The present invention relates to air-cooled heat-exchange systems used to remove heat from electronic devices that generate heat during operation.
Over the past 40 years, many electronic technologies such as telecommunications, and active sensing and imaging have undergone tremendous technological innovation. During this same time, the technologies, designs and performance of air-cooled heat exchangers has remained fundamentally unchanged. Performance data for present day heat exchangers and blowers is based on that old technology.
Because of the improved performance and increased power consumption of electronic technologies, heat rejection systems have grown in size, weight, complexity and cost. In some instances, conventional air-cooled heat sinks have become inadequate. This has resulted in more exotic liquid-cooled manifolds, spray-cooled enclosures, and vapor-compression refrigeration being proposed. All these newly proposed cooling approaches add complexity associated with operation of active pumps and compressors, as well as the need to prevent fluid or vapor leakage. Reliability of those approaches has not been demonstrated at this time.
Conventional designs rely on high heat transfer impingement flows generated by axial fans placed above the heat sink. Airflow at the fan outer diameter passes over a portion of the available heat transfer area, thus requiring high airflow rates and high fan power input.
An integrated centrifugal blower-diffuser with a vaned heat-sink provides cooling of electronics and other devices that generate heat during use. Airflow is introduced radially onto the heat sink such that the centrifugal blower and fin-diffuser direct the bulk of the airflow outward across the available heat transfer area of the device. Air is induced through space in the shaft of an electric motor, and the air is then accelerated centrifugally through a set of rotating impellor vanes, and then diffused radially through a set of radial heat sink fins. The radial heat sink fins form the spiral diffuser fins (or vanes) to provide pressure recovery within the heat sink. This enables tight intra-vane spacing and increased heat transfer surface area.
The device may also include passive vanes, surface features and microfabricated active elements to provide heat transfer enhancement at reduced air flow rates, thus providing reduced thermal resistance of the heat sink device.
Air cooling system 10 for cooling component C is shown in
Motor 11 is shown as a toroidal electric motor with a central airway 12 around its rotational axis. Air is drawn by rotation of blower 13 axially down through central airway 12 into blower 13 and then into diffuser 15. Air flows outward. Other motors may also be used, with different configurations and sources of power, depending on the size and shape of the object to be cooled. Controller 31 provides a source of energy via line 29 to drive motor 11 and other active components described below. In operation, motor 11 causes air to be drawn into central airway 12 by blower 13, passing through a central aperture in cover 14 into diffuser 15. The air flows through diffuser 15 and in contact with heat sink base 17 to cool component C. Airflow through diffuser 15 can be radial, spiral or diffuser 15 can be configured for other paths.
As seen in
Blower 13 has an upper hub 13a, lower hub 13b and blades 16. Upper hub 13a is connected to the permanent magnet rotor 19. Blades 16 have an upper end 16a connected to lower hub 13b. A center port 13c in lower hub 13b provides a passage for air flow through lower hub 13b and into space between lower hub 13b and heat sink base 17.
Diffuser 15 includes a plurality of fins or vanes 23 and other elements shown and described below that take air from central passage 12 so that air contacts the vanes 23 and the heat sink base 17 to absorb heat into the air and out of system 10. Diffuser 15 serves two purposes in this device. First, diffuser 15 deflects the flow of air from a vertically downward direction radially outward as will be described below, Second, the diffuser vanes 23 provide additional heat conductive material as part of the heat sink 17, so that more hot metal is exposed to the cooling air flow. This is a significant improvement over conventional designs that simply direct the air flow axially to impinge on a heat sink. The motor 11, blower 13, diffuser 15 and heat sink 17 are attached together to form a single device that can be attached to an electronic package such as a circuit board in the same manner that conventional air-cooled heat-exchangers are attached.
Air flow in
In addition to the basic flow pattern as seen in
In
Reeds 27 are designed to function as vibrating reeds in the space between adjacent fins to further improve heat transfer. In one embodiment, reeds 27 are formed from a silicon material having a piezoelectric component bonded to the silicon so that when the piezoelectric component is actuated by an electric signal in wire 29 from controller 31 in
The combination of dimples 24 on vanes 23, splitter plates 23a and 23b, and the vibrating reeds 27 function as highly integrated active fin, and operate through the introduction of high frequency, unsteady flow within the channels formed by them. This greatly enhances mixing and heat transfer from their walls to the air. This well-mixed air is swept through the thus formed channels by the bulk airflow provided by the blower 13.
A simulated comparison between the present system described above and in the figures and a conventional air-cooled exchanger system shows significant improvement achieved by the present invention.
A conventional device has a thermal resistance of 0.2° C./W, which gives a temperature rise of 230° C., which is above the allowed operating temperature of many electronic devices. The system of this invention is estimated to have a thermal resistance of 0.05° C./W, resulting in a theoretical temperature rise of only 50° C. The system would be usable with many more electronic devices. The Coefficient of Performance (COP) is the electronic device power dissipation divided by the blower and heat sink power. For the conventional system, the COP is 100. Simulated results for the system of this invention is estimated to produces a COP of as low as 30, which results in an estimated power consumption reduction of more than a factor of three. These results are due to the substantial reduction in the airflow and increasing the back-pressure on the blower. This significantly improves operating point efficiency as well as providing a reduction in thermal resistance.
Although the present invention has been described with reference to preferred embodiments, workers skilled in the art will recognize that changes may be made in form and detail without departing from the spirit and scope of the invention.
The U.S. Government has a paid-up license in this invention and the right in limited circumstances to require the patent owner to license others on reasonable terms as provided for by the terms of [Contract No. or Grant No.] ______ awarded by Defense Advanced Research Projects Agency/Microsystems Technology Office.