Embodiments of the present disclosure generally relate to magnetic cooling systems such as magnetocaloric refrigeration systems for cooling. More particularly, embodiments of the present disclosure relate to magnetocaloric refrigeration systems for cooling gas turbine inlet air.
A gas turbine engine combusts a mixture of fuel and air to drive one or more turbine stages. The gas turbine engine generally intakes ambient air into a compressor, which compresses the air to a suitable pressure for optimal combustion of the fuel in a combustor. Unfortunately, the temperature and humidity of the ambient air can vary significantly due to geographic location, seasons, and so forth. A temperature variation of the ambient air may lead to reduced performance of the gas turbine engine. For example, an increase of 50 degrees in temperature may causes more than 25 percent loss of power.
One approach for avoiding the power degradation caused by high temperature of the ambient air is cooling the inlet air before compressing it in the compressor. Such inlet air cooling causes the air to have a higher density so as to create a higher mass flow rate into the compressor. The higher mass flow rate of the air in a compressor allows more air to be compressed so as to allow the gas turbine engine to produce more power output.
Various refrigeration techniques have been proposed such as vapor compression refrigeration, absorption cooling, and evaporative cooling. Disadvantages of such techniques are high cost and energy consumption, utilization of environmentally hazardous fluids (for example, HCFCs) and unreliability of the cooling capacity due to the dependency upon vagaries of weather.
Magnetic refrigeration uses a magnetocaloric material to provide cooling in some refrigeration systems. However, the amount of cooling from conventional magnetic refrigeration systems may not be sufficient for the cooling of inlet air of the gas turbine engines.
An improved magnetic cooling system suitable for cooling of inlet air of gas turbine engines, for example, is disclosed herein. In one aspect, the magnetic cooling system includes at least one magnetic assembly, at least one magnetic regenerator including a magnetocaloric material movably arranged in a closed loop to cyclically pass through the at least one magnetic assembly and a fluid supply device in fluid communication with the at least one magnetic assembly to supply a cooling fluid to the at least one magnetic assembly.
In another aspect, a turbine assembly includes a magnetic cooling system disposed in a path of an inlet air to a turbine system.
These and other features and aspects of embodiments of the present disclosure will become better understood when the following detailed description is read with reference to the accompanying drawings in which like characters in each individual figure, represent like parts throughout the drawings, wherein:
Provided herein are magnetic cooling systems. In particular, embodiments of the present disclosure provide magnetic cooling systems employing magnetocaloric materials. The magnetic cooling systems provides improved cooling, and can be used for various applications such as, for example, cooling inlet air of gas turbines, cooling homes, and cooling offices.
In the following specification and the claims, singular forms “a”, “an” and “the” include plural referents unless the context clearly dictates otherwise. As used herein, the term “or” is not meant to be exclusive and refers to at least one of the referenced components being present and includes instances in which a combination of the referenced components may be present, unless the context clearly dictates otherwise.
Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term such as “about” or “substantially” is not limited to the precise value specified.
In some embodiments, a magnetic cooling system includes at least one magnetic assembly, at least one magnetic regenerator movably arranged in a closed loop to cyclically pass through the at least one magnetic assembly, and a fluid supply device in fluid communication with the at least one magnetic assembly to supply a cooling fluid. The at least one magnetic regenerator includes a magnetocaloric material. In some embodiments, the at least one magnetic regenerator is arranged on a conveyor that passes through the at least one magnetic assembly and forms the closed loop. The at least one magnetic assembly may include a pair of N pole and S pole magnets or a coil.
As used herein, the term “magnetocaloric material” refers to materials that exhibit magnetocaloric effect. In general, the magnetocaloric effect refers to a process of entropic change upon application or withdrawal of an external magnetic field. On application or increase of an external magnetic field, the magnetic moments of a magnetocaloric material become more ordered and cause the magnetocaloric material to generate heat. Conversely, withdrawing or decreasing the external magnetic field allows the magnetic moments of the magnetocaloric material to become more disordered and cause the material to absorb heat. Some magnetocaloric materials exhibit the opposite behavior i.e. generating heat when the magnetic field is removed (which are sometimes referred to as para-magneto caloric materials but both types are referred to collectively herein as magneto caloric materials). The theoretical Carnot cycle efficiency of a refrigeration cycle based on an magnetocaloric material can be significantly higher than for a comparable refrigeration cycle based on a fluid refrigerant. Generally, magnetocaloric materials have pores having high permeability for flow of the heat transfer fluid, and have high capacity to absorb and dissipate heat. Suitable examples of the magnetocaloric materials include, but are not limited to, gadolinium (Gd), manganese iron compound (MnFe), lanthanum iron compounds (LaFe), or a combination thereof.
Examples of the cooling fluids include, but are not limited to, water, alcohols, antifreezes such as ethylene glycol, helium gas, or a combination thereof.
As illustrated, the magnetic assembly 102 is disposed at a portion 108 of the magnetic cooling system 100. In some embodiments, the magnetic assembly 102 is disposed in a casing 112. The casing 112 may have an inlet port 114 allowing the magnetic assembly 102 to be in fluid communication with the fluid supply device 106 and an outlet port 116 allowing the magnetic assembly 102 to be in fluid communication with an outside environment. In some embodiments, the fluid supply device 106 is configured to supply a cooling fluid to the magnetic assembly 102. During operation, the cooling fluid enters to the casing 112 through the inlet port 114, flows through the magnetic assembly 102 and exits from the outlet port 116. In some embodiments, the casing 112 may have a plurality of inlet ports 114 and a plurality of outlet ports 116, as shown in
The magnetic regenerator 104 is movably arranged in a closed loop 101 to cyclically pass through the magnetic assembly 102. In some embodiments, as illustrated in
The magnetic regenerator 104 may be in form of a plate, a sheet, a foil, a strip or a combination thereof having a length. In some embodiments, as illustrated in
The magnetic regenerator 104 is arranged on the conveyor 118. The conveyor 118 may be arranged at any location along the length L of the magnetic regenerator 104. The magnetic regenerator 104 may be mechanically coupled to the conveyor 118. As illustrated in
Further, the magnetic cooling system 100 is configured to allow a fluid that has to be cooled (the fluid may also be referred to as ‘to-be cooled fluid’) to flow across the closed loop 101 through an inlet and an outlet. In some embodiments, as illustrated in
In the magnetic cooling system 100, during operation, the magnetic regenerator 104 moves cyclically in the closed loop 101 to alternately enter and leave the magnetic field generated by the magnetic assembly 102. While in the magnetic assembly 102, the magnetic regenerator 104 becomes cooler. When the to-be cooled fluid flows through the magnetic cooling system 100 across the closed loop 101, heat transfer occurs between the to-be-cooled fluid and the magnetic regenerator 104. One complete cycle of the closed loop 101 performed by the magnetic regenerator 104 may be referred to as a cooling cycle. The process of heat transfer in one cooling cycle, in some embodiments, is described below.
Referring to
In some embodiments, a magnetic cooling system may include a plurality of magnetic assemblies, a plurality of magnetic regenerators or a combination thereof. The level of cooling may depend on the number of cooling cycles encountered by a fluid to be cooled (i.e., to-be cooled fluid), the number of magnetic assemblies, the number of magnetic regenerators, and their combinations arranged in a closed loop of a magnetic cooling system as described above. The number of cooling cycles may further depend, in part, on the number of magnetic regenerators arranged to move in the closed loop, the speed of a conveyor and/or the speed of the to-be-cooled fluid flow. The number of magnetic assemblies, the number of magnetic regenerators or both and the movement of the magnetic regenerators may depend on the desired temperature for the end use application. As an example, for cooling a to-be cooled fluid to a temperature in a range from 15 degrees Celsius to about 22 degrees Celsius such as for home or office cooling, the magnetic cooling system may include one magnetic assembly and a few magnetic regenerators depending on the magnetocaloric material(s) used. In another example, cooling to a much lower temperature for example, lower than 10 degrees Celsius, a plurality of magnetic regenerators and a plurality of magnetic assemblies may be required.
In embodiments where a magnetic cooling system includes a plurality of magnetic assemblies, a plurality of magnetic regenerators or a combination thereof, the plurality of magnetic assemblies may be disposed substantially apart.
In the magnetic cooling system 200 of
One embodiment is directed to a turbine assembly that includes a magnetic cooling system (as described hereinabove) for cooling inlet air provided to a turbine system for example, a gas turbine system. The turbine assembly includes the magnetic cooling system disposed in a path of an inlet air to the turbine system.
The magnetic cooling systems, as disclosed in above embodiments, are advantageously capable of reducing the temperature to a desirable level with some alterations in the configuration. The configuration of the magnetic cooling systems may be tailored by varying the number and size of magnetic regenerators and magnetic assemblies to achieve a desired level of cooling. These magnetic cooling systems are suitable for use in the gas turbine systems for cooling the inlet air (for example, to a temperature up to 5 degrees Celsius) and providing high performance. In a gas turbine system, these magnetic cooling systems provide many advantages over conventional refrigeration or cooling techniques. Unlike, the conventional vapor compression refrigeration, the magnetic cooling system uses no refrigerants that may have environmental concerns and no compressor that may cause large parasitic losses. Further, unlike evaporation cooling techniques, the lowest temperature provided is not limited. In addition, the magnetic cooling systems are compact and have smaller footprint as compared to conventional refrigeration techniques. Their designs also provide cheaper and simpler integration with a gas turbine systems.
While only certain features of the disclosure have been illustrated and described herein, many modifications and changes will occur to those skilled in the art. It is, therefore, to be understood that the appended claims are intended to cover all such modifications and changes as fall within the true spirit of the disclosure.