The present disclosure describes subject matter that relates to closed loop systems, with particular discussion about embodiments of systems that are configured with a cooling system that utilizes a working fluid to evacuate and cool components.
Systems that generate power include closed loop systems that operate under principles of a Rankine Thermodynamic Cycle. These systems use thermal energy from a thermal source fluid to evaporate a working fluid, e.g., a low temperature boiling organic fluid. This process generates high pressure vapor. In conventional designs, the system directs the vapor to power generating machinery, for example, a turbine or like device, that can operate a generator to generate electric power. The system can also cool and condense the vapor to liquid form.
The temperature of the cooling fluid in the cooling circuit 120 is related to the saturation temperature of the working fluid F at the pressure at which the working fluid F is allowed to expand. In closed loop systems like the system 100 of
The present disclosure contemplates improvements that facilitate cooling of components in closed loop systems. Embodiments of the systems below, for example, are configured to depress the local pressure at or near components that are the target of cooling, which in turn permits the cooling fluid to function at temperatures that can remove heat, even when the ambient temperature rises above desirable levels. In one embodiment, the system is configured to use energy of the working fluid F in vapor phase to lower the pressure in a housing, or like environment, that encloses critical elements of the generator. Notably, by utilizing the working fluid F in vapor phase, this configuration forgoes use of devices (e.g., pumps) with external power requirements that, in effect, would operate more as a parasitic loss or load and would likely reduce the overall efficiency of the system.
Reference is now made briefly to the accompanying drawings in which:
Where applicable like reference characters designate identical or corresponding components and units throughout the several views, which are not to scale unless otherwise indicated.
Broadly, the entrainment component 226 include devices that use the energy of a motive fluid to create a low pressure zone or area. These devices include, for example, ejectors and/or injectors (and/or other devices that utilizes similar principles of operation to utilize the energy of one fluid to create a vacuum). In the present example, the cooling system 220 couples the low pressure zone of the entrainment component 226 with the sealed component 224. This configuration draws fluid from the sealed component 224 (e.g., the third fluid component 232). The fluid enters the entrainment component 226, where the fluid mixes with the second fluid component 230 and exits the entrainment component 226 as the fourth fluid component 234.
The sealed component 224 may house electrical and/or power components that generate heat and/or need to be cooled. These components may operate as part of power generating machinery (e.g., a turbine-generator), which integrates into the closed loop system 200. Examples of the power generating machinery may include turbines, which utilize the working fluid F that flows in the closed loop system 200 to generate power and/or electricity. This disclosure contemplates a wide variety of devices, components, and/or systems for use as the power generating component, e.g., devices that utilize impellers, screws, vanes, pistons, and other implements to transform the work of the flow of the working fluid F into power. Moreover, this disclosure recognizes that concepts of the cooling system 222 may extend to other variations of the closed loop system 200.
The flow paths 354, 356 are configured to direct working fluid F from the fluid circuit 310, in both liquid phase and vapor phase. In the present example, the first flow path 354 can couple with the fluid circuit 310 at a first point downstream of the evaporator component 302 and upstream of the turbine member 346 and at a second point upstream of the condenser member 352 and downstream of the turbine member 346. This configuration of the cooling system 322 can distribute working fluid F in vapor phase (from the first point of the fluid circuit 310) to the entrainment component 326, as well as to allow fluid from the entrainment component 326 to reenter the fluid circuit 310 (at the second point). The second flow path 356 can couple with the fluid circuit 310 at a point shown in
During operation, the system 300 leverages changes in the working properties and phases of the working fluid F to convert thermal energy to mechanical and/or electrical energy. Starting in the lower right corner of
The cooling system 322 utilizes a portion of the working fluid F as the cooling fluid to cool components, namely, electronic components found in the sealed component 324. This cooling fluid may, for example, correspond with the high pressure working fluid F (e.g., 20 bar, 40° C.) that exits the pump component 302. In one implementation, the cooling fluid enters the sealed component 324, passes over the electronic components, and expands to the condenser pressure (e.g., 2 bar). To lower the cooling temperature of the cooling fluid, the entrainment component 326 is configured to evacuate the sealed component 324. In one example, the entrainment component 326 is configured as an ejector (and/or an injector) to utilize energy in a small portion of incoming working fluid F in vapor phase (e.g., 20 bar, 125° C.) that exits the evaporator component 304. This incoming working fluid vapor F provides motive power to evacuate the sealed component 324.
Use of the entrainment component 326 can modify operating conditions inside of the sealed component 326. In one implementation, the entrainment component 326 can create a pressure inside of the sealed component 324 that is lower than the condensing pressure. This operating condition, in turn, can overcome thermodynamic limits on the lower bound of the temperature that can be reached because the saturation temperature (e.g., 33.5° C.) corresponds to the condensing pressure. Moreover, since use of thermal energy in the working fluid F is less expensive than, for example, electrical energy that might be required to operate a vacuum pump or similarly configured device, the cooling system 322 can improve the overall efficiency and can expand the operating range of the cooling system 300. This configuration is also beneficial because it can minimize the need to de-rate the system 300 at higher ambient temperatures, there is no contamination or leakage because the system 300 is self-contained, and because there are no moving parts that may compromise reliability and safety.
As best shown in
The ejector device 364 is useful to evacuate the sealed component 324 (
As used herein, an element or function recited in the singular and proceeded with the word “a” or “an” should be understood as not excluding plural said elements or functions, unless such exclusion is explicitly recited. Furthermore, references to “one embodiment” of the claimed invention should not be interpreted as excluding the existence of additional embodiments that also incorporate the recited features.
This written description uses examples to disclose embodiments of the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims.
This application claims the benefit of priority to U.S. Provisional Patent Application Ser. No. 61/837,973, filed on Jun. 21, 2013, and entitled “COOLING SYSTEM AND COOLING METHOD FOR USE WITH CLOSED LOOP SYSTEMS.” The content of this provisional application is incorporated herein by reference in its entirety.
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