydrogen is transferred. Carbonate salt released from recuperator 112 may be stored in a hot (e.g., carbonate salt) reservoir 118 at a temperature, e.g., of about ˜700° C. Flow of carbonate salt 114 may be adjusted to match the flow rate of the hydrogen gas in order to minimize temperature differences (so-called temperature approaches) between the various flows delivered to and from recuperator 112, to and from cool fluid reservoir 116, and to and from hot fluid reservoir 118. For example, matching the flows of fluids permits a close approach_at either end of recuperator 112 such that carbonate salt 114 may leave recuperator 112 at a temperature near (e.g. within ˜20° C.) the hydrogen inlet temperature. Hydrogen may further leave recuperator 112 at a temperature near (i.e. within ˜20° C.) the inlet temperature of cool carbonate salt reservoir 116.
Hydrogen leaving recuperator 112 may then enter recuperator 120 at a lower temperature. Transfer of heat from the hydrogen may be repeated with, e.g., a molten nitrate salt 122 collected from a cool nitrate salt reservoir 124. Cool nitrate salt 122 may be heated by flowing through recuperator 120 and be subsequently stored in hot nitrate salt reservoir 126. Transfer of heat from hydrogen to the nitrate salt cools the hydrogen to a temperature near (e.g. within ˜20° C.) the storage temperature of the cool nitrate salt 122. Hydrogen may then be released from recuperator 120 and enter recuperator 128 where mineral oil 132 from cool reservoir 134 may be heated by exchanging heat with the flowing hydrogen. Heated mineral oil 130 may be stored in a hot (mineral oil) reservoir 134. Hydrogen may be released from recuperator 128 at a temperature near (i.e. within ˜20° C.) of the ambient temperature, which may then be received into low temperature metal hydride bed 52. Absorption of hydrogen into LT hydride bed 52 generates heat 136, which may be rejected to the ambient environment due to its low exergetic value. For example, at an ambient temperature of 25° C., each Watt of heat rejected at 50° C. may have an exergetic value of about 0.08 Watts). A typical heat loss target may be about 1% of the total heat input to the system during any 24 hour thermal cycle. At the end of the storage cycle, the working capacity of hydrogen resides in LT bed 52 and heat transfer fluids 114, 122, and 130 reside in their respective high temperature reservoirs 118, 126, and 134.
FIG. 6B shows operation of heat recovery system 300 during heat retrieval. Heat released during heat retrieval mode may be used to drive a Rankine steam cycle 54 that generates electricity. At the start of the heat retrieval cycle, heat transfer fluids 114, 122, and 130 reside in their respective high temperature (hot) reservoirs 118, 126, and 134. In the figure, high-temperature heat 110 may be withdrawn from HT bed 42 and used for generation of steam 140. Steam 140 drives turbines 142 that produce electricity 58 as an output. Steam 140 may then be condensed 144 using, e.g., a steam condenser 146 (e.g., ˜40° C. Rankine cycle condenser). Condenser 146 may be used since it operates at a temperature slightly above ambient (e.g. <100° C., and preferably <50° C.). A fraction of heat 148 obtained from condensation may be delivered to LT hydride bed 52 which releases LT hydrogen 56 from LT bed 52. Hydrogen
Hydrogen 56 from LT bed 52 may be heated in recuperator 128 by flowing mineral oil 130 from hot (mineral oil) reservoir 134 through recuperator 128 back to cool reservoir 132. Hydrogen released from recuperator 128 may be introduced to recuperator 120 where the hydrogen may be heated to a higher temperature by flowing molten nitrate salt 122 from hot reservoir 126 to cool reservoir 124. Hydrogen released from recuperator 120 may be introduced to recuperator 112 to heat the hydrogen further. The hydrogen may be heated by flowing molten carbonate salt 114 from hot reservoir 118 through recuperator 112 to cool reservoir 116. Hydrogen released from recuperator 112 may then be absorbed into HT hydride bed 42 where the heat of reaction maintains the temperature of the bed as heat is withdrawn for production of electricity. While three transfer fluids have been shown, the present invention is not intended to be limited thereto. For example, use of multiple heat transfer fluids overcomes the difficulty of identifying a single heat transfer fluid that can be used over a temperature range from ambient to 700° C. Nitrate salts cannot be used at ambient temperature because they solidify and cannot be used above about 500° C. because they thermally decompose. In some embodiments, two heat transfer fluids may be employed including, e.g., liquid sodium metal as the HT transfer fluid and mineral oil as the LT transfer fluid to span the entire temperature range.
Rate at which heat is transferred into or out of the metal hydride beds of the respective storage reservoirs determines at least in part the rate at which a hydride can absorb or release hydrogen, and thus absorb or release thermal energy. Thermal conductivity dictates the design of the respective storage reservoirs. An optimized heat transfer structure optimizes the thermal conductivity and determines the efficiencies attained.
FIG. 7 shows outer wall temperatures of the HT metal hydride reservoir and the LT metal hydride reservoir described previously in reference to FIG. 1. Temperatures of both the outer wall and inner wall and inner core are important. For example, if thermal conductivity is low, metal hydride beds within the HT and LT storage reservoirs can have a decreased capacity; cycle lifetimes can also decrease. Exergetic efficiency of the metal hydride beds within the HT and LT storage containers depend on efficient thermal conductivity through the metal hydride beds and exterior and interior walls of respective HT and LT containers. As such, a low temperature gradient is preferred that achieves heat transfer within the metal hydride beds. Temperature of the metal hydride beds and reservoirs may be controlled by balancing heat loss with heat input. For example, heating of the HT metal hydride bed may be accomplished by increasing input heat to a level above the steady-state heat loss. Cooling may be accomplished by reducing input heat to a level immediately below the steady state heat loss. Modeling results predict the outer wall temperature of the LT bed (TiFe_0.925Ni_0.075) can vary from about ˜20° C. to ˜55° C. during the thermal cycle. Heating to 55° C. can occur via the bottom of the steam cycle (i.e. heating with steam exiting the low pressure turbine or using steam condensate). Simulation results show that the system can be charged or discharged over a period of 8 hours with the hydrogen pressure remaining constant and the HT hydride bed varying from ˜660° C. to 700° C. while the LT bed varies from 55° C. to 20° C. The small overshoot in the transition to idle state indicates a small thermal gradient is required to achieve the thermal flux. Isotherms and cycling behavior are described further in reference to FIG. 8 and FIG. 9.
FIG. 8 plots adsorption isotherms and desorption isotherms predicted based on a model using a measured adsorption isotherm as a basis. The model uses data on the reaction enthalpy for titanium hydride as a function of hydride loading determined by Danzter, [J. Phys. Chem. Solids. Vol. 44, No. 9, pp. 913-923, 1983] to extrapolate conditions where actual data are not available. The model was incorporated as a component in a multi-physics model (e.g., COMSOL Multiphysics® Software, COMSOL Inc., Burlington, Mass., USA) that simulated formation/decomposition of the hydride in response to changes in temperature with simultaneous heat and mass transport within storage reservoirs. In the figure, hydrogen pressure (psia) is plotted against moles of H₂absorbed/desorbed in the metal hydride bed. Operation pressures were selected at 2.4 bar. Isotherm data were then fitted for titanium hydride (Ti—H). Model isotherms show that equilibrium loading may be optimized in the Ti—H bed at pressures of about 2.4 bar and temperatures between about 650° C. and about 700° C. Swings in equilibrium hydrogen loading (dashed lines) can occur at temperatures between 650° C. and 700° C. Plateau pressures are observed at an average hydrogen pressure of about 2.4 bar over the selected temperature range. Model isotherms also show average atomic ratios between [H:Ti] at the plateau pressures between about 0.88 and about 1.55. For example, equilibrium loading is predicted to swing from 0.88 mol H:mol Ti at 700° C. to 1.55 mol H:mol Ti at 650° C. for a swing of 0.67 mol H/mol Ti. The swing corresponds to a hydrogen loading swing of about 1.4 wt % with respect to titanium mass. Actual loading swings achieved in the model depend on local temperatures reached during the loading/unloading cycle.
FIG. 9 shows adsorption/desorption isotherms (hydrogen loading curves) from tests conducted of the thermal energy storage and retrieval system of FIG. 1 during thermal cycling over the temperature range from about 650° C. to about 700° C. In the figure, pressure (psia) is plotted against moles of H₂in the metal hydride bed. Performance tests were conducted using an automated hydrogenation system controlled with a programming environment (e.g., LabVIEW, National Instruments Corp., Austin, Tex., USA). Optimum temperature for the HT reactor tank was selected between about 650° C. and about 700° C. A pressure of 2.4 bar is typical. Experimental data agree with model data (FIG. 8). In particular, plateau temperatures are reached in the temperature range from about 630° C. to about 670° C. and selected hydrogen pressures between about 5 psia and about 40 psia over the selected temperature range. Results show a cycle lifetime of over 100 thermal cycles with no loss adsorption/desorption capacity.
The dual bed TES system of the present invention finds applications: in conversion of renewable energies (e.g., concentrated solar power), in nuclear power plants, in the electrical power grid, in buildings, and in the transportation sector including the automotive sector.

EXAMPLES

The following Examples provide a further understanding of various aspects of the present invention.

Example 1

Bench-Scale Thermal Energy Storage System

A 2.5 gram sample of titanium hydride (TiH) was loaded into a temperature controlled sample container with the ability to add or remove hydrogen to maintain pressure over the sample. Operating temperature was between about 640° C. and about 650° C. Hydrogen pressure was 1 bar. Results showed a minimum of 100 thermal cycles without a loss in capacity.

Example 2

Lab-Scale Thermal Energy Storage System

10 Kg Test Bed, 3 kWh Prototype

The TES system of FIG. 1 was used for performance testing. Prior to operation, the TES system was positioned vertically with a protective Plexiglas® cover positioned at one end of the TES system in a fume hood. The high-temperature (HT) reservoir and the low-temperature (LT) reservoir were each filled with a dense (8% nominal density) copper metal foam containing 10 pores per inch (ppi) (e.g., DUOCEL® copper foam, ERG Materials and Aerospace Corp., Oakland, Calif., USA). Titanium powder was introduced into the HT reservoir by vibrating the reservoir which facilitated uniform distribution and loose compaction of the powder into the open cells of the copper metal foam. Argon gas was flowed through the test beds during filling. A total of 9.4 kilogram of metal foam was loaded with titanium powder.

Example 3

Full-Scale System (˜1,000 Kg)

A full-scale system conceptual of a 240 kWh prototype design is envisioned illustrated in FIG. 3. A HT metal hydride storage tank and a LT metal hydride storage tank described herein will be constructed. Each tank will comprise a metal hydride bed containing up to 1,000 kg of a selected metal powders in compressed form. The storage tanks will be connected to a solar collector/solar collector that will collect heat from solar collection (i.e., an On-Sun Test) and provide energy to the selected MH tanks.
While various preferred embodiments of the invention have been shown and described, it is to be distinctly understood that this invention is not limited thereto but may be variously embodied to practice within the scope of the following claims. From the foregoing description, it will be apparent that various changes may be made without departing from the spirit and scope of the present invention as defined by the following claims.

Claims

What is claimed is:

1. A reversible thermal energy storage and retrieval system, comprising:

at least one HT reservoir and at least one LT reservoir, each reservoir including a metal hydride bed,

wherein the metal hydride bed of the HT reservoir comprises a titanium-containing metal in the presence of hydrogen gas that reversibly forms a metal hydride at a temperature at or above about 600° C.;

wherein the metal hydride bed of the LT reservoir comprises a transition metal alloy that reversibly forms a metal hydride in a hydrogen gas environment at a temperature at or below about 100° C.; and

a hydrogen transfer device configured to transfer hydrogen gas between the metal hydride bed of the HT reservoir and the metal hydride bed of the LT reservoir or vice versa that maintains an ambient or near-ambient hydrogen pressure in the respective reservoirs during a thermal cycle operation.

2. The system of claim 1, wherein the metal hydride bed of the respective HT and LT reservoirs include one or more storage containers with an internal compartment comprising a selected density of adjacent conducting metal disks disposed a selected distance apart therein that span at least a portion of the length or internal volume of the internal compartment, the separation distance between the metal disks defines a space configured to receive a titanium-containing metal or a transition metal alloy therein configured to reversibly form a metal hydride during operation, the metal disks enhance thermal conductivity through the metal hydride in the metal hydride bed in at least a radial direction during a thermal cycle.

3. The system of claim 1, wherein the gas transfer device is a sintered porous conduit disposed within the metal hydride bed with an inner bore of a selected dimension configured to deliver hydrogen into the metal hydride bed for formation of the metal hydride and to recover hydrogen released from the metal hydride bed during operation.

4. The system of claim 1, wherein the heat transfer fluid for the HT metal hydride bed is selected from sodium metal, lead-bismuth, tin-antimony, and the heat transfer fluid for the LT metal hydride bed is selected from water, propylene glycol, ethylene glycol, or mixtures thereof.

5. The system of claim 1, wherein the titanium-containing metal and transition metal alloy are in the form of compressed powder disks disposed in the one or more HT and LT reservoirs, respectively.

6. The system of claim 1, wherein the metal disposed within the HT metal hydride bed comprises titanium metal and the metal alloy within the LT metal hydride bed comprises one or more metals selected from: Ti, Fe, Ni, Mn, or combinations thereof.

7. The system of claim 1, wherein the energy density is at least about 750 kJ/kg and the volumetric energy density is at least about 3,000 kWh/m³.

8. The system of claim 1, wherein the exergetic efficiency is up to about 95% or better.

9. A reversible thermal energy storage and retrieval device, comprising:

a container constructed of a corrosion-resistant metal or metal alloy with an internal compartment comprising a selected density of adjacent conducting metal disks disposed a selected distance apart therein that span at least a portion of the length or internal volume of the internal compartment, the separation distance between the metal disks defines a space configured to receive a titanium-containing metal or a transition metal alloy that when introduced defines a metal hydride bed configured to reversibly form a metal hydride during operation at a temperature at or above 600° C. or at or below 100° C., the metal disks enhance thermal conductivity through the metal hydride in the metal hydride bed in at least a radial direction during a thermal cycle.

10. The device of claim 9, wherein the metal or metal alloy is in the form of compressed powder disks that are insertable in the space disposed between the conducting metal disks.

11. The device of claim 9, wherein the metal alloy comprises one or more metals selected from the group consisting of: Ti, Fe, Ni, Mn, and combinations thereof.

12. The device of claim 9, wherein the titanium-containing metal reversibly forms titanium metal hydride at a high temperature between about 600° C. and about 800° C.

13. The device of claim 9, wherein the transition metal alloy is a titanium-containing metal alloy that reversibly forms a metal hydride at a low temperature between about 20° C. and about 100° C.

14. The device of claim 9, further includes a sintered porous metal conduit that couples to the conducting metal disks disposed therein constructed of a selected metal or metal alloy with an inner bore of a selected dimension configured to deliver hydrogen into the metal hydride bed for formation of the metal hydride and to recover hydrogen released from the metal hydride bed during a thermal cycle operation.

15. The device of claim 14, wherein the sintered porous conduit maintains a hydrogen gas pressure in the metal hydride beds of the HT and LT reservoirs between about 0.1 MPa and about 1 MPa.

16. The device of claim 9, wherein the heat transfer fluid for the HT bed includes selected from sodium metal, lead-bismuth, tin-antimony, and the heat transfer fluid for the LT bed is selected from water, propylene glycol, ethylene glycol or mixtures thereof.

17. The device of claim 9, wherein the density of conducting metal disks is between 2% and 10% of the volume of the HT or LT reservoir, respectively.

18. A process for reversible thermal energy storage and retrieval, comprising the steps of:

providing at least one HT reservoir and at least one LT reservoir each containing a metal hydride bed comprising a titanium-containing metal or a transition metal alloy, the HT metal hydride bed is configured to reversibly form a metal hydride at a temperature at or above about 600° C., the LT metal hydride bed is configured to reversibly form a transition metal alloy at a temperature at or below about 100° C.;

contacting the metal hydride in the HT reservoir with heat introduced from a high-temperature heat source to release hydrogen from the metal hydride therein;

absorbing hydrogen released from the HT reservoir in the metal hydride bed of the LT reservoir to store high-temperature heat therein;

releasing high-temperature heat at a temperature above 600° C. from the metal hydride bed of the HT reservoir to generate power.

19. The process of claim 18, wherein providing the HT reservoir and the LT reservoir includes inserting the titanium-containing metal or the transition metal-containing metal alloy between adjacent conducting metal disks disposed within one or more storage containers within the metal hydride beds of the HT and LT reservoirs, respectively.

20. The process of claim 18, wherein releasing heat from the HT metal hydride bed includes delivering the heat to a Rankine steam cycle to generate power.

21. The process of claim 18, further including recovering high-temperature heat from hydrogen gas released from the HT metal hydride bed in a recuperation system to recuperate heat used to preheat feed water into a Rankine steam cycle.

22. The process of claim 18, wherein the process includes matching the hydrogen flow rate between the HT reservoir and the LT reservoir during operation.