HYBRID POWER GENERATION SYSTEMS AND METHODS
20220042452 · 2022-02-10
Assignee
Inventors
Cpc classification
F05D2220/76
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/232
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C1/05
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B2315/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B15/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02C1/05
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A thermodynamic power generation system for generating power from a low-grade or mid-grade heat source includes a turbine coupled to an electrical generator and a closed circuit fluid flow path for a refrigerant. The system also includes an adsorption thermal compressor positioned in the flow path, the adsorption thermal compressor comprising an inlet buffer vessel, an outlet buffer vessel, and two or more fluidized adsorber beds, each containing a sorbent. The fluidized adsorber beds are arranged in parallel. The system also includes a refrigerant configured to circulate within the fluid flow path, the turbine, and the adsorption thermal compressor, for driving the turbine. The refrigerant is configured to be adsorbed and desorbed by the sorbent in a vapor phase without condensing into a liquid phase. The two or more fluidized adsorber beds each cycle between an adsorption phase and a desorption phase.
Claims
1. A thermodynamic power generation system for generating power from a low-grade or mid-grade heat source, the system comprising: a turbine coupled to an electrical generator; a closed circuit fluid flow path for a refrigerant, the fluid flow path extending from an outlet of the turbine to an inlet of the turbine, such that the turbine is within the flow path; an adsorption thermal compressor positioned in the flow path, the adsorption thermal compressor comprising: an inlet buffer vessel; an outlet buffer vessel; two or more fluidized adsorber beds, each adsorber bed containing a sorbent, the two or more fluidized adsorber beds being arranged in parallel, with an inlet end of each adsorber bed in fluid communication with the inlet buffer vessel, and with an outlet end of each adsorber bed in fluid communication with the outlet buffer vessel; a refrigerant configured to circulate within the fluid flow path, the turbine, and the adsorption thermal compressor, for driving the turbine, wherein the refrigerant is configured to be adsorbed and desorbed by the sorbent in a vapor phase without condensing into a liquid phase; wherein the two or more fluidized adsorber beds are in thermal communication with the low-grade or mid-grade heat source, wherein the two or more fluidized adsorber beds are configured to transfer heat from the low-grade or mid-grade heat source to the refrigerant; and wherein the two or more fluidized adsorber beds each cycle between an adsorption phase and a desorption phase.
2. The system of claim 1, wherein the two or more fluidized adsorber beds operate out of phase with one another, such that at least one fluidized adsorber bed is adsorbing refrigerant while at least one other fluidized adsorber bed is desorbing refrigerant.
3. The system of claim 1, wherein refrigerant exiting the outlet of the turbine is configured to flow into one of the fluidized adsorber beds during an adsorption phase, and wherein refrigerant entering the inlet of the turbine is configured to flow from one of the fluidized adsorber beds during a desorption phase.
4. The system of claim 1, wherein the two or more fluidized adsorber beds comprise four fluidized adsorber beds, and wherein the four fluidized adsorber beds alternately cycle between a precooling phase, an adsorption phase, a pre-heating phase, and a desorption phase.
5. The system of claim 1, wherein the closed circuit fluid flow path lacks a condenser.
6. The system of claim 1, wherein the closed circuit fluid flow path lacks an evaporator.
7. The system of claim 1, wherein the closed circuit fluid flow path lacks a refrigerant pump.
8. The system of claim 1, wherein the sorbent comprises a metal organic framework with a chemical affinity for the refrigerant.
9. The system of claim 1, wherein the sorbent comprises at least one metal selected from groups Ia, IIa, IIIa, Iva to VIIIa, and Ib to VIb, wherein the at least one metal has a chemical affinity for the refrigerant.
10. The system of claim 1, wherein the sorbent comprises at least one metal selected from the group consisting of Mg, Ca, Sr, Ba, Sc, Y, Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Mn, Re, Fe, Ro, Os, Co, Rh, Ir, Ni, Pd, Pt, Cu, Ag, Au, Zn, Cd, Hg, Al, Ga, In, Ti, Si, Ge, Sn, Pb, As, Sb, Bi, and the lanthanide family, wherein the at least one metal has a chemical affinity for the refrigerant.
11. The system of claim 1, wherein the sorbent comprises at least one metal selected from the group consisting of Zr, Cr, and Fe, wherein the at least one metal has a chemical affinity for the refrigerant.
12. The system of claim 1, wherein the sorbent comprises a covalent organic framework with a chemical affinity for the refrigerant.
13. The system of claim 1, wherein the sorbent comprises a hierarchical porous carbon with a chemical affinity for the refrigerant.
14. The system of claim 1, wherein the sorbent comprises a zeolite or mesoporous silica framework with a chemical affinity for the refrigerant.
15. The system of claim 1, wherein the sorbent comprises a composite combination of two or more of a metal organic framework, a covalent organic framework, a hierarchical porous carbon, and a zeolite or mesoporous silica framework, and wherein the sorbent is in the form of a mixed matrix with a chemical affinity for the refrigerant.
16. The system of claim 1, wherein the fluidized adsorber beds are configured to provide a high capacity uptake of the refrigerant in pores of the sorbent while the refrigerant remains in vapor phase.
17. The system of claim 1, wherein the adsorption thermal compressor further comprises a periodic adsorption power generation system.
18. The system of claim 1, wherein, when a fluidized adsorber bed is in the desorption phase, an output pressure of the adsorber bed falls to a minimum while a temperature of the adsorber bed rises to a maximum, and wherein, when a fluidized adsorber bed is in the adsorption phase, the output pressure of the adsorber bed increases to a maximum while the temperature of the adsorber bed falls to a minimum.
19. The system of claim 1, wherein the refrigerant comprises a pure hydrofluorocarbon (HFC) or hydrofluoroolefin (HFO).
20. The system of claim 1, wherein the refrigerant comprises a mixture of two or more hydrofluorocarbons (HFCs) or hydrofluoroolefins (HFOs).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0036] For a better understanding of the described embodiments and to show more clearly how they may be carried into effect, reference will now be made, by way of example, to the accompanying drawings in which:
[0037]
[0038]
[0039]
[0040]
[0041]
[0042]
[0043]
[0044]
[0045] The drawings included herewith are for illustrating various examples of articles, methods, and apparatuses of the teaching of the present specification and are not intended to limit the scope of what is taught in any way.
DESCRIPTION OF EXAMPLE EMBODIMENTS
[0046] Various apparatuses, methods and compositions are described below to provide an example of an embodiment of each claimed invention. No embodiment described below limits any claimed invention and any claimed invention may cover apparatuses and methods that differ from those described below. The claimed inventions are not limited to apparatuses, methods and compositions having all of the features of any one apparatus, method or composition described below or to features common to multiple or all of the apparatuses, methods or compositions described below. It is possible that an apparatus, method or composition described below is not an embodiment of any claimed invention. Any invention disclosed in an apparatus, method or composition described below that is not claimed in this document may be the subject matter of another protective instrument, for example, a continuing patent application, and the applicant(s), inventor(s) and/or owner(s) do not intend to abandon, disclaim, or dedicate to the public any such invention by its disclosure in this document.
[0047] Furthermore, it will be appreciated that for simplicity and clarity of illustration, where considered appropriate, reference numerals may be repeated among the figures to indicate corresponding or analogous elements. In addition, numerous specific details are set forth in order to provide a thorough understanding of the example embodiments described herein. However, it will be understood by those of ordinary skill in the art that the example embodiments described herein may be practiced without these specific details. In other instances, well-known methods, procedures, and components have not been described in detail so as not to obscure the example embodiments described herein. Also, the description is not to be considered as limiting the scope of the example embodiments described herein.
[0048] The overarching purpose of systems and methods disclosed herein is to convert low-grade or mid-grade heat into electricity. The disclosed technology exploits the known property of certain sorbents, nominally a metal-organic framework (MOF), to adsorb and desorb fluorocarbon refrigerants depending on temperature. More specifically, the disclosed technology extends this concept by integrating a MOF fluidized adsorption thermal compressor to improve heat and mass transfer.
[0049]
[0050] The organic chemicals typically used by an ORC include traditional refrigerants, such as iso-pentane, chlorofluorocarbons (CFCs), hydrofluorocarbons (HFCs), butane, propane, and ammonia. Such traditional refrigerants typically require high temperature heat sources between 100° C. (212° F.) and 143° C. (290° F.), and cannot operate effectively at temperatures higher than 143° C. or less than 37° C. (100° F.). A refrigerant capable of operating outside these temperature ranges may therefore be considered desirable.
[0051] In systems and methods disclosed herein, refrigerants may include a mixture of two or more of the following components: HFC 134a (1,1,1,2-tetrafluoro ethane, having a chemical formula of CHF); HFC245fa (1,1,1,3,3-pentafluoropropane, having a chemical formula of CHFs); HFC365mfc (1,1,1,3,3-pentafluorobutane, having a chemical formula of CHFs); etc. Such refrigerant mixtures may differ from the traditional pure refrigerants in that they may boil at extremely low temperatures and are capable of capturing heat at temperatures less than 23° C. (73° F.), thus facilitating power generation power from low and medium heat sources (e.g. industrial waste heat). Alternatively, a single ‘pure’ refrigerant may be used.
[0052] The composition of refrigerant mixtures may be adjusted so that the mixture may boil and generate power over a wide range of heat source temperatures from as low as 23° C. to 480° C. (about 70 to 900° F.). The refrigerant mixtures may be characterized by variable saturation temperatures, and their boiling points may be tailored to maximize the heat absorption at the evaporator and produce improved, and preferably optimized, power generation.
[0053] As a result, such refrigerant mixtures may produce power from captured low and medium heat sources in applications such as process industries, solar and geothermal energy, gray water and warm ocean waters. Compared with using typical fossil fuels, using an organic Rankine cycle with refrigerant mixtures as disclosed herein may significantly reduce the output of NO.sub.x compounds (i.e., NO.sub.2 and NO.sub.3) and CO. Further, the present quaternary refrigerant mixtures may have a long life-cycle therefore require reduced maintenance and repair costs. These factors may result in a relatively short payback period for an initial investment, when compared to existing ORC systems.
[0054]
[0055] When heat is available, the adsorption bed A, which begins saturated with refrigerant, is initially isolated from the turbine by valves 1A and 2A. In this process, when heat is applied to the adsorption bed A, its temperature and pressure increase. During the desorption process, valve 1A is opened while valve 2A remains closed. When the pressure of the full system rises up to the turbine pressure, the refrigerant evaporates and flows towards the turbine (expander). The desorbed vapor then enters the turbine—which is connected to an electric generator—and expands. The amount of desorbed refrigerant from the adsorption bed increases with increasing bed temperature and the adsorbate (refrigerant) concentration continues to decrease.
[0056] When the adsorption bed has reached the desirable refrigerant concentration, valve 1A between the turbine input and adsorption bed A is closed and the adsorption bed A is cooled to its initial temperature. The system pressure is reduced after the expansion. During the adsorption process, the adsorption bed B is at the initial temperature that connects to the turbine output through the valve 1B. This time valve 2B is closed. The low-pressure refrigerant vapor from the turbine output is adsorbed through the valve 1B by the cooled adsorption bed B. This completes the adsorption cycle. For continuous operation, the two adsorption beds work alternatively as an adsorption and desorption process.
[0057] When the absorption bed B is saturated with refrigerant vapor coming from the turbine, the valve 1B is closed and the valve 2B is opened. At this time the heat is applied to the adsorption bed B and starts for the desorption process. The cycle begins and the valve 2A is opened for the adsorption process by the adsorption bed A.
[0058]
[0059] With reference to the system illustrated in
[0064] The flow sheet model illustrated in
[0072] The system of
[0073] The amount of refrigerant that loads onto a solid adsorbent depends on temperature and pressure. In HYBRX system, loading can be expected to increase at lower temperatures and higher pressures, and to decrease at higher temperatures and lower pressures. To date, calculations for HYBRX systems have been based on published data. It is expected that loading data collected experimentally (e.g. in a laboratory) will verify these calculations.
[0074] Loading isotherms (a mathematical model) were used in order to construct a simulation of the HYBRX process. Loading data for a R134A/MIL-101(Cr) system were published by Zheng et al. (2019) over the range of 15 to 35° C. and 0 to 5 bar (a). This loading data was fitted using a Langmuir temperature dependent isotherm model:
where w.sub.i is loading in kmol/kg, P.sub.i is the partial pressure of the refrigerant in bar (a), T is temperature in K, and IP.sub.x are independent fitting parameters.
[0075]
[0076]
[0077] As discussed above, HYBRX systems and methods integrate a fluidized adsorption bed to improve heat and mass transfer. The fluidization behavior of spherical particles is strongly dependent on particle diameter and density. Larger, denser particles have higher terminal velocities, and also higher minimum fluidization velocities. This means they require more energy to fluidize. However, very small and low density particles exhibit other challenging fluidization behavior—the electrostatic forces between the particles becomes dominant over drag, which leads to channeling and poor fluidization as the particles adhere to one another.
[0078] These challenges can be overcome by use of special methods, such as high velocity gas jets, pulsating flow, and mechanical vibration of the beds. However, this usually leads to fluidization of more uniform agglomerates rather than true fluidization of nano-scale particles.
[0079] For conventional fluidization techniques, Geldart researched different powders and proposed a fluidization chart, an example of which is illustrated in
[0080] The use of fluidized beds in HYBRX systems is expected to provide significantly improved heat and mass transfer compared to fixed beds of solids in gas/solid contacting applications. For example,
[0081] Based on available experimental data, the trends indicate that higher pressures and smaller particle diameters may lead to higher achievable heat transfer coefficients. It is believed that a value of 700 W/m2 K is a reasonable target for an achievable heat transfer coefficient given small particle size and sufficient gas velocity. The heat transfer coefficient for a HYBRX system will depend on, e.g. the material and size of solid particles that will be used, and/or the refrigerant (or refrigerant mix).
[0082] As used herein, the wording “and/or” is intended to represent an inclusive-or. That is, “X and/or Y” is intended to mean X or Y or both, for example. As a further example, “X, Y, and/or Z” is intended to mean X or Y or Z or any combination thereof.
[0083] While the above description describes features of example embodiments, it will be appreciated that some features and/or functions of the described embodiments are susceptible to modification without departing from the spirit and principles of operation of the described embodiments. For example, the various characteristics which are described by means of the represented embodiments or examples may be selectively combined with each other. Accordingly, what has been described above is intended to be illustrative of the claimed concept and non-limiting. It will be understood by persons skilled in the art that other variants and modifications may be made without departing from the scope of the invention as defined in the claims appended hereto. The scope of the claims should not be limited by the preferred embodiments and examples, but should be given the broadest interpretation consistent with the description as a whole.