The present invention relates to the thermal management of building envelopes using thermally anisotropic composites that are connected to a thermal loop that serves as a heat sink or source.
In buildings, thermal management is important for both energy consideration and thermal comfort. Thermal management to limit heat transfer through the building envelope (walls, roof, and foundation) has traditionally been performed with insulation materials. Alternative methods have been proposed, including an emphasis on thermal mass, solar control and shading, and ventilation. Vacuum insulation panels and aerogels are among a new generation of high-performance insulation materials being investigated. These materials can provide higher thermal resistance compared to current foam and fibrous insulation materials, but suffer from high cost, low durability, and diminishing savings. Accordingly, there remains a continued need for new thermal management systems for building envelopes, and in particular, thermal management systems that can be dynamically controlled to reduce peak energy demand, shape energy use, and redirect heat for thermal energy harvesting or thermal storage in existing and new buildings. Previously proposed dynamic systems primarily focus on controlling the heat transfer rate through the envelope by changing their thermal resistance, but are not able to redirect heat.
An improved system for thermal management is provided. The system includes thermally anisotropic composites coupled with a thermal loop to dynamically redirect, reduce, and/or shape heat flows through a building envelope, having the potential to (1) significantly reduce envelope-generated heating and cooling loads in buildings and (2) provide grid services such as decreasing peak loads and shaping energy use.
In one embodiment, the thermal management system includes an anisotropic composite that is made of alternating layer(s) of thermal insulation material and thin layer(s) of thermally conductive material. The thermal management system also includes a thermal loop that serves as heat sink or source along a long edge or the entire perimeter of the anisotropic composite. The temperature of the fluid circulating in the thermal loop (referred to as fluid hereafter) is either dynamically controlled or is let to float. During cooling periods, the fluid in the thermal loop is maintained at a temperature that is lower than that of the outdoor ambient temperature. When the outdoor ambient temperature reaches a building balance point temperature (the building balance point temperature is the outdoor air temperature when the heat gains of the building are equal to the heat losses), for example, 12.78° C. (55° F.), the thermal loop can stop circulating a cooling fluid (i.e., temperature of the fluid is lower than outdoor air temperature) and optionally switches to circulating a heating fluid (i.e., temperature of the fluid is greater than outdoor air temperature).
In another embodiment, the thermal management system operates as part of the ceiling, roof, or ground floor to dynamically redirect, reduce, and/or shape heat transfer through the building envelope. The thin layer(s) of thermally conductive material includes a thickness of between 5 microns and 500 microns, inclusive, further optionally about 100 microns, and the polyisocyanurate foam or any insulation board includes a thickness of between 0.25 inches and 7 inches, inclusive, further optionally 0.5 inches. The thermal loop can include a pipe (e.g., copper, crosslinked polyethylene (PEX)) for circulating a fluid at a dynamically controlled or floating temperature. The thermal loop can switch between a heat sink mode and a heat source mode depending on the outdoor ambient temperature and can turn off circulation at other times. As set forth below, finite element heat transfer simulations and large-scale laboratory experiments of the thermal management system of the present invention demonstrated the feasibility of greater than 20% reductions in envelope-related cooling energy with a negligible increase in wall thickness when compared to a wall with exterior continuous insulation. The embodiments of the present invention are well suited for both new constructions and existing constructions across a variety of climates to (1) significantly reduce envelope-generated heating and cooling loads and (2) provide grid services such as decreasing peak loads and shaping energy use.
Energy from the thermal loop can be harvested and used for domestic hot water systems, heat pump systems, thermoelectric cloth dryers, or any appliances and equipment that needs thermal energy. Energy from the thermal loop can also be harvested and stored in thermal energy storage systems that use phase-change materials, chemical energy storage, or other thermal energy storage systems to use the thermal energy at later time. If no device is available to utilize the harvested thermal energy, it can be discarded in the ground or outdoor air. To operate the thermal loop as heat source, waist heat from appliances, equipment, and/or ground can be utilized.
These and other features and advantages of the present invention will become apparent from the following description of the invention, when viewed in accordance with the accompanying drawings and appended claims.
This patent or application file contains at least one drawing executed in color. Copies of this patent or patent application with color drawing(s) will be provided by the Office upon request and payment of the necessary fee.
Referring to
The thermal management system 10 includes an anisotropic composite 12. As used herein, an “anisotropic composite” means a composite whose thermal conductivity is anisotropic, such that its in-plane thermal conductivity differs from its through-plane thermal conductivity. In the illustrated embodiment, the thermal conductivity (W/(m·K)) of the anisotropic composite 12 is greater in-plane than through-plane. To achieve this anisotropic thermal conductivity, the composite 12 is composed of alternating layers of a thermally conductive material 16 and an insulating material 18. The conductive material 16 is placed on the insulating material 18, being aluminum in the present embodiment, optionally with a thickness of between 5 microns and 500 microns, inclusive, further optionally 100 microns. The conductive material 16 can include other materials in other embodiments, for example copper foil. The insulating material 18 includes a polyisocyanurate foam board in the current embodiment. In other embodiments, the insulating material 18 includes rigid extruded polystyrene (XPS) or other foam insulation, for example extruded polystyrene foam, while in still other embodiments the insulating core material 18 can include fibrous insulation materials, for example polyester fibers or glass fibers. The composite 12 includes insulation boards a thickness of between 0.25 inches and 7 inches, inclusive, further optionally 0.5 inches.
Each anisotropic composite 12 is composed of alternating layers of an insulating material 18 and a thermally conductive material 16, which, during the cooling season, draws heat in-plane toward the thermal loop 14 and decreases the through-plane (inward) heat transfer to the building interior. The thermal management system 10 includes an anisotropic composite with three alternating layers of conductive and insulating materials 12 that are in contact with each other in the present embodiment. The anisotropic composite can be made of greater or fewer alternating layers of conductive and insulating materials in other embodiments. The thermal loop 14 is disposed along the side of the anisotropic composite 12, in direct contact with the edge of the conductive material 16. In other embodiments, the thermal loop 14 is disposed within a portion of the composite 12, between adjacent conductive materials, being entirely self-contained within the composite 12. In still other embodiments, one or more thermal loops 14 are disposed distal from the edges (as shown in
In the current embodiment, the thermal loop 14 includes one or more copper pipes 20 circulating water 22 (depicted in box 14 in
The thermal management system 10 is disposed between conventional building materials along an exterior of the building structure. As shown in
A method for installing the thermal management system 10 for new constructions or as a retrofit includes positioning the anisotropic composite 12 between a wall structure (or roof structure) and its exterior cladding 24. The anisotropic composite 12 comprises of alternating layers of an insulating material, for example polyisocyanurate foam, and a thermally conductive material, for example aluminum sheets. Three alternating layers of 0.5-inch-thick insulation boards and 0.04-inch-thick aluminum sheets are used at each wall section, but greater or fewer panels and panels of varying thicknesses can be used in other embodiments. Once secured to the wall structure, for example OSB 26 that is opposite cavity insulation 28, the method includes running a thermal loop 14 along the long edge or the entire perimeter of the composite 12. The method then includes applying the outer cladding to the outermost layer of the composite 12. The method further includes operating the thermal loop 14 in a cooling mode to maintain its temperature lower than the outdoor ambient temperature or operating the thermal loop 14 in a heating mode to maintain it at greater than the outdoor ambient temperature. In some operations, the thermal loop 14 turns off. Below a building balance point temperature, the thermal loop can be switched to a heat source with temperatures 10 C higher than outdoor temperatures.
Two geometries were constructed for modeling wall-generated cooling modes. As shown in
In this example, the thermal performance of the following systems were evaluated: (a) 0.25″ stucco over 0.5″ sheathing (“baseline”); (b) 0.25″ stucco over 1.5″ continuous insulation PIR board (“CI”); (c) 0.25″ stucco over three alternating layers of 0.5″ PIR panels and 0.04″ aluminum sheets and a heat sink of 10° C. below ambient (“PIR-Al(1)”); (d) and 0.25″ stucco over three alternating layers of 0.5″ PIR and 0.04″ aluminum sheets and a heat sink of 10° C. below ambient but turned off below 12.78° C. (55° F.) (“PIR-Al(2)”). These materials were assumed to extend over 0.625″ OSB, 3.5″ cavity insulation, and 0.5″ drywall.
In this example, the net heat transfer through a thermal anisotropic composite (“TAC”), discussed below, was measured by the net heating or cooling power (Qmeter) needed to maintain a meter chamber at or near the “room” temperature of 23.9° C. This example was performed in a large-scale climate simulator (LSCS) consisting of three chambers: climate, meter, and guard. The climate chamber was above ground and simulates outdoor weather conditions, the meter and guard chambers were below ground and simulated indoor temperature and humidity. The meter chamber was surrounded on five sides by the guard chamber except for the side facing up, which is exposed to the test specimen. During testing, the edge of the meter chamber is sealed against the indoor side of the wall assembly and provides a measurement of the total heat flow through the 2.44 m×2.44 m central measurement area of the test specimen. The LSCS serves as a guarded hot box apparatus and testing was performed in according with ASTM C1363. A positive Qmeter indicates net heat flow from the climate chamber to the meter chamber (heat gain) or a cooling load, while negative Qmeter indicates heat loss from the meter chamber or a heating load.
The TAC is shown in
The above description is that of current embodiments of the invention. Various alterations and changes can be made without departing from the spirit and broader aspects of the invention as defined in the appended claims, which are to be interpreted in accordance with the principles of patent law including the doctrine of equivalents. This disclosure is presented for illustrative purposes and should not be interpreted as an exhaustive description of all embodiments of the invention or to limit the scope of the claims to the specific elements illustrated or described in connection with these embodiments. For example, and without limitation, any individual element(s) of the described invention may be replaced by alternative elements that provide substantially similar functionality or otherwise provide adequate operation. This includes, for example, presently known alternative elements, such as those that might be currently known to one skilled in the art, and alternative elements that may be developed in the future, such as those that one skilled in the art might, upon development, recognize as an alternative. Further, the disclosed embodiments include a plurality of features that are described in concert and that might cooperatively provide a collection of benefits. The present invention is not limited to only those embodiments that include all of these features or that provide all of the stated benefits, except to the extent otherwise expressly set forth in the issued claims. Any reference to claim elements in the singular, for example, using the articles “a,” “an,” “the” or “said,” is not to be construed as limiting the element to the singular.
This application claims the benefit of U.S. Provisional Application 62/833,842, filed Apr. 15, 2019, the disclosure of which is incorporated by reference in its entirety.
This invention was made with government support under Contract No. DE-AC05-00OR22725 awarded by the U.S. Department of Energy. The government has certain rights in the invention.
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