Patent Application
20170040242
The invention relates generally to thermal management systems, and more particularly, to systems and methods for packaging synthetic jets.
As the size of semiconductor devices has continued to shrink and circuit densities have increased accordingly, thermal management of these devices has become more challenging. In the past, thermal management in semiconductor devices was often addressed through the use of forced convective air cooling, either alone or in conjunction with various heat sink devices, and was accomplished through the use of fans. However, fan-based cooling systems are undesirable due to the noise attendant to their use. Moreover, the use of fans requires relatively large moving parts, and correspondingly high power inputs, in order to achieve the desired level of heat transfer. As a result of the moving parts, fan reliability is also an issue Furthermore, while fans are adequate for providing global movement of air over electronic devices, they generally provide insufficient localized cooling to provide adequate heat dissipation for the hot spots that typically exist in semiconductor devices and in many types of electronic equipment.
More recently, thermal management systems have been developed which utilize synthetic jets. Such systems are more energy efficient than comparable fan-based systems, and also offer reduced levels of noise and electromagnetic interference. The use of synthetic jets has proven very efficient in providing localized heat dissipation, and hence can be used to address hot spots in semiconductor devices and electronic equipment. Synthetic jets may be used in conjunction with fan-based systems to provide thermal management systems that afford both global and localized heat dissipation.
Despite their notable advantages, however, there is a need in the art for further improvements in synthetic jet ejectors. In particular, synthetic jets need to be packaged in fins that provide reduced thermal resistance and steer fluid flow in the jet, for optimal performance. However, such packaging is complex.
Therefore, there is a need in the art for an optimally packaged thermal management system.
In accordance with an embodiment of the invention, a thermal management system is provided. The thermal management system includes at least one heat sink including one or more respective fins, wherein the one or more fins include one or more respective cavities. The thermal management system also includes a synthetic jet stack including at least one synthetic jet mounted within each of the respective cavities employing at least one engaging structure to provide a rigid positioning of the synthetic jet stack within the fins, wherein the synthetic jet includes at least one orifice through which a fluid is ejected.
In accordance with another embodiment of the invention, a method for manufacturing a thermal management system is provided. The method includes disposing at least one heat sink comprising one or more respective fins, each of the fins including one or more respective cavities. The method also includes mounting a synthetic jet stack including at least one synthetic jet within each of the respective cavities, employing at least one engaging structure to provide a rigid positioning of the synthetic jet stack within the fins, wherein the synthetic jet includes at least one orifice through which a fluid is ejected.
These and other features, aspects, and advantages of the present invention will become better understood when the following detailed description is read with reference to the accompanying drawings in which like characters represent like parts throughout the drawings, wherein:
As discussed in detail below, embodiments of the invention include systems and methods for packaging synthetic jet embedded fins. The systems and methods include various techniques of mechanically coupling the synthetic fin within the fins to provide high performance cooling. Although embodiments illustrated below include one synthetic jet attached to a single fin, it should be noted that the techniques are applicable to multiple synthetic jets attached to multiple fins and heat sinks.
In the illustrated embodiment, the synthetic jet 16 is inserted into the fin 28 via the wire frame 12. For example, the wire frame or array of wires includes three wires 32, 34, 36 attached to the synthetic jet through holes (not shown) on the fin 28. Non-limiting example of material used in the wires 32, 34, and 36 are copper and aluminum. In another example, the fin is made of aluminum. The synthetic jet 16 also includes multiple orifices 19 through which a fluid 23 is ejected. In one embodiment, the fluid is air. To increase robustness, a slot at a base center 37 of the fin 28 may be opened and a similar wire frame 12 may be employed therein. It will be appreciated that although one heat sink, one fin and synthetic jet is illustrated herein, there may be any number of heat sinks, fins and synthetic jets employed.
In another embodiment, the engaging structure is employed by disposing multiple locator pins on an outer surface of the synthetic jet, and the locator pins are fit into multiple respective holes drilled into the heat sink. In another embodiment, the engaging structure is employed by adhering a sheet of non-conductive tape to each outer surface of the synthetic jets, and a layer of silicone is applied at a top opening side of the fins to enclose the synthetic jets into the cavities. In yet another embodiment, the engaging structure is employed by forming extrusions in the synthetic jets, and the extrusions are fit into multiple external support slots on at least one of a top and a bottom surface of the fins, and a silicone adhesive is applied to the slots to ensure a rigid attachment. In another embodiment, the engaging structure is employed by disposing a fin cap on a top opening of each of the respective fins such that the synthetic jets are rigidly disposed within the fins, wherein the fin cap includes one or more holes to facilitate electrical connection to the synthetic jets. In yet another embodiment, the engaging structure is employed by disposing a top plate comprising multiple fin caps configured to cover each of the fins, such that the synthetic jets are rigidly disposed within the fins, the fin cap including one or more holes to facilitate electrical connection to the synthetic jets.
The various embodiments of a thermal management system and method described above thus provide a way to achieve a convenient and efficient means of packaging synthetic jet embedded fins. This technique also provides energy efficient cooling of electronic devices. Further, such systems may be employed with low power fans in electronics to provide the desirable high performance cooling.
It is to be understood that not necessarily all such objects or advantages described above may be achieved in accordance with any particular embodiment. Thus, for example, those skilled in the art will recognize that the systems and techniques described herein may be embodied or carried out in a manner that achieves or optimizes one advantage or group of advantages as taught herein without necessarily achieving other objects or advantages as may be taught or suggested herein.
Furthermore, the skilled artisan will recognize the interchangeability of various features from different embodiments. Similarly, the various features described, as well as other known equivalents for each feature, can be mixed and matched by one of ordinary skill in this art to construct additional systems and techniques in accordance with principles of this disclosure.
While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
The present application is a continuation of, and claims priority to, U.S. patent application Ser. No. 12/911,995, filed Oct. 26, 2010, the disclosure of which is incorporated herein by reference in its entirety.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 12911995 | Oct 2010 | US |
| Child | 15298677 | US |
