The present invention is in the field of thermodynamics and is more specifically directed to a heat engine and a related heat to electricity system that utilizes the Rankine thermodynamic cycle in combination with selected working fluids to produce power from a wide range of thermal sources.
Heat is often created as a byproduct of industrial processes where flowing streams of liquids, solids or gasses that contain heat must be exhausted into the environment or removed in some way in an effort to maintain the operating temperatures of the industrial process equipment. Sometimes the industrial process can use heat exchanger devices to capture the heat and recycle it back into the process via other process streams. Other times it is not feasible to capture and recycle this heat because it is either too high in temperature or it may contain insufficient mass flow. This heat is referred to as “waste” heat. Waste heat is typically discharged directly into the environment or indirectly through a cooling medium, such as water.
Waste heat can be utilized by turbine generator systems which employ a well known thermodynamic method known as the Rankine cycle to convert heat into work. Typically, this method is steam-based, wherein the waste heat is used to raise steam in a boiler to drive a turbine. The steam-based Rankine cycle is not always practical because it requires heat source streams that are relatively high in temperature (600° F. or higher) or are large in overall heat content. The complexity of boiling water at multiple pressures/temperatures to capture heat at multiple temperature levels as the heat source stream is cooled, is costly in both equipment cost and operating labor. The steam-based Rankine cycle is not a realistic option for streams of small flow rate and/or low temperature.
There exists a need in the art for a system that can efficiently and effectively produce power from not only waste heat but also from a wide range of thermal sources.
A waste heat recovery system executes a thermodynamic cycle using a working fluid in a working fluid circuit which has a high pressure side and a low pressure side. Components of the system in the working fluid circuit include a waste heat exchanger in thermal communication with a waste heat source also connected to the working fluid circuit, whereby thermal energy is transferred from the waste heat source to the working fluid in the working fluid circuit, an expander located between the high pressure side and the low pressure side of the working fluid circuit, the expander operative to convert a pressure/enthalpy drop in the working fluid to mechanical energy, a recuperator in the working fluid circuit operative to transfer thermal energy between the high pressure side and the low pressure side of the working fluid circuit, a cooler in thermal communication with the low pressure side of the working fluid circuit operative to control temperature of the working fluid in the low side of the working fluid circuit, a pump in the working fluid circuit and connected to the low pressure side and to the high pressure side of the working fluid circuit and operative to move the working fluid through the working fluid circuit, and a mass management system connected to the working fluid circuit, the mass management system having a working fluid vessel connected to the low pressure side of the working fluid circuit.
In one embodiment, a waste heat energy recovery and conversion device includes a working fluid circuit having conduit and components for containing and directing flow of a working fluid between components of the device operative to convert thermal energy into mechanical energy, the working fluid circuit having a high pressure side and a low pressure side; a support structure for supporting the conduit of the working fluid circuit and the components, the components comprising: an expander operative to convert a pressure drop in the working fluid to mechanical energy, a power generator (such as for example an alternator) which is coupled to the expander, a recuperator, a cooler, a pump and a pump motor operative to power the pump; and a mass management system having a mass control tank for receiving and holding the working fluid, the mass control tank connected by conduit to the high pressure side of the working fluid circuit and to the low pressure side of the working fluid circuit. An enclosure may also be provided to substantially enclose some or all of the components of the device. One or more heat exchangers may be located on or off of the support structure. The heat exchanger(s), recuperator and cooler/condenser may include printed circuit heat exchange panels. A control system for controlling operation of the device may be remote or physically packaged with the device.
The disclosure and related inventions further includes a method of converting thermal energy into mechanical energy by use of a working fluid in a closed loop thermodynamic cycle contained in a working fluid circuit having components interconnected by conduit, the components including at least one heat exchanger operative to transfer thermal energy to the working fluid, at least one expansion device operative to convert thermal energy from the working fluid to mechanical energy, at least one pump operative to transfer working fluid through the working fluid circuit, the working fluid circuit having a high pressure side and a low pressure side, and a mass management system comprising a mass management vessel connected by conduit to the low pressure side of the working fluid circuit, the method including the steps of: placing a thermal energy source in thermal communication with a heat exchanger component; pumping the working fluid through the working fluid circuit by operation of the pump to supply working fluid in a supercritical or subcritical state to the expander; directing the working fluid away from the expander in a sub-critical state through the working fluid circuit and to the pump; controlling flow of the working fluid in a super-critical state from the high pressure side of the working fluid circuit to the mass management vessel, and controlling an amount of working fluid in a sub-critical or super-critical state from the mass management vessel to the low pressure side of the working fluid circuit and to the pump.
The disclosure and related inventions further includes a mass management system for controlling an amount of working fluid mass in a thermodynamic cycle in a working fluid circuit having a pump or a compressor, the mass management system having a working fluid control tank for holding an amount of the working fluid at a first pressure P, the working fluid control tank located outside of the working fluid circuit; and a fluid connection between the working fluid control tank and a low pressure side of the thermodynamic cycle in the working fluid circuit to allow passage of the working fluid between the working fluid circuit and the working fluid control tank.
These and other aspects of the disclosure and related inventions are further described below in representative forms with reference to the accompanying drawings.
The inventive heat engine 100 (also referred to herein in the alternative as a “thermal engine”, “power generation device”, “waste heat recovery system” and “heat recovery system”, “heat to electricity system”) of the present disclosure utilizes a thermodynamic cycle which has elements of the Rankine thermodynamic cycle in combination with selected working fluid(s), such as carbon dioxide, to produce power from a wide range of thermal sources. By “thermal engine” or “heat engine” what is generally referred to is the equipment set that executes the thermodynamic cycle described herein; by “heat recovery system” what is generally referred to is the thermal engine in cooperation with other equipment to deliver heat (from any source) to and remove heat from the inventive thermal engine.
The thermodynamic cycle executed by the heat engine 100 is described with reference to a pressure-enthalpy diagram for a selected working fluid,
The thermodynamic cycle that is executed by the thermal engine is shown in its most rudimentary form in
In the preferred embodiment of the thermal engine, the cycle is executed during normal, steady state operation such that the low pressure side of the system (points A and D on
In a preferred embodiment of the thermal engine, the working fluid is carbon dioxide. The use of the term carbon dioxide is not intended to be limited to carbon dioxide of any particular type, purity or grade of carbon dioxide although industrial grade carbon dioxide is the preferred working fluid. Carbon dioxide is a neutral working fluid that offers benefits such as non-toxicity, non-flammability, easy availability, and low price.
In the preferred embodiment, the working fluid is in a supercritical state over certain portions of the system (the “high pressure side”), and in a subcritical state at other portions of the system (the “low pressure side”). In other embodiments, the entire cycle may be operated such that the working fluid is in a supercritical or subcritical state during the entire execution of the cycle.
In various embodiments, the working fluid may a binary, ternary or other working fluid blend. The working fluid combination would be selected for the unique attributes possessed by the fluid combination within a heat recovery system as described herein. For example, one such fluid combination is comprised of a liquid absorbent and carbon dioxide enabling the combined fluid to be pumped in a liquid state to high pressure with less energy input than required to compress CO2. In another embodiment, the working fluid may be a combination of carbon dioxide and one or more other miscible fluids. In other embodiments, the working fluid may be a combination of carbon dioxide and propane, or carbon dioxide and ammonia.
One of ordinary skill in the art would recognize that using the term “working fluid” is not intended to limit the state or phase of matter that the working fluid is in. In other words, the working fluid may be in a fluid phase, a gas phase, a supercritical phase, a subcritical state or any other phase or state at any one or more points within the cycle.
The inventive heat to electricity system may utilize other fluids in other parts of the system, such as water, thermal oils or suitable refrigerants; these other fluids may be used within heat exchangers and equipment external to the heat engine 100 (such as at the Cooler 12 and/or Waste Heat Exchanger 5 shown in
As further described, in one representative embodiment, a 250 kW (net) or greater skid-based system, as illustrated conceptually in
The heat engine 100 of the disclosure has three primary classes of equipment through which the working fluid may be circulated as the thermodynamic cycle is executed, (i) one or more heat exchangers (ii) one or more pumps and/or compressors and (iii) one or more expansion (work) devices (such as a turbine, a ramjet, or a positive displacement expander 3 such as a geroler or gerotor). Each of these pieces of equipment is operatively coupled in the cycle as shown on
The heat engine 100 may also include a means for converting mechanical energy from the one or more expansion devices into electricity; such means may include but are not limited to a generator, alternator 2, or other device(s) and related power conditioning or conversion equipment or devices.
In one embodiment, certain components of the heat engine 100 may share common elements such as in the case of a turboalternator (shown on
The heat engine 100 may also include other equipment and instruments such as sensors, valves (which may be on/off or variable), fittings, filters, motors, vents, pressure relief equipment, strainers, suitable conduit, and other equipment and sensors. The preferred heat engine 100 includes the additional equipment shown on
The preferred heat engine 100 also includes a system for managing the amount of working fluid within the system such as the mass management system disclosed on
The preferred heat engine 100 also includes a control system and related equipment allowing for the automated and/or semi-automated operation of the engine, the remote control of the system and/or the monitoring of system performance.
The preferred heat engine 100 also includes one or more cooling cycle systems to remove heat from and/or provide thermal management to one or more of the expansion device, the electrical producing means and/or the power electronics 1. In the preferred embodiment, there is provided a cooling cycle shown on
The system of the current invention is flexible and may utilize many different types of conventional heat exchangers. The preferred embodiment of the inventive heat engine system 100 utilizes one or more printed circuit heat exchangers (PCHE) or other construction of the heat exchanger, recuperator or cooler components, each of which may contain one or more cores where each core utilizes microchannel technology.
As used hereinand known in the art, “microchannel technology” includes, but is not limited to, heat exchangers that contain one or more microchannels, mesochannels, and/or minichannels. As used herein the terms “microchannels,” “mesochannels,” and/or “minichannels” are utilized interchangeably. Additionally, the microchannels, mesochannels, and/or minichannels of the present invention are not limited to any one particular size, width and/or length. Any suitable size, width or length can be utilized depending upon a variety of factors. Furthermore, any orientation of the microchannels, mesochannels, and/or minichannels can be utilized in conjunction with the various embodiments of the present invention.
The expansion device (also referred to herein as an “expander”) may be a valve or it may be a device capable of transforming high temperature and pressure fluid into mechanical energy. The expansion device may have an axial or radial construction; it may be single or multi-staged. Examples include a geroler, a gerotor, other types of positive displacement devices such as a pressure swing, a turbine, or any other device capable of transforming a pressure or pressure/enthalpy drop in a working fluid into mechanical energy.
In a preferred embodiment, the device is a turboalternator wherein the turbine is operatively coupled to the alternator 2 by either (i) sharing a single shalt, such as by a shaft 62 depicted in
Among other differentiating attributes of the preferred turboalternator are its single axis design, its ability to deliver high isentropic efficiency (>70%), that it operates at high rotational speeds (>20K rpm), that its bearings are either not lubricated during operation or lubricated during operation only by the working fluid, and its capability of directly coupling a high speed turbine and alternator 2 for optimized system (turboalternator) efficiency. In the preferred embodiment, the turboalternator uses air-foil bearings; air foil bearings are selected as the preferred design due because they reduce or eliminate secondary systems and eliminate the requirement for lubrication (which is particularly important when working with the preferred working fluid, carbon dioxide). However, hydrostatic bearings, aerostatic bearings, magnetic bearings and other bearing types may be used.
The heat engine 100 also provides for the delivery of a portion of the working fluid into the expander 3 chamber (or housing) for purposes of cooling one or more parts of the expander 3. In a preferred embodiment, due to the potential need for dynamic pressure balancing within the preferred heat engine's turboalternator, the selection of the site within the thermal engine from which to obtain this portion of the working fluid is critical because introduction of the portion of the working fluid into the turboalternator must not disturb the pressure balance (and thus stability) of the turboalternator during operation. This is achieved by matching the pressure of the working fluid delivered into the turboalternator for purposes of cooling with the pressure of the working fluid at the inlet of the turbine; in the preferred heat engine 100, this portion of the working fluid is obtained after the working fluid passes a valve 25 and a filter F4. The working fluid is then conditioned to be at the desired temperature and pressure prior to being introduced into the turboalternator housing. This portion of the working fluid exits the turboalternator at the turboalternator outlet. A variety of turboalternator designs are capable of working within the inventive system and to achieve different performance characteristics.
The device for increasing the pressure of the working fluid from point A-B on
The pump 9 and a pump motor 8 may be coupled to a VFD (variable frequency drive) 11 to control speed which in turn can be used to control the mass flow rate of the working fluid in the system, and as a consequence, control the high pressure side system pressure. The VFD 11 may be in communication with a control system, as further described.
In another embodiment of the inventive thermal engine, as depicted in
The electrical producing means of one embodiment of the thermal engine is a high speed alternator 2 that is operatively coupled to the turbine to form a turboalternator (as described above). The electrical producing means may alternatively be any known means of converting mechanical energy into electricity including a generator or alternator 2. It may be operatively coupled to the primary system expander 3 by a gear box, by sharing a common shaft, or by any other mechanical connection.
The electrical producing means is operatively connected to power electronics 1 equipment set. In the preferred embodiment, the electrical output of the alternator 2 is mated with a high efficiency power electronics 1 equipment set that has equipment to provide active load adjustment capability (0-100%). In the preferred embodiment, the power electronics 1 system has equipment to provide the capability to convert high frequency, high voltage power to grid-tie quality power at appropriate conditions with low total harmonic distortion (THD), SAG support, current and voltage following, VAR compensation, for providing torque to start the turboalternator, and dynamic braking capability for versatile and safe control of the turboalternator in the event of load loss; it has also capability of synchronizing and exporting power to the grid for a wide voltage and speed range of the alternator 2.
In the preferred embodiment, the pump 9 inlet pressure has a direct influence on the overall system efficiency and the amount of power that can be generated. Because of the thermo-physical properties of the preferred working fluid, carbon dioxide, as the pump 9 inlet temperature rises and falls the system must control the inlet pressure over wide ranges of inlet pressure and temperature (for example, from −4 deg F. to 104 deg F.; and 479 psia to 1334 psia). In addition, if the inlet pressure is not carefully controlled, pump 9 cavitation is possible.
A mass management system is provided to control the inlet pressure at the pump 9 by adding and removing mass from the system, and this in turn makes the system more efficient. In the preferred embodiment, the mass management system operates with the system semi-passively. The system uses sensors to monitor pressures and temperatures within the high pressure side (from pump 9 outlet to expander 3 inlet) and low pressure side (from expander 3 outlet to pump 9 inlet) of the system. The mass management system may also include valves, tank heaters or other equipment to facilitate the movement of the working fluid into and out of the system and a mass control tank 7 for storage of working fluid.
As shown on
In the preferred embodiment of the system, the Mass Control Tank 7 is filled with working fluid. It is in fluid communication with valves 14 and 16 such that opening either or both valves 14,16 will deliver working fluid to the top of the Mass Control Tank 7. The Mass Control Tank 6 is in fluid communication with valve 15 such that opening valve 15 will remove working fluid from the bottom of the Mass Control Tank 7. The working fluid contained within the Mass Control Tank 7 will stratify with the higher density working fluid at the bottom of the tank and the lower density working fluid at the top of the tank. The working fluid may be in liquid phase, vapor phase or both; if the working fluid is in both vapor phase and liquid phase, there will be a phase boundary separating one phase of working fluid from the other with the denser working fluid at the bottom of the Mass Control Tank 7. In this way, valve 15 will also deliver to the system the densest working fluid within the Mass Control Tank 7.
In the case of the preferred embodiment, this equipment set is combined with a set of sensors within the main heat engine system 100 and a control system as described within.
In the case of the preferred embodiment, this mass management system also includes equipment used in a variety of operating conditions such as start up, charging, shut-down and venting the heat engine system 100 as shown on
Exemplary operation of the preferred embodiment of the mass control management system follows. When the working fluid in the mass control tank 7 is at vapor pressure for a given ambient temperature, and the low side pressure in the system is above the vapor pressure, the pressure in the mass control tank 7 must be increased, to allow for the addition of mass into the system. This can be controlled by opening the valve 14 and thereby allowing higher pressure, higher temperature, lower density supercritical working fluid to flow into the mass control tank 7. Valve 15 is opened to allow higher density liquid working fluid at the bottom of the mass control tank 7 to flow into the system and increase pump 9 suction pressure.
The working fluid may be in liquid phase, vapor phase or both. If the working fluid is in both vapor phase and liquid phase, there will be a phase boundary in the mass control tank 7. In general, the mass control tank 7 will contain either a mixture of liquid and vapor phase working fluid, or a mass of supercritical fluid. In the former case, there will be a phase boundary. In the latter case, there will not be a phase boundary (because one does not exist for supercritical fluids). The fluid will still tend to stratify however, and the valve 15 can be opened to allow higher density liquid working fluid at the bottom of the mass control tank 7 to flow into the system and increase pump suction pressure. Working fluid mass may be added to or removed from the working fluid circuit via the mass control tank 7.
The mass management system of the disclosure may be coupled to a control system such that the control of the various valves and other equipment is automated or semi-automated and reacts to system performance data obtained via sensors located throughout the system, and to ambient and environmental conditions.
Other configurations for controlling pressure and/or temperature (or both) in the mass control tank 7 in order to move mass in and out of the system (i.e., the working fluid circuit), include the use of a heater and/or a coil within the vessel/tank or any other means to add or remove heat from the fluid/vapor within the mass control tank 7. Alternatively, mechanical means, such as providing pump may be used to get working fluid from the mass control tank 7 into the system.
One method of controlling the pressure of the working fluid in the low side of the working fluid circuit is by control of the temperature of the working fluid vessel or mass control tank 7. A basic requirement is to maintain the pump 9 inlet pressure above the boiling pressure at the pump 9 inlet. This is accomplished by maintaining the temperature of the mass control tank 7 at a higher level than the pump 9 inlet temperature. Exemplary methods of temperature control of the mass control tank 7 are: direct electric heat; a heat exchanger coil with pump 9 discharge fluid (which is at a higher temperature than at the pump 9 inlet), or a heat exchanger coil with spent cooling water from the cooler/condenser (also at a temperature higher than at the pump 9 inlet).
As shown in
Also included on or off the skid, or otherwise in fluid or thermal communication with the working fluid circuit of the system, is at least one waste heat exchanger (WHE) 5 (also shown in
Supercritical working fluid exits the pump 9 and flows to the recuperator (REC) 6, where it is preheated by residual heat from the low pressure working fluid. The working fluid then travels to the waste heat exchanger (WHE) 5. From WHE 5, the working fluid travels to the expander (EXP) 3. On the downstream side of the EXP 3, the working fluid is contained in a low pressure side of the cycle. From the EXP 3 the working fluid travels through the REC 6, then to the cooler 12 and then back to the Pump 9.
Suitable pressure and temperature monitoring at points along the lines and at the components is provided and may be integrated with an automated control system.
A control system can be provided in operative connection with the inventive heat engine system 100 to monitor and control the described operating parameters, including but not limited to: temperatures, pressures (including port, line and device internal pressures), flow metering and rates, port control, pump operation via the VFD, fluid levels, fluid density leak detection, valve status, filter status, vent status, energy conversion efficiency, energy output, instntmentation, monitoring and adjustment of operating parameters, alarms and shut-offs.
As further described, a representative control system may include a suitably configured programmable logic controller (PLC) with inputs from the described devices, components and sensors and output for control of the operating parameters. The control system may be integral with and mounted directly to the inventive heat engine 100 or remote, or as part of distributed control system and integrated with other control systems such as for an electrical supply grid. The control system is programmable to set, control or change any of the various operating parameters depending upon the desired performance of the system. Operating instrumentation display may be provided as a composite dashboard screen display of the control system, presenting textual and graphic data, and a virtual display of the inventive heat engine 100 and overall and specific status. The control system may further include capture and storage of heat engine 100 operational history and ranges of all parameters, with query function and report generation.
A control system and control logic for a 250 kW nominally net power rated Thermafficient Heat Engine 100 of the disclosure may include the following features, functions and operation: automated unmanned operation under a dedicated control system; local and remote human machine interface capability for data access, data acquisition, unit health monitoring and operation; controlled start-up, operation and shut down in the case of a loss of electrical incoming supply power or power export connection; fully automated start/stop, alarm, shut down, process adjustment, ambient temperature adjustment, data acquisition and synchronization; a controls/power management system designed for interfacing with an external distributed plant control system.
An exemplary control system for the thermafficient heat engine 100 may have multiple control states as depicted in
As represented in
The invention thus disclosed in sufficient particularity as to enabling an understanding by those of skill in the art, the following claims encompassing all of the concepts, principles and embodiments thus described, and all equivalents.
This application is a conversion of U.S. Provisional patent application No. 61/243,200, filed Sep. 17, 2009.
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Number | Date | Country | |
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20110185729 A1 | Aug 2011 | US |
Number | Date | Country | |
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61243200 | Sep 2009 | US |