Basic refrigeration systems cool a target fluid circulating through an evaporator where the latent heat of vaporization of a working fluid is obtained from the sensible heat of the target fluid, thereby reducing the temperature of the target fluid. In order for the working fluid to evaporate, the working fluid must first be in a liquid state at a pressure below the vapor pressure of the working fluid. In typical refrigeration cycles, this liquid state is obtained by compressing the working fluid to a high pressure and temperature, rejecting the thermal energy to the environment either by conduction or convection, and then passing the working fluid through a throttling valve to reduce the pressure of the working fluid in an isenthalpic expansion. The resulting liquid working fluid is then evaporated in the evaporator by absorbing thermal energy from the target fluid. The evaporated working fluid is then returned to the compressor to complete the cycle.
One disadvantage to this type of refrigeration system is that the compression system requires power in the form of expensive mechanical energy. An alternate way of compressing the working fluid is through the use of an ejector which uses a high pressure and temperature motive fluid to entrain the working fluid (e.g., a suction fluid) after the working fluid has been discharged from the evaporator. The fluid mixture discharged from the ejector follows the conventional refrigeration cycle before being re-entrained into the ejector by additional, high temperature motive fluid.
Although there are several types of refrigeration cycles that employ ejectors, it nonetheless remains desirable to find improved refrigeration cycles in varying thermodynamic applications that offer improved efficiency and reduction in production costs.
Embodiments of the disclosure may provide a working fluid circuit for converting thermal energy into mechanical energy and/or electrical energy. The working fluid circuit may include a pump configured to circulate a working fluid through the working fluid circuit. A heat exchanger may be in fluid communication with the pump and in thermal communication with a heat source, and the heat exchanger may be configured to transfer thermal energy from the heat source to the working fluid. A condenser may be fluidly coupled to the pump and configured to cool the working fluid before returning to the pump for recirculation. An ejector may be fluidly coupled to the heat exchanger and configured to receive a motive fluid and a suction fluid. The motive fluid may be a portion of the working fluid discharged from the heat exchanger and the suction fluid may be a portion of the working fluid discharged from the condenser, and the ejector may discharge a mixed fluid into or adjacent an inlet of the condenser. An expansion valve may be fluidly coupled to the condenser and configured to receive and expand the suction fluid. An evaporator may be in fluid communication with the expansion valve and have a target fluid circulating therein. The evaporator may be configured to transfer thermal energy from the target fluid to the suction fluid such that the target fluid is cooled.
Embodiments of the disclosure may also provide a method for cooling a target fluid. The method may include circulating a working fluid through a working fluid circuit with a pump. The working fluid may be heated in a heat exchanger arranged in the working fluid circuit in fluid communication with the pump, and the heat exchanger may be in thermal communication with a waste heat source. The working fluid may be cooled with a condenser arranged in the working fluid circuit upstream from and fluidly coupled to the pump. A portion of the working fluid discharged from the heat exchanger may be extracted to be used as a motive fluid in an ejector, and the ejector may be fluidly coupled to the heat exchanger. A portion of the working fluid discharged from the condenser may be extracted to be used as a suction fluid in the ejector. The suction fluid may be expanded in an expansion valve to generate a cooled suction fluid, and the expansion valve may be fluidly coupled to the condenser. The target fluid may be cooled with the cooled suction fluid in an evaporator fluidly coupled to the expansion valve.
Embodiments of the disclosure may further provide a refrigeration cycle, such as a jet pump refrigeration cycle containing or otherwise utilizing a working fluid containing carbon dioxide. The refrigeration cycle may include an ejector fluidly coupled to a heat exchanger arranged in a working fluid circuit and configured to receive a motive fluid from the heat exchanger. The heat exchanger may be configured to transfer thermal energy from a waste heat source to a working fluid containing carbon dioxide circulating throughout the working fluid circuit, and the motive fluid is a portion of the working fluid discharged from the heat exchanger. A condenser may be arranged in the working fluid circuit and fluidly coupled to a discharge of the ejector, and the condenser may be configured cool the working fluid in the working fluid circuit and simultaneously cool a mixed fluid discharged from the ejector. An expansion valve may be fluidly coupled to the condenser and configured to receive and expand a suction fluid to generate a cooled suction fluid. The suction fluid may be a portion of the working fluid discharged from the condenser and subsequently entrained into the ejector to form part of the mixed fluid. An evaporator may be in fluid communication with the expansion valve and have a target fluid circulating therein. The evaporator may be configured to transfer thermal energy from the target fluid to the suction fluid such that the target fluid is cooled and the suction fluid evaporates. An upstream source may be fluidly coupled to the evaporator and provide the target fluid to the evaporator.
Embodiments of the present disclosure is best understood from the following detailed description when read with the accompanying Figures. It is emphasized that, in accordance with the standard practice in the industry, various features are not drawn to scale. In fact, the dimensions of the various features may be arbitrarily increased or reduced for clarity of discussion.
It is to be understood that the present disclosure describes several exemplary embodiments for implementing different features, structures, or functions of the invention. Exemplary embodiments of components, arrangements, and configurations are described below to simplify the present disclosure, however, these exemplary embodiments are provided merely as examples and are not intended to limit the scope of the invention. Additionally, the present disclosure may repeat reference numerals and/or letters in the various exemplary embodiments and across the Figures provided herein. This repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various exemplary embodiments and/or configurations discussed in the various Figures. Moreover, the formation of a first feature over or on a second feature in the description that follows may include embodiments in which the first and second features are formed in direct contact, and may also include embodiments in which additional features may be formed interposing the first and second features, such that the first and second features may not be in direct contact. Finally, the exemplary embodiments presented below may be combined in any combination of ways, i.e., any element from one exemplary embodiment may be used in any other exemplary embodiment, without departing from the scope of the disclosure.
Additionally, certain terms are used throughout the present disclosure and claims to refer to particular components. As one skilled in the art will appreciate, various entities may refer to the same component by different names, and as such, the naming convention for the elements described herein is not intended to limit the scope of the invention, unless otherwise specifically defined herein. Further, the naming convention used herein is not intended to distinguish between components that differ in name but not function. Further, in the present disclosure and in the claims, the terms “including” and “comprising” are used in an open-ended fashion, and thus should be interpreted to mean “including, but not limited to”. All numerical values in this disclosure may be exact or approximate values unless otherwise specifically stated. Accordingly, various embodiments of the disclosure may deviate from the numbers, values, and ranges disclosed herein without departing from the intended scope. Furthermore, as it is used in the claims or specification, the term “or” is intended to encompass both exclusive and inclusive cases, i.e., “A or B” is intended to be synonymous with “at least one of A and B,” unless otherwise expressly specified herein.
The working fluid circuit 100 may operate as a closed-loop thermodynamic cycle that circulates a working fluid throughout a variety of conduits adapted to interconnect the various components of the working fluid circuit 100. The working fluid circuit 100 in
In one or more embodiments, the working fluid used in the working fluid circuit 100 may be or contain carbon dioxide (CO2), but not limited to carbon dioxide of any particular type, purity, or grade. For example, industrial grade carbon dioxide may be used without departing from the scope of the disclosure. In many examples, the working fluid contained within the working fluid circuit 100 contains carbon dioxide and may be in a supercritical state in at least one portion of the working fluid circuit. In other embodiments, the working fluid may be a binary, ternary, or other working fluid combination. One such fluid combination includes a liquid absorbent and carbon dioxide mixture enabling the combination to be pumped in a liquid state to high pressure with less energy input than required to compress carbon dioxide independently. In yet other embodiments, the working fluid may be a combination of carbon dioxide and one or more other miscible fluids. In yet other embodiments, the working fluid may be a combination of carbon dioxide and propane, or carbon dioxide and ammonia, without departing from the scope of the disclosure.
Use of the term “working fluid” is not intended to limit the state or phase of matter that the working fluid is in at any point in the working fluid circuit 100. For instance, the working fluid may be in a fluid phase, a gas phase, a supercritical state, a subcritical state or any other phase or state at any one or more points within the working fluid circuit 100 or thermodynamic cycle. In one or more embodiments, the working fluid is in a supercritical state over certain portions of the working fluid circuit 100 (e.g., a high pressure side) and in a subcritical state at other portions of the working fluid circuit 100 (e.g., a low pressure side). In many examples, the working fluid contains carbon dioxide, the working fluid is in a supercritical state (e.g., sc-CO2) contained within the high pressure side of the working fluid circuit 100, and the working fluid is in a subcritical state (e.g., sub-CO7) contained within the low pressure side of the working fluid circuit 100. In other embodiments, the entire thermodynamic cycle may be operated such that the working fluid is maintained in either a supercritical or subcritical state throughout the entire working fluid circuit 100.
In some embodiments, the high pressure side of the working fluid circuit 100 contains the working fluid (e.g., sc-CO2) at a pressure of greater than 15 MPa, such as about 20 MPa or greater. For example, the high pressure side of the working fluid circuit 100 may have a pressure within a range from about 20 MPa to about 30 MPa, more narrowly within a range from about 21 MPa to about 25 MPa, and more narrowly within a range from about 22 MPa to about 24 MPa, such as about 23 MPa. The low pressure side of the working fluid circuit 100 contains the working fluid (e.g., sub-CO2) at a pressure of less than 15 MPa, such as about 10 MPa or less. For example, the low pressure side of the working fluid circuit 100 may have a pressure within a range from about 2 MPa to about 10 MPa, more narrowly within a range from about 4 MPa to about 8 MPa, and more narrowly within a range from about 5 MPa to about 7 MPa, such as about 6 MPa.
A main pump 102 may be utilized to pressurize and circulate the working fluid within the working fluid circuit 100. In one embodiment, the main pump 102 is driven by a motor 103 or other comparable driving mechanism. The working fluid is directed through a heat exchanger 104 configured to increase the temperature of the working fluid. The heat exchanger 104 is in thermal communication with a heat source Qin which may derive thermal energy from a variety of high temperature sources.
For example, the heat source Qin may be a waste heat stream such as, but not limited to, gas turbine exhaust, process stream exhaust, or other combustion product exhaust streams, such as furnace or boiler exhaust streams. Accordingly, the working fluid circuit 100 may be configured to transform waste heat into electricity for applications ranging from bottom cycling in gas turbines, stationary diesel engine gensets, industrial waste heat recovery (e.g., in refineries and compression stations), and hybrid alternatives to the internal combustion engine. In some examples, the heat source Qin is a waste heat stream and the heat exchanger 104 is a waste heat exchanger. In other embodiments, the heat source Qin may derive thermal energy from renewable sources of thermal energy such as, but not limited to, solar thermal and geothermal sources.
While the heat source Qin may be a fluid stream of the high temperature source, in other embodiments the heat source Qin may be a thermal fluid that is in contact with the high temperature source. The thermal fluid may deliver the thermal energy to the heat exchanger 104 to transfer the energy to the working fluid in the working fluid circuit 100.
A first expansion device 106 is arranged downstream from the heat exchanger 104 for receiving and expanding the heated working fluid discharged from the heat exchanger 104. The first expansion device 106 may be any type of expansion device, such as an expander or a turbine, and may be operatively coupled to a work-producing device 108. The work-producing device 108 may be a pump, a compressor, an electrical generator, either coupled by a gearbox or directly driving corresponding high-speed alternators, or combinations thereof. The first expansion device 106 may be operable to discharge the working fluid into a first recuperator fluidly coupled downstream thereof. The first recuperator 110 may be configured to transfer residual thermal energy from the working fluid discharged from the first expansion device 106 to the working fluid discharged from the main pump 102. The working fluid discharged from the first recuperator 110 is then returned to a lower temperature state at a condenser 112 and then returned to the main pump 102 to commence the cycle anew.
The refrigeration cycle 114 may be fluidly coupled to the working fluid circuit 100 at one or more locations and adapted to use a portion of the working fluid circulating in the working fluid circuit 100 to cool a target fluid for use in a separate system or duty. The refrigeration cycle 114 may include an ejector 116 fluidly coupled to the working fluid circuit 100 via a first conduit 118, where the first conduit 118 redirects a portion of the working fluid to be used as a motive fluid for the ejector 116. As illustrated, the first conduit 118 may be tied into the working fluid circuit 100 at a location downstream from the heat exchanger 104 but prior to the first expansion device 106. Consequently, the motive fluid directed to the ejector 116 is working fluid discharged from the heat exchanger 104 at a generally high temperature and pressure.
The ejector 116 converts the pressure energy of the motive fluid into velocity energy, thereby creating a low pressure zone within the ejector 116. The low pressure zone effectively entrains a suction fluid into the ejector 116 via a second conduit 120 fluidly coupled thereto. As the mixed fluid (e.g., the motive fluid mixed with the suction fluid) traverses the ejector 116, the mixed fluid expands and the velocity is reduced, which has the effect of recompressing the mixed fluid by converting the velocity energy back into pressure energy. The mixed fluid discharged from the ejector 116 into a third conduit 122 which may be fluidly coupled to the working fluid circuit 100 upstream from the condenser 112, such as adjacent the inlet to the condenser 112.
The suction fluid entrained into the ejector 116 may also be obtained from the working fluid circuit 100 by redirecting a fraction of the working fluid downstream from the condenser 112 into a fourth conduit 124. An expansion valve 126 is arranged in the fourth conduit 124 for expanding the suction fluid extracted from the working fluid circuit 100. The expansion valve 126 may be any device adapted to expand a fluid, such as, but not limited to, a valve, an expander, a turbine, or the like. Expanding the suction fluid with the expansion valve 126 reduces the pressure and temperature of the suction fluid, and results in a suction fluid that is primarily in a liquid state. As can be appreciated, the resulting pressure and temperature of the suction fluid can be selectively varied by adjusting, positioning, or otherwise varying the relative position of the expansion valve 126 between open and closed positions.
The liquid suction fluid may then be directed through an evaporator 128 fluidly coupled to the discharge of the expansion valve 126. The evaporator 128 serves to transfer thermal energy between the suction fluid and a target fluid originating from an upstream source 130 such that the target fluid is cooled. The target fluid may be directed to the evaporator 128 via a fifth conduit 132. The evaporator 128 transfers thermal energy from the target fluid to the suction fluid, thereby reducing the temperature of the target fluid and simultaneously increasing the enthalpy of the suction fluid although the temperature of the suction fluid may or may not increase. Increasing the enthalpy of the suction fluid may cause the suction fluid to evaporate before the suction fluid is entrained into the ejector 116, as described above. The cooled target fluid may be discharged from the evaporator 128 and used or otherwise employed in a separate downstream system or the duty 134, such as another heat exchanging device of a downstream application that requires the use of cooled water.
In one or more embodiments, the target fluid may be a liquid or a gas, or any other known thermal fluid or heat transfer fluid. For example, the target fluid may be air, water, or a mixture of glycol and water. Although the upstream source 130 is shown as providing both the target fluid via the fifth conduit 132 and the coolant for the condenser 112, it may be appreciated that the coolant for the condenser 112 may originate from a different source, and thus, not be in fluid communication with the target fluid. After cooling the working fluid passing through the condenser 112, the coolant water may be directed to a cooling water return 136.
Referring now to
The first mass flow m1 is directed though the heat exchanger 104 and subsequently expanded in the first expansion device 106, as described above. The first expansion device 106 discharges the first mass flow m1 into the first recuperator 110 fluidly coupled downstream thereof. The first recuperator 110 may be configured to transfer residual thermal energy in the first mass flow m1 to the second mass flow m2 which also passes through the first recuperator 110. Consequently, the temperature of the first mass flow m1 is decreased and the temperature of the second mass flow m2 is increased. The second mass flow m2 may be subsequently expanded in a second expansion device 204. The second expansion device 204 may be any type of expansion device, such as an expander or a turbine.
In one embodiment, the second expansion device 204 is operatively coupled to a second work-producing device 210, which may be similar to the work-producing device 108 described above. For example, the second work-producing device 210 may be a pump, a compressor, an electrical generator, either coupled by a gearbox or directly driving corresponding high-speed alternators, or combinations thereof. In other embodiments, the second work-producing device 210 may be omitted and the second expansion device 204 may be operatively coupled to the main pump 102 via a shaft 205. Accordingly, the main pump 102 may be driven by expansion of the second mass flow m2 in the second expansion device 204.
The second expansion device 204 discharges the second mass flow m2 into a second recuperator 206 fluidly coupled downstream thereof. The second recuperator 206 may be configured to transfer residual thermal energy from the second mass flow m2 to the combined working fluid m1+m2 discharged from the main pump 102 and passing through the second recuperator 206. The mass flows m1, m2 discharged from each recuperator 110, 206, respectively, are recombined at point 208 in the working fluid circuit 200 and then returned to a lower temperature state at the condenser 112. After passing through the condenser 112, the combined working fluid m1+m2 is returned to the main pump 102 and the cycle is started anew.
The refrigeration cycle 114 is coupled to the working fluid circuit 200 adjacent the discharge of the heat exchanger 104 and directs motive fluid to the ejector 116 via the first conduit 118. The suction fluid derived from the second conduit 120 again originates from the working fluid circuit 200 at a location downstream from the condenser 112 via a fourth conduit 124. The third conduit 122 receives the mixed fluid as the mixed fluid is discharged from the ejector 116 and injects the mixed fluid into the working fluid circuit 200 upstream from the condenser 112, such as adjacent the inlet to the condenser 112.
Operation of the expansion valve 126 and the evaporator 128 in conjunction with the target fluid derived from the upstream source 130 is substantially similar as described above with reference to
After expansion in the second expansion device 204, the second mass flow m2 may be re-combined with the first mass flow m1 at point 304. The combined working fluid m1+m2 may then transfer thermal energy to the second mass flow m2 via the first recuperator 110 prior to the second mass flow m2 passing through the second recuperator 206, as described above. The combined working fluid m1+m2 is cooled via the first recuperator 110 and subsequently directed to the condenser 112 for additional cooling, after which the working fluid is generally returned to the main pump 102 where the cycle starts anew.
As with prior embodiments, the refrigeration cycle 114 is coupled to the working fluid circuit 300 adjacent the discharge of the heat exchanger 104 to provide high temperature and pressure motive fluid to the ejector 116 via the first conduit 118. The suction fluid derived from the second conduit 120 again originates from the working fluid circuit 300 at a location downstream from the condenser 112 via the fourth conduit 124. The third conduit 122 receives the mixed fluid discharged from the ejector 116 and injects the mixed fluid into the working fluid circuit 300 upstream from the condenser 112, such as adjacent the inlet to the condenser 112.
Operation of the expansion valve 126 and the evaporator 128 in conjunction with the target fluid derived from the upstream source 130 is comparable to the embodiments described above with reference to
Referring now to
As illustrated, the heat exchangers 402, 404 are arranged in series within the heat source Qin, but in parallel in the working fluid circuit 400. The first heat exchanger 402 may be fluidly coupled to the first expansion device 106 and the second heat exchanger 404 may be fluidly coupled to the second expansion device 204. In turn, the first expansion device 106 is fluidly coupled to the first recuperator 110 and the second expansion device 204 is fluidly coupled to the second recuperator 206. The recuperators 110, 206 may be arranged in series on a low temperature side of the working fluid circuit 400 and in parallel on a high temperature side of the working fluid circuit 400. For example, the high temperature side of the working fluid circuit 400 includes the portions of the working fluid circuit 400 arranged downstream from each recuperator 110, 206 where the working fluid is directed to the heat exchangers 402, 404. The low temperature side of the working fluid circuit 400 includes the portions of the working fluid circuit 400 downstream from each recuperator 110, 206 where the working fluid is directed away from the heat exchangers 402, 404.
The main pump 102 may be operatively coupled to the second expansion device 204 via the shaft 205 (indicated by the dashed line), but in other embodiments the main pump 102 is driven by the motor 103, as described above. In embodiments where the second expansion device 204 drives the main pump 102 via the shaft 205, a starter pump 406 may be included in the working fluid circuit 400 to facilitate the start sequence for the combination of the main pump 102 and second expansion device 204 (e.g., a combination turbopump). The starter pump 406 may be driven primarily by an auxiliary motor 408, and once steady-state operation of the second expansion device 204 is reached, the starter pump 406 may be deactivated.
The first expansion device 106 may operate at a higher relative temperature (e.g., higher inlet temperature) than the second expansion device 204, due to the temperature drop of the heat source Qin realized across the first heat exchanger 402. Each expansion device 106, 204, however, may be configured to operate at the same or substantially the same inlet pressure. The low-pressure discharge mass flow exiting each recuperator 110, 206 may be directed to the condenser 112 to be cooled for return to either the main pump 102 or the starter pump 406, depending on the stage of operation.
During steady-state operation, the main pump 102 circulates the working fluid throughout the working fluid circuit 400, and the working fluid is separated into the first and second mass flows m1, m2 at point 410. The first mass flow m1 is directed through the first heat exchanger 402 and subsequently expanded in the first expansion device 106. Following the first expansion device 106, the first mass flow m1 passes through the first recuperator 110 and transfers residual thermal energy to the first mass flow m1 as the first mass flow m1 is directed toward the first heat exchanger 402.
The second mass flow m2 is directed through the second heat exchanger 404 and subsequently expanded in the second expansion device 204. Following the second expansion device 204, the second mass flow m2 passes through the second recuperator 206 to receive residual thermal energy from the second mass flow m2 coursing towards the second heat exchanger 404. The second mass flow m2 is then re-combined with the first mass flow m1 and the combined mass flow m1+m2 is subsequently cooled in the condenser 112 and directed back to the main pump 102 to commence the working fluid circuit 400 anew.
The refrigeration cycle 114 is coupled to the working fluid circuit 400 adjacent the discharge of the first heat exchanger 402 to provide high temperature and pressure motive fluid to the ejector 116 via the first conduit 118. In other embodiments, the first conduit 118 may be coupled to the working fluid circuit 400 at or near the discharge of the second heat exchanger 404, without departing from the scope of the disclosure. The suction fluid entrained into the ejector 116 via the second conduit 120 may again originate from the working fluid circuit 400 at a location downstream from the condenser 112 via the fourth conduit 124. The third conduit 122 receives the mixed fluid discharged from the ejector 116 and injects the mixed fluid back into the working fluid circuit 400 at a location upstream from the condenser 112.
Operation of the expansion valve 126 and the evaporator 128 in conjunction with the target fluid derived from the upstream source 130 is substantially similar as described above with reference to
In the working fluid circuit 500, the working fluid is separated into the first mass flow m1 and the second mass flow m2 at a point 502. The first mass flow m1 is eventually directed through the first heat exchanger 402 and subsequently expanded in the first expansion device 106. The first mass flow m1 then passes through the first recuperator 110 to transfer residual thermal energy back to the first mass flow m1 coursing towards the first heat exchanger 402. The second mass flow m2 may be directed through the second heat exchanger 404 and subsequently expanded in the second expansion device 204. Following the second expansion device 204, the second mass flow m2 is merged with the first mass flow m1 at point 504 to generate the combined working fluid flow m1+m2. The combined working fluid flow m1+m2 may be directed through the second recuperator 206 to transfer residual thermal energy to the first mass flow m1 as the fluid passes through the second recuperator 206 on the way to the first recuperator 110.
The arrangement of the recuperators 110, 206 allows the residual thermal energy in the combined working fluid flow m1+m2 to be transferred to the first mass flow m1 in the second recuperator 206 prior to the combined working fluid flow m1+m2 reaching the condenser 112. Following the condenser 112, the working fluid flow m1+m2 returns to the main pump 102 to commence the cycle anew.
Similar to the working fluid circuit 400, the refrigeration cycle 114 may be coupled to the working fluid circuit 500 adjacent the discharge of the first heat exchanger 402 to provide the motive fluid for the ejector 116 via the first conduit 118. In other embodiments, the first conduit 118 may be coupled to the working fluid circuit 400 at or near the discharge of the second heat exchanger 404. The suction fluid entrained into the ejector 116 via the second conduit 120 may originate from the working fluid circuit 500 at a location downstream from the condenser 112 via the fourth conduit 124. The third conduit 122 receives the mixed fluid discharged from the ejector 116 and injects the mixed fluid back into the working fluid circuit 500 at a location upstream from the condenser 112. Operation of the expansion valve 126 and the evaporator 128 in conjunction with the target fluid derived from the upstream source 130 is substantially similar as described above, and therefore will not be described again. As with prior embodiments, the cooled target fluid is discharged from the evaporator 128 and directed to the separate downstream system or the duty 134 requiring cooled target fluid.
During steady-state operation of the working fluid circuit 600, the main pump 102 discharges the working fluid that is subsequently separated into first and second mass flows m1, m2, respectively, at point 604. The third heat exchanger 602 may be configured to transfer thermal energy from the heat source Qin to the first mass flow m1 flowing therethrough. The first mass flow m1 is then directed to the first heat exchanger 402 and the first expansion device 106 for expansion power generation. Following expansion in the first expansion device 106, the first mass flow m1 passes through the first recuperator 110 to transfer residual thermal energy to the first mass flow m1 discharged from the third heat exchanger 602 and coursing towards the first heat exchanger 402.
The second mass flow m2 is directed through the second heat exchanger 404 and subsequently expanded in the second expansion device 204 to optionally drive the main pump 102 via the shaft 205. After being discharged from the second expansion device 204, the second mass flow m2 merges with the first mass flow m1 at point 606. The combined mass flow m1+m2 thereafter passes through the second recuperator 206 to provide residual thermal energy to the second mass flow m2 as the second mass flow m2 courses toward the second heat exchanger 404. The condenser 112 receives the combined mass flow m1+m2 discharged from the second recuperator 206 and the cycle is started anew at the main pump 102.
The refrigeration cycle 114 may be coupled to the working fluid circuit 600 at or adjacent the discharge of the first heat exchanger 402 to provide the motive fluid for the ejector 116 via the first conduit 118. In other embodiments, the first conduit 118 may be coupled to the working fluid circuit 400 at or near the discharge of the second or third heat exchangers 404, 602, respectively, without departing from the scope of the disclosure. The suction fluid entrained into the ejector 116 via the second conduit 120 may originate from the working fluid circuit 600 at a location downstream from the condenser 112 via the fourth conduit 124. The third conduit 122 receives the mixed fluid discharged from the ejector 116 and injects the mixed fluid back into the working fluid circuit 600 at a location upstream from the condenser 112. Operation of the expansion valve 126 and the evaporator 128 in conjunction with the target fluid derived from the upstream source 130 is the same as described above, and the cooled target fluid is discharged from the evaporator 128 to be used in the separate downstream system or the duty 134 requiring cooled target fluid.
In other embodiments, the first mass flow m1 discharged from the third heat exchanger 602 may be directed back through the third recuperator 702 via line 704 before the first mass flow m1 is channeled to the first heat exchanger 402. Accordingly, the temperature of the first mass flow m1 may be increased further prior to receiving thermal energy transferred from the first recuperator 110 and the heat source Qin in the first heat exchanger 402. As illustrated, the recuperators 110, 206, 702 may operate as separate heat exchanging devices. However, in other embodiments, the recuperators 110, 206, 702 may be combined as a single, integral recuperator. Steady-state operation of the working fluid circuit 700, including the integration of the refrigeration cycle 114, may operate substantially similar as described above in
The working fluid is separated into first and second mass flows m1 and m2 at point 802 in the working fluid circuit 800. The first mass flow m1 is eventually directed through the first heat exchanger 402 and subsequently expanded in the first expansion device 106. Upon discharge from the first expansion device 106, the first mass flow m1 passes through the first recuperator 110 to transfer residual thermal energy back to the first mass flow m1 coursing towards the first heat exchanger 402. The second mass flow m2 may be directed through the second heat exchanger 404 and subsequently expanded in the second expansion device 204. Upon discharge from the second expansion device 204, the second mass flow m2 passes through the second recuperator 206 to transfer residual thermal energy back to the second mass flow m2 coursing towards the second heat exchanger 404. The first and second mass flows m1, m2 are re-combined at point 804 to generate the combined working fluid flow m1+m2. The combined working fluid flow m1+m2 may be directed through the condenser 112 and return to the main pump 102 to start the cycle anew.
The refrigeration cycle 114 may be coupled to the working fluid circuit 800 adjacent the discharge of the first heat exchanger 402 to provide the motive fluid for the ejector 116 via the first conduit 118. In other embodiments, the first conduit 118 may be coupled to the working fluid circuit 800 at or near the discharge of the second heat exchanger 404, without departing from the scope of the disclosure. The suction fluid entrained into the ejector 116 via the second conduit 120 may originate from the working fluid circuit 800 at a location downstream from the condenser 112 via the fourth conduit 124. The third conduit 122 receives the mixed fluid discharged from the ejector 116 and injects the mixed fluid back into the working fluid circuit 800 at a location upstream from the condenser 112. Operation of the expansion valve 126 and the evaporator 128 in conjunction with the target fluid derived from the upstream source 130 is substantially similar as described above. As with prior embodiments, the cooled target fluid from the fifth conduit 132 is discharged from the evaporator 128 and directed to the separate downstream system or the duty 134 requiring cooled target fluid.
Each of the described working fluid circuits 100-800 depicted in
A portion of the working fluid discharged from the heat exchanger may be extracted to be used as a motive fluid in an ejector, as at 908. The ejector may be fluidly coupled to the heat exchanger. Also, a portion of the working fluid discharged from the condenser may be extracted to be used as a suction fluid in the ejector, as at 910. The suction fluid may then be expanded in an expansion valve to generate a cooled suction fluid, as at 912. The expansion valve may be fluidly coupled to the condenser. The method 900 may further include cooling the target fluid with the cooled suction fluid in an evaporator, as at 914. The evaporator may be fluidly coupled to the expansion valve.
The foregoing has outlined features of several embodiments so that those skilled in the art may better understand the present disclosure. Those skilled in the art should appreciate that they may readily use the present disclosure as a basis for designing or modifying other processes and structures for carrying out the same purposes and/or achieving the same advantages of the embodiments introduced herein. Those skilled in the art should also realize that such equivalent constructions do not depart from the spirit and scope of the present disclosure, and that they may make various changes, substitutions and alterations herein without departing from the spirit and scope of the present disclosure.
This application claims the benefit of U.S. Appl. No. 61/542,478, filed Oct. 3, 2011, which is hereby incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
2575478 | Wilson | Nov 1951 | A |
2634375 | Guimbal | Apr 1953 | A |
2691280 | Albert | Oct 1954 | A |
3095274 | Crawford | Jun 1963 | A |
3105748 | Stahl | Oct 1963 | A |
3237403 | Feher | Mar 1966 | A |
3277955 | Laszlo | Oct 1966 | A |
3401277 | Larson | Sep 1968 | A |
3622767 | Koepcke | Nov 1971 | A |
3630022 | Jubb | Dec 1971 | A |
3736745 | Karig | Jun 1973 | A |
3772879 | Engdahl | Nov 1973 | A |
3791137 | Jubb | Feb 1974 | A |
3830062 | Morgan et al. | Aug 1974 | A |
3939328 | Davis | Feb 1976 | A |
3971211 | Wethe | Jul 1976 | A |
3982379 | Gilli | Sep 1976 | A |
3998058 | Park | Dec 1976 | A |
4009575 | Hartman, Jr. | Mar 1977 | A |
4029255 | Heiser | Jun 1977 | A |
4030312 | Wallin | Jun 1977 | A |
4049407 | Bottum | Sep 1977 | A |
4070870 | Bahel | Jan 1978 | A |
4099381 | Rappoport | Jul 1978 | A |
4119140 | Cates | Oct 1978 | A |
4150547 | Hobson | Apr 1979 | A |
4152901 | Munters | May 1979 | A |
4164848 | Gilli | Aug 1979 | A |
4164849 | Mangus | Aug 1979 | A |
4170435 | Swearingen | Oct 1979 | A |
4182960 | Reuyl | Jan 1980 | A |
4183220 | Shaw | Jan 1980 | A |
4198827 | Terry et al. | Apr 1980 | A |
4208882 | Lopes | Jun 1980 | A |
4221185 | Scholes | Sep 1980 | A |
4233085 | Roderick | Nov 1980 | A |
4236869 | Laurello | Dec 1980 | A |
4248049 | Briley | Feb 1981 | A |
4257232 | Bell | Mar 1981 | A |
4287430 | Guido | Sep 1981 | A |
4336692 | Ecker | Jun 1982 | A |
4347711 | Noe | Sep 1982 | A |
4347714 | Kinsell | Sep 1982 | A |
4372125 | Dickenson | Feb 1983 | A |
4384568 | Palmatier | May 1983 | A |
4391101 | Labbe | Jul 1983 | A |
4420947 | Yoshino | Dec 1983 | A |
4428190 | Bronicki | Jan 1984 | A |
4433554 | Rojey | Feb 1984 | A |
4439687 | Wood | Mar 1984 | A |
4439994 | Briley | Apr 1984 | A |
4448033 | Briccetti | May 1984 | A |
4450363 | Russell | May 1984 | A |
4455836 | Binstock | Jun 1984 | A |
4467609 | Loomis | Aug 1984 | A |
4467621 | O'Brien | Aug 1984 | A |
4475353 | Lazare | Oct 1984 | A |
4489562 | Snyder | Dec 1984 | A |
4489563 | Kalina | Dec 1984 | A |
4498289 | Osgerby | Feb 1985 | A |
4516403 | Tanaka | May 1985 | A |
4538960 | Iino et al. | Sep 1985 | A |
4549401 | Spliethoff | Oct 1985 | A |
4555905 | Endou | Dec 1985 | A |
4558228 | Larjola | Dec 1985 | A |
4573321 | Knaebel | Mar 1986 | A |
4578953 | Krieger | Apr 1986 | A |
4589255 | Martens | May 1986 | A |
4636578 | Feinberg | Jan 1987 | A |
4674297 | Vobach | Jun 1987 | A |
4694189 | Haraguchi | Sep 1987 | A |
4697981 | Brown et al. | Oct 1987 | A |
4700543 | Krieger | Oct 1987 | A |
4730977 | Haaser | Mar 1988 | A |
4756162 | Dayan | Jul 1988 | A |
4765143 | Crawford | Aug 1988 | A |
4773212 | Griffin | Sep 1988 | A |
4798056 | Franklin | Jan 1989 | A |
4813242 | Wicks | Mar 1989 | A |
4821514 | Schmidt | Apr 1989 | A |
4867633 | Gravelle | Sep 1989 | A |
4892459 | Guelich | Jan 1990 | A |
4986071 | Voss | Jan 1991 | A |
4993483 | Harris | Feb 1991 | A |
5000003 | Wicks | Mar 1991 | A |
5050375 | Dickinson | Sep 1991 | A |
5083425 | Hendriks et al. | Jan 1992 | A |
5098194 | Kuo | Mar 1992 | A |
5102295 | Pope | Apr 1992 | A |
5104284 | Hustak, Jr. et al. | Apr 1992 | A |
5164020 | Wagner | Nov 1992 | A |
5176321 | Doherty | Jan 1993 | A |
5203159 | Koizumi et al. | Apr 1993 | A |
5228310 | Vandenberg | Jul 1993 | A |
5291960 | Brandenburg | Mar 1994 | A |
5320482 | Palmer et al. | Jun 1994 | A |
5335510 | Rockenfeller | Aug 1994 | A |
5358378 | Holscher | Oct 1994 | A |
5360057 | Rockenfeller | Nov 1994 | A |
5392606 | Labinov | Feb 1995 | A |
5440882 | Kalina | Aug 1995 | A |
5444972 | Moore | Aug 1995 | A |
5488828 | Brossard | Feb 1996 | A |
5490386 | Keller | Feb 1996 | A |
5503222 | Dunne | Apr 1996 | A |
5531073 | Bronicki | Jul 1996 | A |
5538564 | Kaschmitter | Jul 1996 | A |
5542203 | Luoma | Aug 1996 | A |
5570578 | Saujet | Nov 1996 | A |
5588298 | Kalina | Dec 1996 | A |
5600967 | Meckler | Feb 1997 | A |
5634340 | Grennan | Jun 1997 | A |
5647221 | Garris, Jr. | Jul 1997 | A |
5649426 | Kalina | Jul 1997 | A |
5676382 | Dahlheimer | Oct 1997 | A |
5680753 | Hollinger | Oct 1997 | A |
5738164 | Hildebrand | Apr 1998 | A |
5754613 | Hashiguchi | May 1998 | A |
5771700 | Cochran | Jun 1998 | A |
5789822 | Calistrat | Aug 1998 | A |
5813215 | Weisser | Sep 1998 | A |
5833876 | Schnur | Nov 1998 | A |
5862666 | Liu | Jan 1999 | A |
5873260 | Linhardt | Feb 1999 | A |
5874039 | Edelson | Feb 1999 | A |
5894836 | Wu | Apr 1999 | A |
5899067 | Hageman | May 1999 | A |
5903060 | Norton | May 1999 | A |
5918460 | Connell | Jul 1999 | A |
5941238 | Tracy | Aug 1999 | A |
5943869 | Cheng | Aug 1999 | A |
5946931 | Lomax | Sep 1999 | A |
5973050 | Johnson | Oct 1999 | A |
6037683 | Lulay | Mar 2000 | A |
6041604 | Nicodemus | Mar 2000 | A |
6058930 | Shingleton | May 2000 | A |
6062815 | Holt | May 2000 | A |
6065280 | Ranasinghe | May 2000 | A |
6066797 | Toyomura | May 2000 | A |
6070405 | Jerye | Jun 2000 | A |
6082110 | Rosenblatt | Jul 2000 | A |
6105368 | Hansen | Aug 2000 | A |
6112547 | Spauschus | Sep 2000 | A |
6129507 | Ganelin | Oct 2000 | A |
6158237 | Riffat | Dec 2000 | A |
6164655 | Bothien | Dec 2000 | A |
6202782 | Hatanaka | Mar 2001 | B1 |
6223846 | Schechter | May 2001 | B1 |
6233938 | Nicodemus | May 2001 | B1 |
6282900 | Bell | Sep 2001 | B1 |
6282917 | Mongan | Sep 2001 | B1 |
6295818 | Ansley | Oct 2001 | B1 |
6299690 | Mongeon | Oct 2001 | B1 |
6341781 | Matz | Jan 2002 | B1 |
6374630 | Jones | Apr 2002 | B1 |
6393851 | Wightman | May 2002 | B1 |
6432320 | Bonsignore | Aug 2002 | B1 |
6434955 | Ng | Aug 2002 | B1 |
6442951 | Maeda | Sep 2002 | B1 |
6446425 | Lawlor | Sep 2002 | B1 |
6446465 | Dubar | Sep 2002 | B1 |
6463730 | Keller | Oct 2002 | B1 |
6484490 | Olsen | Nov 2002 | B1 |
6539720 | Rouse et al. | Apr 2003 | B2 |
6539728 | Korin | Apr 2003 | B2 |
6571548 | Bronicki | Jun 2003 | B1 |
6581384 | Benson | Jun 2003 | B1 |
6598397 | Hanna | Jul 2003 | B2 |
6644062 | Hays | Nov 2003 | B1 |
6657849 | Andresakis | Dec 2003 | B1 |
6668554 | Brown | Dec 2003 | B1 |
6684625 | Kline | Feb 2004 | B2 |
6695974 | Withers | Feb 2004 | B2 |
6715294 | Anderson | Apr 2004 | B2 |
6734585 | Tornquist | May 2004 | B2 |
6735948 | Kalina | May 2004 | B1 |
6739142 | Korin | May 2004 | B2 |
6751959 | McClanahan | Jun 2004 | B1 |
6769256 | Kalina | Aug 2004 | B1 |
6799892 | Leuthold | Oct 2004 | B2 |
6808179 | Bhattacharyya | Oct 2004 | B1 |
6810335 | Lysaght | Oct 2004 | B2 |
6817185 | Coney | Nov 2004 | B2 |
6857268 | Stinger | Feb 2005 | B2 |
6910334 | Kalina | Jun 2005 | B2 |
6918254 | Baker | Jul 2005 | B2 |
6921518 | Johnston | Jul 2005 | B2 |
6941757 | Kalina | Sep 2005 | B2 |
6960839 | Zimron | Nov 2005 | B2 |
6960840 | Willis | Nov 2005 | B2 |
6962054 | Linney | Nov 2005 | B1 |
6964168 | Pierson | Nov 2005 | B1 |
6968690 | Kalina | Nov 2005 | B2 |
6986251 | Radcliff | Jan 2006 | B2 |
7013205 | Hafner et al. | Mar 2006 | B1 |
7021060 | Kalina | Apr 2006 | B1 |
7022294 | Johnston | Apr 2006 | B2 |
7033533 | Lewis-Aburn et al. | Apr 2006 | B2 |
7033553 | Johnston et al. | Apr 2006 | B2 |
7036315 | Kang | May 2006 | B2 |
7041272 | Keefer | May 2006 | B2 |
7047744 | Robertson | May 2006 | B1 |
7048782 | Couch | May 2006 | B1 |
7062913 | Christensen | Jun 2006 | B2 |
7096665 | Stinger | Aug 2006 | B2 |
7096679 | Manole | Aug 2006 | B2 |
7124587 | Linney | Oct 2006 | B1 |
7174715 | Armitage | Feb 2007 | B2 |
7194863 | Ganev | Mar 2007 | B2 |
7197876 | Kalina | Apr 2007 | B1 |
7200996 | Cogswell | Apr 2007 | B2 |
7234314 | Wiggs | Jun 2007 | B1 |
7249588 | Russell | Jul 2007 | B2 |
7278267 | Yamada | Oct 2007 | B2 |
7279800 | Bassett | Oct 2007 | B2 |
7287381 | Pierson | Oct 2007 | B1 |
7305829 | Mirolli | Dec 2007 | B2 |
7313926 | Gurin | Jan 2008 | B2 |
7340894 | Miyahara et al. | Mar 2008 | B2 |
7340897 | Zimron | Mar 2008 | B2 |
7406830 | Valentian | Aug 2008 | B2 |
7416137 | Hagen et al. | Aug 2008 | B2 |
7453242 | Ichinose | Nov 2008 | B2 |
7458217 | Kalina | Dec 2008 | B2 |
7458218 | Kalina | Dec 2008 | B2 |
7464551 | Althaus et al. | Dec 2008 | B2 |
7469542 | Kalina | Dec 2008 | B2 |
7516619 | Pelletier | Apr 2009 | B2 |
7600394 | Kalina | Oct 2009 | B2 |
7621133 | Tomlinson | Nov 2009 | B2 |
7654354 | Otterstrom | Feb 2010 | B1 |
7665291 | Anand | Feb 2010 | B2 |
7665304 | Sundel | Feb 2010 | B2 |
7685821 | Kalina | Mar 2010 | B2 |
7730713 | Nakano | Jun 2010 | B2 |
7735335 | Uno | Jun 2010 | B2 |
7770376 | Brostmeyer | Aug 2010 | B1 |
7775758 | Legare | Aug 2010 | B2 |
7827791 | Pierson | Nov 2010 | B2 |
7838470 | Shaw | Nov 2010 | B2 |
7841179 | Kalina | Nov 2010 | B2 |
7841306 | Myers | Nov 2010 | B2 |
7854587 | Ito | Dec 2010 | B2 |
7866157 | Ernst | Jan 2011 | B2 |
7900450 | Gurin | Mar 2011 | B2 |
7950230 | Nishikawa | May 2011 | B2 |
7950243 | Gurin | May 2011 | B2 |
7972529 | Machado | Jul 2011 | B2 |
7997076 | Ernst | Aug 2011 | B2 |
8096128 | Held et al. | Jan 2012 | B2 |
8099198 | Gurin | Jan 2012 | B2 |
8146360 | Myers | Apr 2012 | B2 |
8281593 | Held | Oct 2012 | B2 |
8419936 | Berger et al. | Apr 2013 | B2 |
20010015061 | Viteri et al. | Aug 2001 | A1 |
20010020444 | Johnston | Sep 2001 | A1 |
20010030952 | Roy | Oct 2001 | A1 |
20020029558 | Tamaro | Mar 2002 | A1 |
20020066270 | Rouse et al. | Jun 2002 | A1 |
20020078696 | Korin | Jun 2002 | A1 |
20020078697 | Lifson | Jun 2002 | A1 |
20020082747 | Kramer | Jun 2002 | A1 |
20030000213 | Christensen | Jan 2003 | A1 |
20030061823 | Alden | Apr 2003 | A1 |
20030154718 | Nayar | Aug 2003 | A1 |
20030182946 | Sami | Oct 2003 | A1 |
20030213246 | Coll et al. | Nov 2003 | A1 |
20030221438 | Rane et al. | Dec 2003 | A1 |
20040011038 | Stinger | Jan 2004 | A1 |
20040011039 | Stinger et al. | Jan 2004 | A1 |
20040020185 | Brouillette et al. | Feb 2004 | A1 |
20040020206 | Sullivan et al. | Feb 2004 | A1 |
20040021182 | Green et al. | Feb 2004 | A1 |
20040035117 | Rosen | Feb 2004 | A1 |
20040083731 | Lasker | May 2004 | A1 |
20040083732 | Hanna et al. | May 2004 | A1 |
20040088992 | Brasz et al. | May 2004 | A1 |
20040097388 | Brask et al. | May 2004 | A1 |
20040105980 | Sudarshan et al. | Jun 2004 | A1 |
20040107700 | McClanahan et al. | Jun 2004 | A1 |
20040159110 | Janssen | Aug 2004 | A1 |
20040211182 | Gould | Oct 2004 | A1 |
20050022963 | Garrabrant et al. | Feb 2005 | A1 |
20050056001 | Frutschi | Mar 2005 | A1 |
20050096676 | Gifford, III et al. | May 2005 | A1 |
20050109387 | Marshall | May 2005 | A1 |
20050137777 | Kolavennu et al. | Jun 2005 | A1 |
20050162018 | Realmuto et al. | Jul 2005 | A1 |
20050167169 | Gering et al. | Aug 2005 | A1 |
20050183421 | Vaynberg et al. | Aug 2005 | A1 |
20050196676 | Singh et al. | Sep 2005 | A1 |
20050198959 | Schubert | Sep 2005 | A1 |
20050227187 | Schilling | Oct 2005 | A1 |
20050252235 | Critoph et al. | Nov 2005 | A1 |
20050257812 | Wright et al. | Nov 2005 | A1 |
20060010868 | Smith | Jan 2006 | A1 |
20060060333 | Chordia et al. | Mar 2006 | A1 |
20060066113 | Ebrahim et al. | Mar 2006 | A1 |
20060080960 | Rajendran et al. | Apr 2006 | A1 |
20060112693 | Sundel | Jun 2006 | A1 |
20060182680 | Keefer et al. | Aug 2006 | A1 |
20060211871 | Dai et al. | Sep 2006 | A1 |
20060213218 | Uno et al. | Sep 2006 | A1 |
20060225421 | Yamanaka et al. | Oct 2006 | A1 |
20060225459 | Meyer | Oct 2006 | A1 |
20060249020 | Tonkovich et al. | Nov 2006 | A1 |
20060254281 | Badeer et al. | Nov 2006 | A1 |
20070001766 | Ripley et al. | Jan 2007 | A1 |
20070017192 | Bednarek et al. | Jan 2007 | A1 |
20070019708 | Shiflett et al. | Jan 2007 | A1 |
20070027038 | Kamimura et al. | Feb 2007 | A1 |
20070056290 | Dahm | Mar 2007 | A1 |
20070089449 | Gurin | Apr 2007 | A1 |
20070108200 | McKinzie, II | May 2007 | A1 |
20070119175 | Ruggieri et al. | May 2007 | A1 |
20070130952 | Copen | Jun 2007 | A1 |
20070151244 | Gurin | Jul 2007 | A1 |
20070161095 | Gurin | Jul 2007 | A1 |
20070163261 | Strathman | Jul 2007 | A1 |
20070195152 | Kawai et al. | Aug 2007 | A1 |
20070204620 | Pronske et al. | Sep 2007 | A1 |
20070227472 | Takeuchi et al. | Oct 2007 | A1 |
20070234722 | Kalina | Oct 2007 | A1 |
20070245733 | Pierson et al. | Oct 2007 | A1 |
20070246206 | Gong et al. | Oct 2007 | A1 |
20080000225 | Kalina | Jan 2008 | A1 |
20080006040 | Peterson et al. | Jan 2008 | A1 |
20080010967 | Griffin | Jan 2008 | A1 |
20080023666 | Gurin | Jan 2008 | A1 |
20080053095 | Kalina | Mar 2008 | A1 |
20080066470 | MacKnight | Mar 2008 | A1 |
20080135253 | Vinegar et al. | Jun 2008 | A1 |
20080163625 | O'Brien | Jul 2008 | A1 |
20080173450 | Goldberg et al. | Jul 2008 | A1 |
20080211230 | Gurin | Sep 2008 | A1 |
20080250789 | Myers et al. | Oct 2008 | A1 |
20080252078 | Myers | Oct 2008 | A1 |
20090021251 | Simon | Jan 2009 | A1 |
20090085709 | Meinke | Apr 2009 | A1 |
20090107144 | Moghtaderi et al. | Apr 2009 | A1 |
20090139234 | Gurin | Jun 2009 | A1 |
20090139781 | Straubel | Jun 2009 | A1 |
20090173337 | Tamaura et al. | Jul 2009 | A1 |
20090173486 | Copeland | Jul 2009 | A1 |
20090180903 | Martin et al. | Jul 2009 | A1 |
20090205892 | Jensen et al. | Aug 2009 | A1 |
20090211251 | Petersen et al. | Aug 2009 | A1 |
20090211253 | Radcliff et al. | Aug 2009 | A1 |
20090266075 | Westmeier et al. | Oct 2009 | A1 |
20090293503 | Vandor | Dec 2009 | A1 |
20100024421 | Litwin | Feb 2010 | A1 |
20100077792 | Gurin | Apr 2010 | A1 |
20100083662 | Kalina | Apr 2010 | A1 |
20100102008 | Hedberg | Apr 2010 | A1 |
20100122533 | Kalina | May 2010 | A1 |
20100146949 | Stobart et al. | Jun 2010 | A1 |
20100146973 | Kalina | Jun 2010 | A1 |
20100156112 | Held et al. | Jun 2010 | A1 |
20100162721 | Welch et al. | Jul 2010 | A1 |
20100205962 | Kalina | Aug 2010 | A1 |
20100218513 | Vaisman et al. | Sep 2010 | A1 |
20100218930 | Proeschel | Sep 2010 | A1 |
20100263380 | Biederman et al. | Oct 2010 | A1 |
20100287934 | Glynn et al. | Nov 2010 | A1 |
20100300093 | Doty | Dec 2010 | A1 |
20100326076 | Ast et al. | Dec 2010 | A1 |
20110027064 | Pal et al. | Feb 2011 | A1 |
20110030404 | Gurin | Feb 2011 | A1 |
20110048012 | Ernst et al. | Mar 2011 | A1 |
20110061384 | Held et al. | Mar 2011 | A1 |
20110061387 | Held et al. | Mar 2011 | A1 |
20110088399 | Briesch et al. | Apr 2011 | A1 |
20110179799 | Allam | Jul 2011 | A1 |
20110185729 | Held | Aug 2011 | A1 |
20110192163 | Kasuya | Aug 2011 | A1 |
20110203278 | Kopecek et al. | Aug 2011 | A1 |
20110259010 | Bronicki et al. | Oct 2011 | A1 |
20110299972 | Morris et al. | Dec 2011 | A1 |
20110308253 | Ritter | Dec 2011 | A1 |
20120047892 | Held et al. | Mar 2012 | A1 |
20120067055 | Held | Mar 2012 | A1 |
20120128463 | Held | May 2012 | A1 |
20120131918 | Held | May 2012 | A1 |
20120131919 | Held | May 2012 | A1 |
20120131920 | Held | May 2012 | A1 |
20120131921 | Held | May 2012 | A1 |
20120159922 | Gurin | Jun 2012 | A1 |
20120159956 | Gurin | Jun 2012 | A1 |
20120174558 | Gurin | Jul 2012 | A1 |
20120186219 | Gurin | Jul 2012 | A1 |
20120247134 | Gurin | Oct 2012 | A1 |
20120247455 | Gurin et al. | Oct 2012 | A1 |
20120261090 | Durmaz et al. | Oct 2012 | A1 |
20130019597 | Kalina | Jan 2013 | A1 |
20130033037 | Held et al. | Feb 2013 | A1 |
20130036736 | Hart et al. | Feb 2013 | A1 |
20130113221 | Held | May 2013 | A1 |
Number | Date | Country |
---|---|---|
2794150 | Nov 2011 | CA |
1165238 | Nov 1997 | CN |
1432102 | Jul 2003 | CN |
101614139 | Dec 2009 | CN |
202055876 | Nov 2011 | CN |
202544943 | Nov 2012 | CN |
202718721 | Feb 2013 | CN |
2632777 | Feb 1977 | DE |
19906087 | Aug 2000 | DE |
10052993 | May 2002 | DE |
1977174 | Oct 2008 | EP |
1998013 | Dec 2008 | EP |
2419621 | Feb 2012 | EP |
2446122 | May 2012 | EP |
2478201 | Jul 2012 | EP |
2500530 | Sep 2012 | EP |
2550436 | Jan 2013 | EP |
856985 | Dec 1960 | GB |
2010974 | Jul 1979 | GB |
2075608 | Nov 1981 | GB |
58-193051 | Nov 1983 | JP |
60040707 | Mar 1985 | JP |
61-152914 | Jul 1986 | JP |
01-240705 | Sep 1989 | JP |
05-321612 | Dec 1993 | JP |
06-331225 | Nov 1994 | JP |
08028805 | Feb 1996 | JP |
09-100702 | Apr 1997 | JP |
2641581 | May 1997 | JP |
09-209716 | Aug 1997 | JP |
2858750 | Dec 1998 | JP |
H11270352 | May 1999 | JP |
2000257407 | Sep 2000 | JP |
2001-193419 | Jul 2001 | JP |
2002-097965 | Apr 2002 | JP |
2003529715 | Oct 2003 | JP |
2004-239250 | Aug 2004 | JP |
2004-332626 | Nov 2004 | JP |
2005030727 | Feb 2005 | JP |
2005-533972 | Nov 2005 | JP |
2005-533972 | Nov 2005 | JP |
2006037760 | Feb 2006 | JP |
2006177266 | Jul 2006 | JP |
2007-198200 | Aug 2007 | JP |
2007-198200 | Sep 2007 | JP |
4343738 | Oct 2009 | JP |
2011-017268 | Jan 2011 | JP |
10-0191080 | Jun 1999 | KR |
100191080 | Jun 1999 | KR |
10 2007 0086244 | Aug 2007 | KR |
10-0766101 | Oct 2007 | KR |
10-0844634 | Jul 2008 | KR |
10-0844634 | Jul 2008 | KR |
10-20100067927 | Jun 2010 | KR |
1020110018769 | Feb 2011 | KR |
1069914 | Sep 2011 | KR |
1103549 | Jan 2012 | KR |
10-2012-0058582 | Jun 2012 | KR |
2012-0068670 | Jun 2012 | KR |
2012-0128753 | Nov 2012 | KR |
2012-0128755 | Nov 2012 | KR |
WO 9105145 | Apr 1991 | WO |
WO 9609500 | Mar 1996 | WO |
0071944 | Nov 2000 | WO |
WO 0144658 | Jun 2001 | WO |
WO 2006060253 | Jun 2006 | WO |
WO 2006137957 | Dec 2006 | WO |
WO 2007056241 | May 2007 | WO |
WO 2007079245 | Jul 2007 | WO |
WO 2007082103 | Jul 2007 | WO |
WO 2007112090 | Oct 2007 | WO |
WO 2008039725 | Apr 2008 | WO |
2008101711 | Aug 2008 | WO |
2009-045196 | Apr 2009 | WO |
WO 2009058992 | May 2009 | WO |
2010-074173 | Jul 2010 | WO |
2010083198 | Jul 2010 | WO |
WO 2010121255 | Oct 2010 | WO |
WO 2010126980 | Nov 2010 | WO |
WO 2010151560 | Dec 2010 | WO |
WO 2011017450 | Feb 2011 | WO |
WO 2011017476 | Feb 2011 | WO |
WO 2011017599 | Feb 2011 | WO |
WO 2011034984 | Mar 2011 | WO |
WO 2011094294 | Aug 2011 | WO |
WO 2011119650 | Sep 2011 | WO |
2012-074907 | Jun 2012 | WO |
2012-074911 | Jun 2012 | WO |
20124074905 | Jun 2012 | WO |
WO 2012074940 | Jun 2012 | WO |
WO 2013055391 | Apr 2013 | WO |
WO 2013059687 | Apr 2013 | WO |
WO 2013059695 | Apr 2013 | WO |
WO 2013070249 | May 2013 | WO |
WO 2013074907 | May 2013 | WO |
Entry |
---|
Alpy, N., et al., “French Atomic Energy Commission views as regards SCO2 Cycle Development priorities and related R&D approach,” Presentation, Symposium on SCO2 Power Cycles, Apr. 29-30, 2009, Troy, NY, 20 pages. |
Angelino, G., and Invernizzi, C.M., “Carbon Dioxide Power Cycles using Liquid Natural Gas as Heat Sink”, Applied Thermal Engineering Mar. 3, 2009, 43 pages. |
Bryant, John C., Saari, Henry, and Zanganeh, Kourosh, “An Analysis and Comparison of the Simple and Recompression Supercritical CO2 Cycles” Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 8 pages. |
Chapman, Daniel J., Arias, Diego A., “An Assessment of the Supercritical Carbon Dioxide Cycle for Use in a Solar Parabolic Trough Power Plant”, Presentation, Abengoa Solar, Apr. 29-30, 2009, Troy, NY, 20 pages. |
Chapman, Daniel J., Arias, Diego A., “An Assessment of the Supercritical Carbon Dioxide Cycle for Use in a Solar Parabolic Trough Power Plant”, Paper, Abengoa Solar, Apr. 29-30, 2009, Troy, NY, 5 pages. |
Chen, Yang, Lundqvist, P., Johansson, A., Platell, P., “A Comparative Study of the Carbon Dioxide Transcritical Power Cycle Compared with an Organic Rankine Cycle with R123 as Working Fluid in Waste Heat Recovery”, Science Direct, Applied Thermal Engineering, Jun. 12, 2006, 6 pages. |
Chen, Yang, “Thermodynamic Cycles Using Carbon Dioxide as Working Fluid”, Doctoral Thesis, School of Industrial Engineering and Management, Stockholm, Oct. 2011, 150 pages., (3 parts). |
Chordia, Lalit, “Optimizing Equipment for Supercritical Applications”, Thar Energy LLC, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 7 pages. |
Combs, Osie V., “An Investigation of the Supercritical CO2 Cycle (Feher cycle) for Shipboard Application”, Massachusetts Institute of Technology, May 1977, 290 pages. |
Di Bella, Francis A., “Gas Turbine Engine Exhaust Waste Heat Recovery Navy Shipboard Module Development”, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 8 pages. |
Dostal, V., et al., A Supercritical Carbon Dioxide Cycle for Next Generation Nuclear Reactors, Mar. 10, 2004, 326 pages., (7 parts). |
Dostal, Vaclav, and Dostal, Jan, “Supercritical CO2 Regeneration Bypass Cycle—Comparison to Traditional Layouts”, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 5 pages. |
Eisemann, Kevin, and Fuller, Robert L., “Supercritical CO2 Brayton Cycle Design and System Start-up Options”, Barber Nichols, Inc., Paper, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 7 pages. |
Eisemann, Kevin, and Fuller, Robert L., “Supercritical CO2 Brayton Cycle Design and System Start-up Options”, Presentation, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 11 pages. |
Feher, E.G., et al.., “Investigation of Supercritical (Feher) Cycle”, Astropower Laboratory, Missile & Space Systems Division, Oct. 1968, 152 pages. |
Fuller, Robert L., and Eisemann, Kevin, “Centrifugal Compressor Off-Design Performance for Super-Critical CO2” , Barber Nichols, Inc. Presentation, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 20 pages. |
Fuller, Robert L., and Eisemann, Kevin, “Centrifugal Compressor Off-Design Performance for Super-Critical CO2”, Paper, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 12 pages. |
Gokhstein, D.P. and Verkhivker, G.P. “Use of Carbon Dioxide as a Heat Carrier and Working Substance in Atomic Power Stations”, Soviet Atomic Energy, Apr. 1969, vol. 26, Issue 4, pp. 430-432. |
Gokhstein, D.P.; Taubman, El.; Konyaeva, G.P., “Thermodynamic Cycles of Carbon Dioxide Plant with an Additional Turbine After the Regenerator”, Energy Citations Database, Mar. 1973, 1 Page, Abstract only. |
Hejzlar, P. et al., “Assessment of Gas Cooled Gas Reactor with Indirect Supercritical CO2 Cycle” Massachusetts Institute of Technology, Jan. 2006, 10 pages. |
Hoffman, John R., and Feher, E.G “150 kwe Supercritical Closed Cycle System”, Transactions of the ASME, Jan. 1971, pp. 70-80. |
Jeong, Woo Seok, et al., “Performance of S-CO2 Brayton Cycle with Additive Gases for SFR Application”, Korea Advanced Institute of Science and Technology, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 5 pages. |
Johnson, Gregory A., & McDowell, Michael, “Issues Associated with Coupling Supercritical CO2 Power Cycles to Nuclear, Solar and Fossil Fuel Heat Sources”, Hamilton Sundstrand, Energy Space & Defense-Rocketdyne, Apr. 29-30, 2009, Troy, NY, Presentation, 18 pages. |
Kawakubo, Tomoki, “Unsteady Roto-Stator Interaction of a Radial-Inflow Turbine with Variable Nozzle Vanes”, ASME Turbo Expo 2010: Power for Land, Sea, and Air; vol. 7: Turbomachinery, Parts A, B, and C; Glasgow, UK, Jun. 14-18, 2010, Paper No. GT2010-23677, pp. 2075-2084, (1 page, Abstract only). |
Kulhanek, Martin, “Thermodynamic Analysis and Comparison of S-CO2 Cycles”, Presentation, Czech Technical University in Prague, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 14 pages. |
Kulhanek, Martin, “Thermodynamic Analysis and Comparison of S-CO2 Cycles”, Paper, Czech Technical University in Prague, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 7 pages. |
Kulhanek, Martin., and Dostal, Vaclav, “Supercritical Carbon Dioxide Cycles Thermodynamic Analysis and Comparison”, Abstract, Faculty Conference held in Prague, Mar. 24, 2009, 13 pages. |
Ma, Zhiwen and Turchi, Craig S., “Advanced Supercritical Carbon Dioxide Power Cycle Configurations for Use in Concentrating Solar Power Systems”, National Renewable Energy Laboratory, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 4 pages. |
Moisseytsev, Anton, and Sienicki, Jim, “Investigation of Alternative Layouts for the Supercritical Carbon Dioxide Brayton Cycle for a Sodium-Cooled Fast Reactor”, Supercritical CO2 Power Cycle Symposium, Troy, NY, Apr. 29, 2009, 26 pages. |
Munoz De Escalona, Jose M., “The Potential of the Supercritical Carbon Dioxide Cycle in High Temperature Fuel Cell Hybrid Systems”, Paper, Thermal Power Group, University of Seville, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 6 pages. |
Munoz De Escalona, Jose M., et al., “The Potential of the Supercritical Carbon Dioxide Cycle in High Temperature Fuel Cell Hybrid Systems”, Presentation, Thermal Power Group, University of Seville, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 19 pages. |
Muto, Y., et al., “Application of Supercritical CO2 Gas Turbine for the Fossil Fired Thermal Plant”, Journal of Energy and Power Engineering, Sep. 30, 2010, vol. 4, No. 9, 9 pages. |
Noriega, Bahamonde J.S., “Design Method for s-CO2 Gas Turbine Power Plants”, Master of Science Thesis, Delft University of Technology, Oct. 2012, 122 pages., (3 parts). |
Oh, Chang, et al., “Development of a Supercritical Carbon Dioxide Brayton Cycle: Improving PBR Efficiency and Testing Material Compatibility”, Presentation, Nuclear Energy Research Initiative Report, Oct. 2004, 38 pages. |
Oh, Chang; et al., “Development of a Supercritical Carbon Dioxide Brayton Cycle: Improving VHTR Efficiency and Testing Material Compatibility”, Presentation, Nuclear Energy Research Initiative Report, Final Report, Mar. 2006, 97 pages. |
Parma, Ed, et at, “Supercritical CO2 Direct Cycle Gas Fast Reactor (SC-GFR) Concept” Presentation for Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 40 pages. |
Parma, Ed, et al., “Supercritical CO2 Direct Cycle Gas Fast Reactor (SC-GFR) Concept”, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 9 pages. |
Parma, Edward J., et al., “Supercritical CO2 Direct Cycle Gas Fast Reactor (SC-GFR) Concept”, Presentation, Sandia National Laboratories, May 2011, 55 pages. |
PCT/US2006/049623—Written Opinion of ISA dated Jan. 4, 2008, 4 pages. |
PCT/US2007/001120—International Search Report dated Apr. 25, 2008, 7 pages. |
PCT/US2007/079318—International Preliminary Report on Patentability dated Jul. 7, 2008, 5 pages. |
PCT/US2010/031614—International Search Report dated Jul. 12, 2010, 3 pages. |
PCT/US2010/031614—International Preliminary Report on Patentability dated Oct. 27, 2011, 9 pages. |
PCT/US2010/039559—International Preliminary Report on Patentability dated Jan. 12, 2012, 7 pages. |
PCT/US2010/039559—Notification of Transmittal of the International Search Report and Written Opinion of the International Searching Authority, or the Declaration dated Sep. 1, 2010, 6 pages. |
PCT/US2010/044476—International Search Report dated Sep. 29, 2010, 23 pages. |
PCT/US2010/044681—International Search Report and Written Opinion mailed Oct. 7, 2010, 10 pages. |
PCT/US2010/044681—International Preliminary Report on Patentability dated Feb. 16, 2012, 9 pages. |
PCT/US2010/049042—International Search Report and Written Opinion dated Nov. 17, 2010, 11 pages. |
PCT/US2010/049042—International Preliminary Report on Patentability dated Mar. 29, 2012, 18 pages. |
PCT/US2011/029486—International Preliminary Report on Patentability dated Sep. 25, 2012, 6 pages. |
PCT/US2011/029486—International Search Report and Written Opinion dated Nov. 16, 2011, 9 pages. |
PCT/US2011/062266—International Search Report and Written Opinion dated Jul. 9, 2012, 12 pages. |
PCT/US2011/062198—International Search Report and Written Opinion dated Jul. 2, 2012, 9 pages. |
PCT/US2011/062201—International Search Report and Written Opinion dated Jun. 26, 2012, 9 pages. |
PCT/US2011/062204—International Search Report dated Nov. 1, 2012, 10 pages. |
PCT/US2011/62207—International Search Report and Written Opinion dated Jun. 28, 2012, 7 pages. |
PCT/US2012/000470—International Search Report dated Mar. 8, 2013, 10 pages. |
PCT/US2012/061151—International Search Report and Written Opinion dated Feb. 25, 2013, 9 pages. |
PCT/US2012/061159—International Search Report dated Mar. 2, 2013, 10 pages. |
Persichilli, Michael, et al., “Supercritical CO2 Power Cycle Developments and Commercialization: Why sCO2 can Displace Steam” Echogen Power Systems LLC, Power-Gen India & Central Asia 2012, Apr. 19-21, 2012, New Delhi, India, 15 pages. |
Saari, Henry, et al., “Supercritical CO2 Advanced Brayton Cycle Design”, Presentation, Carleton University, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 21 pages. |
San Andres, Luis, “Start-Up Response of Fluid Film Lubricated Cryogenic Turbopumps (Preprint)”, AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, Jul. 8-11, 2007, 38 pages. |
Sarkar, J., and Bhattacharyya, Souvik, “Optimization of Recompression S-CO2 Power Cycle with Reheating” Energy Conversion and Management 50 (May 17, 2009), pp. 1939-1945. |
Tom, Samsun Kwok Sun, “The Feasibility of Using Supercritical Carbon Dioxide as a Coolant for the Candu Reactor”, The University of British Columbia, Jan. 1978, 156 pages. |
VGB PowerTech Service GmbH, “CO2 Capture and Storage”, A VGB Report on the State of the Art, Aug. 25, 2004, 112 pages. |
Vidhi, Rachana, et al., “Study of Supercritical Carbon Dioxide Power Cycle for Power Conversion from Low Grade Heat Sources”, Presentation, University of South Florida and Oak Ridge National Laboratory, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 17 pages. |
Vidhi, Rachana, et al., “Study of Supercritical Carbon Dioxide Power Cycle for Power Conversion from Low Grade Heat Sources”, Paper, University of South Florida and Oak Ridge National Laboratory, Supercritical CO2 Power Cycle Symposium, May 24-25, 2011, Boulder, CO, 8 pages. |
Wright, Steven A., et al., “Modeling and Experimental Results for Condensing Supercritical CO2 Power Cycles”, Sandia Report, Jan. 2011, 47 pages. |
Wright, Steven A., et al., “Supercritical CO2 Power Cycle Development Summary at Sandia National Laboratories”, May 24-25, 2011, (1 page, Abstract only). |
Wright, Steven, “Mighty Mite”, Mechanical Engineering, Jan. 2012, pp. 41-43. |
Yoon, Ho Joon, et al., “Preliminary Results of Optimal Pressure Ratio for Supercritical CO2 Brayton Cycle coupled with Small Modular Water Cooled Reactor”, Presentation, Korea Advanced Institute of Science and Technology and Khalifa University of Science, Technology and Research, Boulder, CO, May 25, 2011, 18 pages. |
Yoon, Ho Joon, et al., “Preliminary Results of Optimal Pressure Ratio for Supercritical CO2 Brayton Cycle coupled with Small Modular Water Cooled Reactor”, Paper, Korea Advanced Institute of Science and Technology and Khalifa University of Science, Technology and Research, May 24-25, 2011, Boulder, CO, 7 pages. |
Vaclav Dostal, Martin Kulhanek, “Research on the Supercritical Carbon Dioxide Cycles in the Czech Republic”, Department of Fluid Mechanics and Power Engineering Czech Technical University in Prague, RPI, Troy, NY, Apr. 29-30, 2009; 8 pages. |
CN Search Report for Application No. 201080035382.1, 2 pages. |
CN Search Report for Application No. 201080050795.7, 2 pages. |
PCT/US2011/062198—Extended European Search Report dated May 6, 2014, 9 pages. |
PCT/US2011/062201—Extended European Search Report dated May 28, 2014, 8 pages. |
PCT/US2013/055547—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated Jan. 24, 2014, 11 pages. |
PCT/US2013/064470—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated Jan. 22, 2014, 10 pages. |
PCT/US2013/064471—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated Jan. 24, 2014, 10 pages. |
PCT/US2014/013154—International Search Report dated May 23, 2014, 4 pages. |
PCT/US2014/013170—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated May 9, 2014, 12 pages. |
PCT/US2014/023026—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated Jul. 22, 2014, 11 pages. |
PCT/US2014/023990—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated Jul. 17, 2014, 10 pages. |
PCT/US2014/026173—Notification of Transmittal of the International Search Report and the Written Opinion of the International Searching Authority, or the Declaration dated Jul. 9, 2014, 10 pages. |
Renz, Manfred, “The New Generation Kalina Cycle”, Contribution to the Conference: “Electricity Generation from Enhanced Geothermal Systems”, Sep. 14, 2006, Strasbourg, France, 18 pages. |
Thorin, Eva, “Power Cycles with Ammonia-Water Mixtures as Working Fluid”, Doctoral Thesis, Department of Chemical Engineering and Technology Energy Processes, Royal Institute of Technology, Stockholm, Sweden, 2000, 66 pages. |
Number | Date | Country | |
---|---|---|---|
20140090405 A1 | Apr 2014 | US |
Number | Date | Country | |
---|---|---|---|
61542478 | Oct 2011 | US |