The present disclosure relates generally to the thermal management of illumination devices, and more particularly to the thermal management of LED-based illumination devices through the use of synthetic jet ejectors.
A variety of thermal management devices are known to the art, including conventional fan based systems, piezoelectric systems, and synthetic jet ejectors. The latter type of system has emerged as a highly efficient and versatile solution, especially in applications where thermal management is required at the local level.
Various examples of synthetic jet ejectors are known to the art. Earlier examples are described in U.S. Pat. No. 5,758,823 (Glezer et al.), entitled “Synthetic Jet Actuator and Applications Thereof”; U.S. Pat. No. 5,894,990 (Glezer et al.), entitled “Synthetic Jet Actuator and Applications Thereof”; U.S. Pat. No. 5,988,522 (Glezer et al.), entitled Synthetic Jet Actuators for Modifying the Direction of Fluid Flows”; U.S. Pat. No. 6,056,204 (Glezer et al.), entitled “Synthetic Jet Actuators for Mixing Applications”; U.S. Pat. No. 6,123,145 (Glezer et al.), entitled “Synthetic Jet Actuators for Cooling Heated Bodies and Environments”; and U.S. Pat. No. 6,588,497 (Glezer et al.), entitled “System and Method for Thermal Management by Synthetic Jet Ejector Channel Cooling Techniques.
Further advances have been made in the art of synthetic jet ejectors, both with respect to synthetic jet ejector technology in general and with respect to the applications of this technology. Some examples of these advances are described in U.S. Pat. No. 7,252,140 (Glezer et al.), entitled “Apparatus and Method for Enhanced Heat Transfer”; U.S. Pat. No. 7,606,029 (Mahalingam et al.), entitled “Thermal Management System for Distributed Heat Sources”; U.S. Pat. No. 7,607,470 (Glezer et al.), entitled “Synthetic Jet Heat Pipe Thermal Management System”; U.S. Pat. No. 7,760,499 (Darbin et al.), entitled “Thermal Management System for Card Cages”; U.S. Pat. No. 7,768,779 (Heffington et al.), entitled “Synthetic Jet Ejector with Viewing Window and Temporal Aliasing”; U.S. Pat. No. 7,784,972 (Heffington et al.), entitled “Thermal Management System for LED Array”; U.S. Pat. No. 7,819,556 (Heffington et al.), entitled “Thermal Management System for LED Array”; U.S. Pat. No. 7,932,535 (Mahalingam et al.), entitled “Synthetic Jet Cooling System for LED Module”; U.S. Pat. No. 8,030,886 (Mahalingam et al.), entitled “Thermal Management of Batteries Using Synthetic Jets”; U.S. Pat. No. 8,035,966 (Reichenbach et al.), entitled “Electronics Package for Synthetic Jet Ejectors”; U.S. Pat. No. 8,006,410 (Booth et al.), entitled “Light Fixture with Multiple LEDs and Synthetic Jet Thermal Management System”; U.S. Pat. No. 8,069,910 (Beltran et al.), entitled “Acoustic Resonator for Synthetic Jet Generation for Thermal Management”; and U.S. Pat. No. 8,136,576 (Grimm), entitled “Vibration Isolation System for Synthetic Jet Devices”.
In addition to the foregoing, other advances have been made in the art of synthetic jet ejectors, both with respect to synthetic jet ejector technology in general and with respect to the applications of this technology. Some examples of these advances are described in U.S. 20100263838 (Mahalingam et al.), entitled “Synthetic Jet Ejector for Augmentation of Pumped Liquid Loop Cooling and Enhancement of Pool and Flow Boiling”; U.S. 20100039012 (Grimm), entitled “Advanced Synjet Cooler Design For LED Light Modules”; U.S. 20100033071 (Heffington et al.), entitled “Thermal Management of LED Illumination Devices”; U.S. 20090141065 (Darbin et al.), entitled “Method and Apparatus for Controlling Diaphragm Displacement in Synthetic Jet Actuators”; U.S. 20090109625 (Booth et al.), entitled Light Fixture with Multiple LEDs and Synthetic Jet Thermal Management System”; U.S. 20090084866 (Grimm et al.), entitled Vibration Balanced Synthetic Jet Ejector”; U.S. 20080219007 (Heffington et al.), entitled “Thermal Management System for LED Array”; U.S. 20080151541 (Heffington et al.), entitled “Thermal Management System for LED Array”; U.S. 20080043061 (Glezer et al.), entitled “Methods for Reducing the Non-Linear Behavior of Actuators Used for Synthetic Jets”; U.S. 20080009187 (Grimm et al.), entitled “Moldable Housing design for Synthetic Jet Ejector”; U.S. 20070096118 (Mahalingam et al.), entitled “Synthetic Jet Cooling System for LED Module”; U.S. 20070023169 (Mahalingam et al.), entitled “Synthetic Jet Ejector for Augmentation of Pumped Liquid Loop Cooling and Enhancement of Pool and Flow Boiling”; U.S. 20070119573 (Mahalingam et al.), entitled “Synthetic Jet Ejector for the Thermal Management of PCI Cards”; U.S. 20070119575 (Glezer et al.), entitled “Synthetic Jet Heat Pipe Thermal Management System”; U.S. 20070127210 (Mahalingam et al.), entitled “Thermal Management System for Distributed Heat Sources”; and U.S. 20070141453 (Mahalingam et al.), entitled “Thermal Management of Batteries using Synthetic Jets”.
In one aspect, an illumination device is provided which comprises (a) a light emitting portion; (b) an LED disposed within said light emitting portion; (c) a threaded connector module adapted to rotatingly engage said illumination device to a source of electricity; (d) a heat sink disposed between said light emitting portion and said connector module; and (e) a synthetic jet ejector disposed between said light emitting portion and said connector module.
In another aspect, an illumination device is provided which comprises (a) a housing having an LED disposed therein, wherein said housing is transmissive to light generated by said LED; (b) a threaded connector module which rotatingly engages a complimentary shaped electrical socket; (c) a heat sink disposed between said housing and said connector module, wherein said heat sink comprises a plurality of fins; and (d) a synthetic jet ejector which directs a synthetic jet into a channel formed by a pair of adjacent fins, wherein said synthetic jet ejector is disposed between said housing and said connector module.
Prior to describing the devices and methodologies described herein, a brief explanation of a typical synthetic jet ejector, and the manner in which it operates to create a synthetic jet, may be useful.
The formation of a synthetic jet may be appreciated with respect to
The movement of the flexible diaphragm 3811 may be controlled by any suitable control system 3817. For example, the diaphragm may be moved by a voice coil actuator. The diaphragm 3811 may also be equipped with a metal layer, and a metal electrode may be disposed adjacent to, but spaced from, the metal layer so that the diaphragm 3811 can be moved via an electrical bias imposed between the electrode and the metal layer. Moreover, the generation of the electrical bias can be controlled by any suitable device, for example but not limited to, a computer, logic processor, or signal generator. The control system 3817 can cause the diaphragm 3811 to move periodically or to modulate in time-harmonic motion, thus forcing fluid in and out of the orifice 3809.
Alternatively, a piezoelectric actuator could be attached to the diaphragm 3811. The control system would, in that case, cause the piezoelectric actuator to vibrate and thereby move the diaphragm 3811 in time-harmonic motion. The method of causing the diaphragm 3811 to modulate is not particularly limited to any particular means or structure.
The operation of the synthetic jet ejector 3811 will now be described with reference to
While thermal management systems which utilize synthetic jets to enhance cooling have many desirable properties, further improvements in these devices are required to meet evolving challenges in the art. For example, many host devices which require thermal management continue to shrink in size. Hence, there is a need in the art to provide thermal management solutions based on synthetic jet ejectors which have reduced dimensions, without sacrificing functionality.
It has now been found that some of the foregoing needs may be met by a thermal management system having a synthetic jet ejector and a heat sink, and in which the synthetic jet ejector and heat sink are combined into a single unit. This may be accomplished, for example, by a thermal management system design which comprises (a) a heat sink comprising a central chamber and having a plurality of heat fins disposed about the perimeter of said central chamber; (b) a synthetic jet actuator disposed in said central chamber; (c) a first plurality of conduits adapted to direct a first plurality of synthetic jets in a first direction across the surfaces of said heat fins; and (d) a second plurality of conduits adapted to direct a second plurality of synthetic jets in a second direction across the surfaces of said heat fins; wherein said first and second directions are essentially orthogonal. Such a configuration may provide improved thermal performance, while also allowing the device to be smaller and to have more entrainment.
It has further been found that some of the foregoing needs may be met through the provision of a light source which comprises (a) an Edison socket; (b) a heat sink disposed adjacent to said socket; and (c) a synthetic jet actuator disposed at least partially within said heat sink or at least partially within said socket, wherein said socket has at least one nozzle defined therein which is adapted to direct at least one synthetic jet across a surface of said heat sink. Currently, the Edison socket serves two functions, namely to make electrical contact to the main power and to house some electronics. In the design disclosed herein, however, some internal volume of the Edison socket is utilized to form synthetic jet nozzles for cooling the heat sink. Hence, the resulting Edison socket has built in nozzles for directing airflow over the heat sink.
It has also been found that some of the foregoing needs may be met through the provision of a heat sink as the synthetic jet actuator support structure. In order to reduce size and cost, if possible, it is advantageous to combine the function of multiple components of a synthetic jet actuator into one integrated component. Many existing synthetic jet actuators have various plastic support structures to support the diaphragm. It has now been found that these components may be designed as part of the heat sink, wherein the heat sink can be metal or can be injection molded with a thermally conductive polymeric composition. Alternatively, a similar end may be met by providing a metal substrate having a plurality of heat fins defined therein, and overmolding the metal substrate with a thermally conductive polymeric resin to form a heat sink containing a plurality of heat fins and having a first cavity defined therein which is in fluidic communication with the surfaces of said fins by way of a first set of channels.
It has further been found that some of the foregoing needs may be met with a thermal management system equipped with one or more diaphragms having a long surround with a small bend radius. Such a construction allows for a larger usable piston area and a smaller diameter assembly.
It has further been found that some of the foregoing needs may be met with an illumination device equipped with a translucent dome, an electrical connector and a heat sink disposed between the dome and the electrical connector. The heat sink is equipped with a synthetic jet ejector which ejects a first plurality of synthetic jets in a first direction along the surface of the illumination device, and a second plurality of synthetic jets in a second direction along the surface of the illumination device. The different directional movement of the jets allows for a circular airflow pattern around the illumination device. In some applications in which the illumination device is installed into a fixture, having jets formed to move air into the fixture may create thermal heating of the air and hence remove heat more efficiently from the illumination device.
It has also been found that some of the foregoing needs may be met with a heat sink design which allows for the compression fit assembly of a diaphragm to housing components. Such an assembly allows for a snap fit or threaded fit type of installation which eliminates the need for adhesives, overmolding or ultrasonic welding.
The devices and methodologies disclosed herein may be further understood with reference to the particular, non-limiting embodiments of the illumination devices depicted in
The light emitting portion 101 in this embodiment houses a pedestal 125 (see
The light emitting portion 201 in this embodiment contains a synthetic jet actuator housing 211 which contains a set of diaphragms 213, and upon an exterior surface of which are disposed a plurality of LEDs 215. The set of diaphragms 213 operate to generate a plurality of synthetic jets 217, which are emitted from a plurality of apertures (not shown) provided in the synthetic jet actuator housing 211, and which transfer heat from the LEDs 215 to the interior of the light emitting portion 203. The apertures may be disposed in a variety of suitable patterns around one or more of the LEDs 215, one particular example of which is depicted in
The embodiment of
The connector module 305 in this embodiment contains a synthetic jet actuator 307 which is equipped with a set of diaphragms 313. The synthetic jet actuator 307 is in fluidic communication with a pedestal 325 which is equipped on one end with a plenum 312. The plenum 312 is equipped with a plurality of apertures 320, and has a plurality of LEDs 315 disposed on an exterior surface thereof. The set of diaphragms 313 operate to generate a plurality of synthetic jets 317, which are emitted from a plurality of apertures 320 provided in the plenum 312, and which transfer heat from the LEDs 315 to the interior of the light emitting portion 303. The apertures 320 may be disposed in a variety of suitable patterns around one or more of the LEDs 315. The heat in the interior of the light emitting portion 303 may then be transferred to the external environment through thermal conduction, through the provision of apertures or vents in the light emitting portion 303, or by other suitable means.
The embodiment of
This embodiment is similar to the embodiment of
[[FIG. A5-1]]
The illumination device 501 in this embodiment is a hybrid of the embodiments depicted in
The illumination device 501 in this embodiment is also equipped with a vent 523 which allows the atmosphere inside of the light emitting portion 503 to be in fluidic communication with the external atmosphere. In some variations of this embodiment, the synthetic jet ejector 509 may be adapted to emit synthetic jets from apertures in the vent 523, either solely or in addition to emitting synthetic jets 517 from the actuator housing 511.
The illumination device 601 in this embodiment is similar in many respects to the illumination device 501 of
The light emitting portion 701 in this embodiment contains an active diaphragm 733 and a passive diaphragm 735 which are in fluidic communication with each other. A heat sink 759 comprising at least one heat fin 727 is disposed between the active diaphragm 733 and the passive diaphragm 735 and has a plurality of LEDs 715 disposed thereon. Each heat fin 727 has at least one channel 737 defined therein which is in fluidic communication with the environment external to the light emitting portion.
In operation, the active diaphragm 733 vibrates to produce a plurality of synthetic jets 717 in the air passing through the channels 737 and into the external environment. Hence, as the heat fins 727 absorb heat from the LEDs 715 mounted on the heat sink 759, this operation ensures that the heat is efficiently transferred to the external environment through the turbulent flow created by the synthetic jets 717. During operation, the larger passive diaphragm 735 basically serves as a counterweight to the active diaphragm 733, which allows the synthetic jet actuator 709 to provide sufficient heat flux while operating outside of the audible range and producing fewer vibrations.
The passive diaphragm 735 preferably has the same mass as the active diaphragm 733, although the dimensions of the two diaphragms may be the same or different. The passive diaphragm 735 may also be of the same or different construction as the active diaphragm 733. In some implementations of the embodiment, the passive diaphragm 735 may comprise a transparent or translucent material.
The illumination device 801 in this embodiment is equipped with a combination synthetic jet ejector/heat sink 829 which contains both a synthetic jet ejector 809 and a heat sink 827. These two components may be combined in a variety of ways, and each of these components, or the combination thereof, may have a variety of shapes or sizes. The two components may also comprise a variety of materials, though the heat sink 827 preferably comprises a thermally conductive material such as a metal (such as, for example, copper, aluminum, tin, steel, or various combinations or alloys thereof) or a thermally conductive loaded polymer. In the particular embodiment depicted, however, the heat sink 827 extends from one side of the synthetic jet ejector 809 and is adapted to direct synthetic jets 817 through channels 837 defined in the heat sink 827. Since the LED 815 is mounted on top of the heat sink 827 and is in thermal communication therewith, this arrangement transfers heat from the LED 815 to the atmosphere external to the illumination device 801.
In the embodiment depicted in
The illumination device 901 of this embodiment is similar in most respects to the illumination device 801 of
In this embodiment, a heat sink 1059 is disposed about the exterior of the light emitting portion 1003 and the synthetic jet ejector 1009 is disposed within the light emitting portion 1003. However, the synthetic jet ejector 1009 is in fluidic communication with the heat sink 1059 by way of one or more channels 1037. In the particular embodiment depicted, these channels 1037 extend from the interior of the light emitting portion to the exterior of the light emitting portion 1003, and are adapted to direct one or more synthetic jets across the surfaces of the heat sink 1059 or the heat fins 1027 thereof.
The illumination device 1101 of this embodiment is similar in most respects to the illumination device 901 of
This embodiment illustrates the application of the principles described herein to a popular type of compact fluorescent light bulb. The synthetic jet actuator 1207 in this embodiment is equipped with a set of nozzles 1241 which are adapted to direct a plurality of synthetic jets 1217 across the surfaces, or into the interior of, the helical coil of the light emitting portion 1203. The nozzles 1241 are in fluidic communication with the interior of the synthetic jet actuator 1207 where the diaphragms 1213 are disposed, and the LEDs 1215 which illuminate the light emitting portion 1203 are disposed in, or adjacent to, this fluidic path.
In operation, the synthetic jet actuator 1207 operates to create a fluidic flow adjacent to, or across the surfaces of, the LEDs 1215, thereby removing heat from the LEDs and rejecting it to the external environment. The hot fluid is ejected as a synthetic jet 1217, and hence is removed a significant distance from the nozzles 1241. The synthetic jets also entrain cool air from the local environment and create a turbulent flow around the surfaces of the helix of the light emitting portion, thus helping to cool this portion of the illumination device 1201 as well. The synthetic jets also draw in cool fluid around the nozzles 1241, which is then drawn into the synthetic jet ejector during the in-flow phase of the diaphragms 1213.
The illumination device of
Various modifications may be made to the embodiment depicted in
The illumination device 1405 of
In some variations of this embodiment, the helical coils of the light emitting portion 1403 may comprise a suitably thermally conductive material. Such a material may provide for more efficient transfer of heat from the LEDs 1439 to the underlying substrate, where it may be rejected to the external atmosphere by the fluidic flow created by the synthetic jet actuator 1407. In other variations, the LEDs 1439 may be directed inward so that their backsides are exposed to the internal environment, and their light emitting surfaces are directed towards the interior of the helical coil. In these different embodiments, a metallic interconnect may be disposed on the interior or exterior surface of the coils, or may be embedded in the walls of the coils.
In this embodiment, the synthetic jet actuator 1507 is centrally disposed within the light emitting portion 1503, and a plurality of LEDs 1515 are disposed around it. A heat sink 1559 is built into the base of the illumination device 1501, and is equipped with channels 1537 which are in fluidic communication with the synthetic jet actuator 1507. During operation, the synthetic jet actuator 1507 creates a fluidic flow which preferably includes synthetic jets 1517, and which rejects heat from the heat sink 1559 to the external environment.
As indicated in
One wall of the synthetic jet ejector 1609 is equipped with a heat sink 1659 comprising a plurality of heat fins 1627. The heat fins 1627 are disposed adjacent to an LED 1615 and define a plurality of channels 1637 which are in fluidic communication with the interior of the synthetic jet ejector 1609.
During operation, the heat sink 1659 absorbs heat from the LEDs 1615, and the synthetic jet ejector 1609 generates a plurality of synthetic jets 1617 in the channels 1637 which transfers the heat to the interior environment of the light emitting portion 1603. From there, the heat is rejected to the external environment through thermal transfer. In some implementations, thermal transfer to the external environment may be facilitated by the provision of suitable venting in the light emitting portion 1603 or by other suitable means. As with the previous embodiment, the design of this illumination device 1601 allows for the use of relatively large diaphragms 1613 in the synthetic jet ejector 1609, which may be useful in achieving high heat flux from the heat sink 1659 to the external environment.
In this embodiment, the synthetic jet ejector 1709 is centrally disposed within a heat sink 1759 having a plurality of external heat fins 1727. The external heat fins 1727 have a plurality of channels 1737 defined therein which are in fluidic communication with the interior of the synthetic jet ejector 1709 and the external environment. An LED 1715 is disposed on top of the heat sink.
In operation, the heat sink 1759 absorbs heat given off by the LED 1715, and this heat is transferred to the heat fins 1727. The synthetic jet ejector 1709 creates a plurality of synthetic jets 1717 in the channels 1737 which rejects the heat to the external environment. As with the previous embodiment, the design of this illumination device 1701 allows for the use of relatively large diaphragms 1713 in the synthetic jet ejector 1709, which may be useful in achieving high heat flux from the heat sink 1759 to the external environment.
In this embodiment, the synthetic jet ejector 1809 is centrally disposed within a heat sink 1859 having a plurality of external heat fins 1827. The portion of the heat sink 1859 which separates the light emitting portion 1803 from the heat fins 1827 is porous, and hence provides for fluidic flow between the interior of the light emitting portion 1803 and the external environment as indicated by arrows 1863. This may be achieved, for example, by forming this portion of the heat sink 1859 out of a foamed, thermally conductive material, such as a foamed metal, or by providing a plurality of apertures or vents in this portion of the heat sink 1859. An LED 1815 is disposed on top of the heat sink 1859.
Similarly, the interior of the light emitting portion 1803 is in fluidic communication with the interior of the synthetic jet ejector 1809. This may be accomplished, for example, by seating the LED 1815 on a metal plate or heat spreader which is in thermal contact with the heat fins 1827, and which has a plurality of apertures 1837 therein adjacent to the LED 1815 which are in fluidic communication with the interior of the synthetic jet ejector 1809.
In operation, the heat sink 1859 absorbs heat given off by the LED 1815, and this heat is transferred to the heat fins 1847. The synthetic jet ejector 1809 emits a plurality of synthetic jets 1817 from the channels 1837, which in turn creates a flow of fluid across the heat fins 1827. The synthetic jets 1817 also facilitate the transfer of heat from the LED 1815 to the interior atmosphere of the light emitting portion 1803, where the warmed fluid can then exit the light emitting portion 1803 to the external environment as indicated by the arrows 1863. This fluidic flow also facilitates the transfer of heat from the heat fins 1827 to the external environment. As with the previous embodiment, the design of this illumination device 1801 allows for the use of relatively large diaphragms 1813 in the synthetic jet ejector 1809, which may be useful in achieving high heat flux from the heat sink 1859 to the external environment.
In this embodiment, the synthetic jet ejector 1909 is centrally disposed within a heat sink 1959 having a plurality of external heat fins 1927. The heat sink 1959 has a plurality of channels defined therein by the space between adjacent heat fins 1927. These channels are in fluidic communication with the external environment, and are also in fluidic communication with the interior of the synthetic jet ejector 1909 by way of a plurality of nozzles 1941 disposed at the top and bottom of the channels. An LED 1915 is disposed on top of the heat sink.
In operation, the heat sink 1959 absorbs heat given off by the LED 1915, and this heat is transferred to the heat fins 1927. The synthetic jet ejector 1909 creates a plurality of synthetic jets 1917 in the channels of the heat sink 1959 which rejects the heat to the external environment.
Various flow patterns are possible with this embodiment. Preferably, for any pair of heat fins which are coplanar (as shown in the figure) or on opposing sides of the heat sink, one heat fin has a synthetic jet directed in a first direction parallel to its major surface, and the second heat fin has a synthetic jet directed in a second direction parallel to its major surface, where the first and second directions are preferably opposing directions. It is also preferred that the heat fins on a first half of the device have synthetic jets directed across their major surfaces in the first direction, and that the heat fins on a second half of the device have synthetic jets directed across their major surfaces in the second direction, since this helps to create a circular flow pattern around the device. However, embodiments are also possibly where the directions of the jets alternate between each channel formed by adjacent pairs of fins.
A synthetic jet ejector 2009 is centrally disposed between the heat sink 2059 and the connector module 2005. The heat sink 2059 has a plurality of channels defined therein by the space between adjacent heat fins 2027. These channels are in fluidic communication with the external environment, and are also in fluidic communication with the interior of the synthetic jet ejector 2009 by way of the interior of the connector module k1-05 as indicated by arrows 2063. An LED 2015 is disposed on top of the heat sink 2059.
In operation, the heat sink 2059 absorbs heat given off by the LED 2015, and this heat is transferred to the heat fins 2027. The synthetic jet ejector 2009 creates a plurality of synthetic jets 2017 in the channels of the heat sink 2059 which rejects the heat to the external environment.
The illumination device 2101 in this embodiment is equipped with a heat sink 2159 comprising a plurality of heat fins 2127, and upon which is disposed an LED 2115. The illumination device 2101 comprises an interior housing element 2155 and an exterior housing element 2157 which, between them, define a channel 2137 for fluidic flow. The channel 2137 is in fluidic communication with the synthetic jet actuator 2107 by way of a series of internal apertures 2109, and is further in fluidic communication with a plurality of nozzles 2141 disposed about the interior of the light emitting portion 2103.
In operation, the synthetic jet actuator 2107, which is driven by one or more diaphragms 2113, creates a plurality of synthetic jets 2117 at the nozzles 2141. The synthetic jets 2117 are directed at, or across, the surfaces of the LED 2115, and especially the light emitting surface thereon. The synthetic jets 2117 facilitate the transfer of heat from the LED 2115 to the interior atmosphere of the light emitting portion 2103, where it can be dissipated through thermal transfer to the internal 2155 and external 2157 housing elements and to the external environment, or through absorption by the heat sink 2159. The heat sink 2159 serves to absorb heat directly from the backside of the LED 2115. In some implementations of this embodiment, the heat sink 2159 may be equipped with one or more heat pipes.
In operation, the light emitted from the LEDs 2215 is reflected off of the reflective surface 2245 and is emitted through the exterior wall of the light emitting portion 2203. The degree of specular or diffuse reflectivity of these two surfaces may be selected to achieve a desired illumination footprint. Heat is withdrawn from the LEDs 2215 by the heat sink 2259. The synthetic jet ejector 2209 creates a fluidic flow across the surfaces of the heat fins 2227 as indicated by the arrows 2263, thus rejecting the heat to the external environment. Preferably, this flow 2263 is in the form of one or more synthetic jets.
In use, the synthetic jet ejector 2309 creates a plurality of synthetic jets 2317 in the vicinity of the LED 2315. The synthetic jets impinge on the surface of the depression 2351, and thus aid in the transfer of heat from the interior of the light emitting portion 2303 to the external environment.
In operation, the synthetic jet ejector 2409 creates a fluidic flow about the LEDs 2415 in the form of one or more synthetic jets 2417. This flow transfers heat from the LEDs 2413 to the surfaces of the tubing 2457 of the light emitting portion 2403, where it is rejected to the external atmosphere.
In operation, the synthetic jet ejector 2509 creates a fluidic flow about the LEDs 2515 in the form of one or more synthetic jets 2517. This flow transfers heat from the LEDs 2515 to the surfaces of the tubing 2557 of the light emitting portion 2503, where it is rejected to the external atmosphere.
In operation, the synthetic jet ejector 2609 creates a fluidic flow about the LEDs 2615 in the form of one or more synthetic jets 2617. This flow transfers heat from the LEDs 2615 to the surfaces of the tubing 2657 of the light emitting portion 2603, where it is rejected to the external atmosphere. The external vent 2623 provides an additional means by which heat may be rejected to the external environment.
In some variations of this embodiment, the illumination device 2601 may be adapted to emit synthetic jets from the external vent 2623. In other variations, the synthetic jet ejector provides a fluidic flow around the LEDs 2615, but only emits synthetic jets at the external vent 2623.
The various embodiments of light fixtures disclosed herein may be equipped with various reflective materials or surfaces. These include, without limitation, specularly or diffusely reflective or scattering materials. Such materials may be applied to the intended substrate as coatings or films. In some implementations, these coatings or films may be formed and then applied to the substrate, while in other implementations, they may be formed on the substrate in situ.
Examples of such scattering films include those based on continuous/disperse phase materials. Such films may be formed, for example, from a disperse phase of polymeric particles disposed within a continuous polymeric matrix. In some embodiments, one or both of the continuous and disperse phases may be birefringent. Such a film may be oriented, typically by stretching, in one or more directions. The size and shape of the disperse phase particles, the volume fraction of the disperse phase, the film thickness, and the amount of orientation may be chosen to attain a desired degree of diffuse reflection and total transmission of electromagnetic radiation of a desired wavelength in the resulting film. Films of this type, and methods for making them, are described, for example, in U.S. Pat. No. 6,031,665 (Carlson et al.), which is incorporated herein by reference in its entirety. Analogous films in which the disperse phase comprises inorganic or non-polymeric materials (such as, for example, silica, alumina, or metal particles) may also be utilized in the devices and methodologies described herein.
Reflective surfaces may also be imparted to the devices described herein through suitable metallization. These include, for example, films of silver or other metals which may be formed through vapor or electrochemical deposition.
The various embodiments of light fixtures disclosed herein may be equipped with various electrical connectors. These include, without limitation, threaded connectors that rotatingly engage complimentary shaped sockets in an electrical outlet; prong connectors, which may be male or female, and which mate with complimentary shaped prongs or receptacles in an electrical outlet; cord connectors; and the like. The choice of connector may vary from one application to another and may depend, for example, on the wattage output of the light fixture and other such considerations as are known to the art. It will be understood, however, that while embodiments of light fixtures may have been disclosed or illustrated herein as having a particular connector type, any other suitable connector, including those described above, may be substituted where suitable for a particular application.
The various embodiments of light fixtures disclosed herein may be equipped with various bulbs. These bulbs, or any portion thereof, may be clear, opaque, specularly or diffusively transmissive, specularly or diffusively reflective, polarizing, mirrored, colored, or any combination of the foregoing. In some embodiments, the bulb may also be equipped with a film or pigment which provides the light fixture with a desired optical footprint. These bulbs may also be equipped with any of the various types of phosphors as are known to the art, or with various combinations of such phosphors.
Various synthetic jet actuators and synthetic jet ejectors may be utilized in the devices and methodologies described herein. Preferably, however, the synthetic jet actuators and synthetic jet ejectors are of the type described in U.S. Ser. No. 61/304,427, entitled “SYNTHETIC JET EJECTOR AND DESIGN THEREOF TO FACILITATE MASS PRODUCTION” (Grimm et al.), which is incorporated herein by reference in its entirety. These synthetic jet actuators and synthetic jet ejectors may have various sizes, dimensions and geometries, and hence may be adapted to spaces available in the host device. Hence, for example, the synthetic jet ejector may be cylindrical, parallelepiped, or irregular in shape. Also, while the use of synthetic jet actuators which utilize voice coils is preferred, one skilled in the art will appreciate that synthetic jet actuators based on various piezoelectric materials may also be utilized.
As best seen in
Notably, in the particular illumination device 2701 depicted, elements of the host illumination device 2701 define the housing of the synthetic jet ejector 2709. Consequently, the overall space occupied by the synthetic jet ejector 2709 is significantly reduced compared to the situation that would exist if the synthetic jet ejector was made as a standalone unit (with its own housing) and subsequently incorporated into the host device. Moreover, in this embodiment, the upper wall 2775 (see
As seen in
Fluidic flow along a first axis parallel to the major surfaces of the heat fins 2807 may be achieved through the provision of a series of flow control devices (preferably in the form of apertures in the perimeter wall 2805) which may be configured to induce the formation of synthetic jets in the ambient media along a first axis (indicated by arrows 2812, 2814) parallel to the major surfaces of the heat fins 2807. Since the perimeter wall 2805 may assume virtually any shape (including, for example, circular, elliptical, irregular or polygonal (including, but not limited to, square, rectangular, pentagonal and hexagonal)), these synthetic jets may be directed in a plurality of directions. Preferably, though not necessarily, the heat fins 2807 will follow the contour of the perimeter wall 2805.
Fluidic flow along a second axis parallel to the major surfaces of the heat fins 2807 may be achieved through the provision of a series of flow control devices which may be configured to induce the formation of synthetic jets in the ambient media along a second axis (indicated by arrows 2816, 2818) parallel to the major surfaces of the heat fins 2807. An example of such a flow control device is disclosed in U.S. Ser. No. 12/503,832, entitled “Advanced Synjet Cooler Design for LED Light Modules” (Grimm), filed on Jul. 15, 2009. Such a flow control device may be utilized, for example, to direct fluidic flow which may include synthetic jets from a series of apertures disposed along the top and bottom of the device. Notably, the direction of flow indicated by arrows 2816, 2818 is preferably orthogonal to the fluidic flow along the first axis.
The synthetic jet ejector 2801 of
The various illumination devices described herein may be equipped with heat sources of various sizes, shapes and geometries. These heat sinks may be readily adapted to the space available within the illumination device or external to it. In some embodiments, these heat sinks may comprise a plurality of heat fins or other suitable heat dissipating structures.
In some applications, it may be desirable to mount the heat sink on the exterior of an illumination device. Examples of such embodiments may be found in
In some embodiments, the heat sink may be utilized as a support structure for the actuator, engine, diaphragm or other components of the synthetic jet ejector. Since many current synthetic jet ejectors have various support structures for these components, this approach helps to reduce the size and cost of synthetic jet ejectors. If desired, some of these components may also be formed out of thermally conductive materials (such as, for example, injection molded plastics with conductive fillers).
The heat sink 2959 in this embodiment comprises a first compartment 2983 which houses one or more LEDs 2915, and a second compartment 2985 which houses the voice coils 2967 and diaphragms 2969 of one or more synthetic jet actuators. A magnet 2981 associated with the one or more synthetic jet actuators is embedded in the material of the heat sink 2959. Also, as indicated by arrows 2963, flow paths are designed in the heat sink 2959. Such flow paths may be in the form of channels molded into the heat sink 2959, which may be closed along portions of their length, or which may be open along all, or a portion of, their lengths. Preferably, these channels are formed by pairs of adjacent heat fins 2927 along portions of their length.
The heat sink 3059 in this embodiment comprises a first compartment 3083 which houses one or more LEDs 3015, and a second compartment 3085 which houses the voice coils 3067 and diaphragms 3069 of one or more synthetic jet actuators. A magnet 3081 associated with the one or more synthetic jet actuators is embedded in the material of the heat sink 3059. Also, as indicated by arrows 3063, flow paths are designed in the heat sink 3059. Such flow paths may be in the form of channels molded into the heat sink 3059, which may be closed along portions of their length, or which may be open along all, or a portion of, their lengths. Preferably, these channels are formed by pairs of adjacent heat fins 3027 along portions of their length.
The heat sink 3159 in this embodiment comprises a first compartment 3183 which may be utilized to house one or more LEDs (not shown), and a second compartment 3185 which houses the voice coils 3167 and diaphragms 3169 of one or more synthetic jet actuators. As indicated by arrows 3163, flow paths are designed in the heat sink 3159. Such flow paths may be in the form of channels molded into the heat sink 3159, which may be closed along portions of their length, or which may be open along all, or a portion of, their lengths. Preferably, these channels are formed by pairs of adjacent heat fins 3127 along portions of their length.
This embodiment is advantageous in that the surround is long and has a small bend radius. Such a construction allows for a larger usable piston area. Moreover, the small radius allows for a smaller diameter assembly with more usable piston area.
With reference to
As seen in
With respect to
When the illumination device 3601 is installed in the light socket 3697, the synthetic jet actuator resident in the light socket 3697 creates a fluidic flow into the light emitting device 3601 as indicated by synthetic jets 3617. This fluidic flow dissipates heat from the heat sink 3659 and to the ambient environment.
The embodiment depicted in
In the embodiments of
The foregoing principles of incorporating synthetic jet ejectors and their components into the structure of host devices allows illumination devices to be produced which may feature a variety of arrangements for synthetic jet modules. This is illustrated by
The synthetic jet ejectors 3309 in this embodiment are placed on the sides of the housing 3357 and preferably parallel to the sides thereof. This arrangement not only allows the synthetic jet ejectors to be positioned so as to dissipate heat from the heat sink, but also allows the length of the optical element to be significantly longer than would be the case if the synthetic jet ejectors 3309 were centrally disposed within the housing 3357, thus improving light output distribution. It also leaves space available for electronics and attachment structures in the upper area of the housing 3357.
In operation, heat flows from the base of the heat sink 3359 (where the LED 3359 is mounted) to the heat fins 3327, where the turbulent air flow created by the synthetic jets 3317 emitted by the synthetic jet ejectors 3309 reject the heat to the environment.
Synthetic jet ejectors may be utilized in the embodiments described herein to induce air flow within an otherwise externally sealed chamber. This principle is demonstrated in
In some embodiments, a second fluidic flow may occur at apertures or nozzles 3441. In these embodiments, the second fluidic flow may be utilized, for example, to disperse the heated fluid generated by the first fluidic flow to the ambient environment, or to cool or thermally manage another heat source or device.
The above description of the present invention is illustrative, and is not intended to be limiting. It will thus be appreciated that various additions, substitutions and modifications may be made to the above described embodiments without departing from the scope of the present invention. Accordingly, the scope of the present invention should be construed in reference to the appended claims.
The present application is a continuation of U.S. Ser. No. 13/470,523, entitled “THERMAL MANAGEMENT OF LED-BASED ILLUMINATION DEVICES WITH SYNTHETIC JET EJECTORS” (Mahalingam et al.), filed Oct. 14, 2012, now pending, and which is incorporated herein by reference in its entirety, which is a continuation-in-part application of U.S. Ser. No. 12/902,295, entitled “THERMAL MANAGEMENT OF LED-BASED ILLUMINATION DEVICES WITH SYNTHETIC JET EJECTORS” (Mahalingam et al.), filed Oct. 12, 2010, now pending, and which is incorporated herein by reference in its entirety, and which is a continuation-in-part of U.S. Ser. No. 12/503,181, now abandoned, entitled “THERMAL MANAGEMENT OF LED-BASED ILLUMINATION DEVICES WITH SYNTHETIC JET EJECTORS” (Heffington et al.), filed on Jul. 15, 2009, and which is incorporated herein by reference in its entirety, and which claims priority to U.S. Ser. No. 61/134,984, entitled “THERMAL MANAGEMENT OF LED-BASED ILLUMINATION DEVICES WITH SYNTHETIC JET EJECTORS” (Heffington et al.), filed on Jul. 15, 2008, and which is incorporated herein by reference in its entirety. This application also claims priority to U.S. Ser. No. 61/486,838, entitled “COOLING CONCEPTS” (Noska et al.), filed on May 17, 2011, and which is incorporated herein by reference in its entirety. This application also claims priority to U.S. Ser. No. 12/503,832, issued Oct. 30, 2012 as U.S. Pat. No. 8,299,691, entitled “Advanced Synjet Cooler Design for LED Light Modules” (Grimm), filed on Jul. 15, 2009, and which is incorporated herein by reference in its entirety, and which claims priority to U.S. Ser. No. 61/134,966, entitled “Advanced Synjet Cooler Design for LED Light Modules” (Grimm), filed on Jul. 15, 2008, and which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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61134984 | Jul 2008 | US |
Number | Date | Country | |
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Parent | 13470523 | May 2012 | US |
Child | 13969976 | US |
Number | Date | Country | |
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Parent | 12902295 | Oct 2010 | US |
Child | 13470523 | US | |
Parent | 12503181 | Jul 2009 | US |
Child | 12902295 | US |