System and method for mounting synthetic jets

Abstract

A system and method for the packaging of a synthetic jet actuator is disclosed. A synthetic jet actuator is provided that includes a first plate, a second plate spaced apart from the first plate and arranged parallelly thereto, and a housing positioned about the first and second plates and defining a chamber. The housing includes at least one orifice therein such that the chamber is in fluid communication with an external environment. The synthetic jet actuator also includes a mounting mechanism configured to mount the first and second plates within the housing in a suspended arrangement and an actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof, thereby changing a volume within the chamber so that a series of fluid vortices are generated and projected to the external environment out from the at least one orifice of the housing.

Claims

1. A synthetic jet actuator comprising: a first plate and a second plate spaced apart from one another; a housing positioned about the first and second plates and defining a chamber, the housing having at least one orifice formed in the housing such that the chamber is in fluid communication with an external environment; an actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof so that fluid is projected out of the at least one orifice of the housing; and a mounting mechanism to mount the first and second plates within the housing, the mounting mechanism comprising: a plurality of female connectors on opposing end surfaces of each of the first and second plates; and a plurality of male connectors extending inward from the housing and configured to engage the female connectors.

2. The synthetic jet actuator of claim 1 wherein the plurality of male connectors comprise point-contact holders.

3. The synthetic jet actuator of claim 1 wherein the male connectors are secured in the female connectors via an adhesive.

4. The synthetic jet actuator of claim 1 wherein the first and second plates are spaced apart from the housing such that the first and second plates are free of contact from the housing.

5. The synthetic jet actuator of claim 1 wherein the actuator element comprises a pair of piezoelectric elements, and wherein each piezoelectric element is attached to a respective one of the first and second plates to selectively cause deflection thereof.

6. The synthetic jet actuator of claim 1 wherein the first and second plates are free of contact from the housing during deflection of the plates induced by the actuator element.

7. A synthetic jet actuator comprising: a housing defining a chamber, the housing having an orifice formed therein such that the chamber is in fluid communication with an external environment; a first plate and a second plate spaced apart from one another and positioned within the housing; an actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof so that fluid is projected out of the at least one orifice of the housing; and a mounting mechanism to mount the first and second plates within the housing, the mounting mechanism providing an interference fit arrangement between the first plate and the housing, and an interference fit arrangement between the second plate and the housing; wherein the mounting mechanism comprises a plurality of point-contact holders coupled to the housing and extending inwardly therefrom, wherein the plurality of point-contact holders form an interference fit with respective end surfaces of the first and second plates.

8. The synthetic jet actuator of claim 7 wherein the point-contact holders are chevron-shaped.

9. The synthetic jet actuator of claim 7 wherein the first and second plates are spaced apart from the housing in a suspended arrangement such that no contact is made between the first and second plates and the housing.

10. The synthetic jet actuator of claim 7 wherein the actuator element comprises a pair of piezoelectric elements, and wherein each piezoelectric element is attached to a respective plate of the first and second plates to selectively cause deflection thereof.

11. The synthetic jet actuator of claim 7 wherein the first and second plates are free of contact from the housing during deflection of the plates induced by the actuator element.

12. A synthetic jet actuator comprising: a housing defining a chamber, the housing having at least one orifice formed therein; at least one plate positioned within the chamber; an actuator element coupled to the at least one plate to selectively cause deflection thereof; and a mounting mechanism to mount the at least one plate within the housing, the mounting mechanism providing an interference fit arrangement between the at least one plate and the housing; wherein the mounting mechanism comprises a plurality of point-contact holders affixed to or formed integrally with the housing, and wherein the plurality of point-contact holders extend inwardly from the housing to form an interference fit with respective end surfaces of the at least one plate.

13. The synthetic jet actuator of claim 12 wherein the point-contact holders are V-shaped.

14. The synthetic jet actuator of claim 12 wherein the at least one plate is spaced apart from the housing in a suspended arrangement such that no contact is made between the at least one plate and the housing.

15. The synthetic jet actuator of claim 12 wherein the actuator element comprises a piezoelectric element.

16. The synthetic jet actuator of claim 12 wherein the at least one plate comprises a plurality of plates.

17. The synthetic jet actuator of claim 16 wherein the actuator element comprises a plurality of piezoelectric elements, and wherein each piezoelectric element is attached to a respective plate of the plurality of plates to selectively cause deflection thereof.

18. The synthetic jet actuator of claim 12 wherein no contact is made between the at least one plate and the housing during deflection of the plate induced by the actuator element.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The drawings illustrate embodiments presently contemplated for carrying out the invention.

(2) In the drawings:

(3) FIG. 1 is a cross-section of a prior art zero net mass flux synthetic jet actuator with a control system.

(4) FIG. 2 is a cross-section of the synthetic jet actuator of FIG. 1 depicting the jet as the control system causes the diaphragm to travel inward, toward the orifice.

(5) FIG. 3 is a cross-section of the synthetic jet actuator of FIG. 1 depicting the jet as the control system causes the diaphragm to travel outward, away from the orifice.

(6) FIG. 4 is a schematic cross-sectional side view of a synthetic jet actuator according to an embodiment of the invention.

(7) FIG. 5 is a schematic cross-sectional side view of a synthetic jet actuator according to another embodiment of the invention.

(8) FIG. 6 is an exploded perspective view of a synthetic jet actuator according to another embodiment of the invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(9) The present invention provides for a system and method of providing a packaged synthetic jet actuator. The packaged synthetic jet actuator includes an outer housing that surrounds synthetic jet plates and actuator elements, which are mounted to the housing in a suspended arrangement.

(10) Referring to FIGS. 1-3, a synthetic jet actuator 10 as known in the art, and the operation thereof, is shown for purposes of describing the general operation of a synthetic jet actuator. The synthetic jet actuator 10 includes a housing 11 defining and enclosing an internal chamber 14. The housing 11 and chamber 14 can take virtually any geometric configuration, but for purposes of discussion and understanding, the housing 11 is shown in cross-section in FIG. 1 to have a rigid side wall 12, a rigid front wall 13, and a rear diaphragm 18 that is flexible to an extent to permit movement of the diaphragm 18 inwardly and outwardly relative to the chamber 14. The front wall 13 has an orifice 16 of any geometric shape. The orifice diametrically opposes the rear diaphragm 18 and connects the internal chamber 14 to an external environment having ambient fluid 39.

(11) The flexible diaphragm 18 may be controlled to move by any suitable control system 24. For example, the diaphragm 18 may 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 18 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 24 can cause the diaphragm 18 to move periodically, or modulate in time-harmonic motion, and force fluid in and out of the orifice 16. Alternatively, a piezoelectric actuator could be attached to the diaphragm 18. The control system would, in that case, cause the piezoelectric actuator to vibrate and thereby move the diaphragm 18 in time-harmonic motion.

(12) The operation of the synthetic jet actuator 10 is described with reference to FIGS. 2 and 3. FIG. 2 depicts the synthetic jet actuator 10 as the diaphragm 18 is controlled to move inward into the chamber 14, as depicted by arrow 26. The chamber 14 has its volume decreased and fluid is ejected through the orifice 16. As the fluid exits the chamber 14 through the orifice 16, the flow separates at sharp orifice edges 30 and creates vortex sheets 32 which roll into vortices 34 and begin to move away from the orifice edges 30 in the direction indicated by arrow 36.

(13) FIG. 3 depicts the synthetic jet actuator 10 as the diaphragm 18 is controlled to move outward with respect to the chamber 14, as depicted by arrow 38. The chamber 14 has its volume increased and ambient fluid 39 rushes into the chamber 14 as depicted by the set of arrows 40. The diaphragm 18 is controlled by the control system 24 so that when the diaphragm 18 moves away from the chamber 14, the vortices 34 are already removed from the orifice edges 30 and thus are not affected by the ambient fluid 39 being drawn into the chamber 14. Meanwhile, a jet of ambient fluid 39 is synthesized by the vortices 34 creating strong entrainment of ambient fluid drawn from large distances away from the orifice 16.

(14) It is recognized that synthetic jet actuators, such as the actuator set forth above, can be subjected to a range of environment conditions during use. In some instances, it is desired that the synthetic jet actuator be protected from the surrounding environment, so as to be protected from temperature extremes, moisture, and physical forces/impacts from surrounding components. As such, it is desired that the synthetic jet actuator be packaged in a housing-type structure, such as a cover positioned over piezoelectric elements in the synthetic jet actuator.

(15) Referring now to FIG. 4, according to an embodiment of the invention a synthetic jet actuator 50 is shown. The synthetic jet actuator includes a pair of synthetic jet plates 52, 54, shown in FIG. 4 as a first plate 52 and an opposing second plate 54 arranged parallel thereto. Attached to at least one of the first and second plates 52, 54, or to both of the first and second plates as shown in FIG. 4, are actuator elements 56, 58 configured to cause displacement of the plates. In an exemplary embodiment, actuator elements 56, 58 comprise piezoelectric elements (e.g., piezoelectric disks) that are configured to periodically receive an electric charge from a controller/power source (not shown), and undergo mechanical stress and/or strain responsive to the charge. The stress/strain of piezoelectric elements 56, 58 causes deflection of first and second plates 52, 54 such that, for example, a time-harmonic motion or vibration of the plates is achieved. It is recognized that the piezoelectric elements 56, 58 coupled to the first and second plates 52, 54, respectively, can be selectively controlled to cause vibration of one or both of the plates so as to control the volume and velocity of a synthetic jet stream 60 expelled from the synthetic jet actuator 50.

(16) The first and second plates 52, 54 and actuator elements 56, 58 are positioned within an outer housing 62 having a plurality of walls 64 that surround the first and second plates 52, 54 and define a chamber or volume 66 within the synthetic jet actuator 50. The outer housing 62 includes therein one or more orifices 68 to place the chamber 66 within outer housing 62 in fluid communication with a surrounding, external environment 70. As shown in FIG. 4, a pair of orifices 68 is formed in outer housing 62 to allow for the drawing in and exhaustion of an ambient fluid into and out of the synthetic jet actuator 50. That is, as set forth above, the piezoelectric elements 56, 58 coupled to the first and second plates 52, 54 are selectively controlled to cause vibration of one or both of the plates so as to control the volume and velocity of synthetic jet stream 60 expelled from one or both of the orifices 68.

(17) As shown in FIG. 4, the synthetic jet actuator 50 is secured within the housing by way of a mounting device 72. In the embodiment, mounting device 72 comprises a plurality of point-contact mounts 74 affixed to an internal surface 76 of the housing 62 and extending inwardly therefrom. The point-contact mounts 74 are configured to attach to end surfaces 78 of the first and second plates 52, 54 so as to secure the plates within outer housing 62 and prevent movement. That is, in one embodiment, point-contact mounts 74 are positioned so as to attach to the short end surfaces 78 of the rectangular shaped first and second plates 52, 54. In an exemplary configuration, point-contact holders 74 are configured as V-shaped holders (i.e., chevron-type holders). A pair of V-shaped holders 74 that are linearly aligned in a lengthwise direction 80 of the outer housing 62 are used to secure each of the first and second plates 52, 54. As shown in FIG. 4, a pair of linearly aligned V-shape holders 74 is positioned on each side of the orifice(s) 68 in the outer housing 62 such that first and second plates 52, 54 can be mounted on opposite sides of the orifice(s) 68. To provide for a secure engagement between the V-shaped holders 74 and the first and second plates 52, 54, short end surfaces 78 of each of the first and second plates 52, 54 can include therein a V-shaped notch 82 that is configured to interfit with the V-shaped holders 74. An adhesive 83 can be added between the notch 82 and V-shaped holder 74 to provide for a more secure bonding. Additionally, the adhesive 83 could have a coefficient of thermal expansion (CTE) between that of the material forming the V-shaped holders 74 and the material forming plates 52, 54. Alternative to having a notch 82 formed in plates 52, 54, it is recognized that an interference fit could be formed between V-shaped holders 74 and end surfaces 78 of the plates 52, 54 to secure the plates within housing 62.

(18) Beneficially, V-shaped holders 74 secure first and second plates 52, 54 within outer housing 62 in a manner that allows for unimpeded performance of the synthetic jet actuator 50. That is, as the pair of V-shaped holders 74 used to secure first and second plates 52, 54 are attached to/interfit with short end surfaces 78 of the plates, the V-shaped holders 74 allow for interference-free deflection of the first and second plates 52, 54. Additionally, as the V-shaped holders 74 hold the first and second plates 52, 54 in a suspended arrangement in which the plates are spaced apart from the housing 62, no contact is made between the first and second plates 52, 54 and the housing 62 during deflection of the plates induced by actuator elements 56, 58. This lack of contact between plates 52, 54 and housing 62 allows the plates to vibrate at their natural frequency and reduce noise generated by the synthetic jet actuator 50.

(19) Referring now to FIG. 5, a synthetic jet actuator 84 is shown according to another embodiment of the invention. The synthetic jet actuator 84 includes a first synthetic jet plate 52 and an opposing second synthetic jet plate 54 arranged parallel thereto. Attached to at least one of the first and second plates 52, 54, or to both of the first and second plates as shown in FIG. 5, are actuator elements 56, 58 configured to cause displacement of the plates. In an exemplary embodiment, actuator elements 56, 58 comprise piezoelectric elements (e.g., piezoelectric disks) that are configured to periodically receive an electric charge from a controller/power source (not shown), and undergo mechanical stress and/or strain responsive to the charge. The stress/strain of piezoelectric elements 56, 58 causes deflection of first and second plates 52, 54 such that, for example, a time-harmonic motion or vibration of the plates is achieved. It is recognized that the piezoelectric elements 56, 58 coupled to the first and second plates 52, 54, respectively, can be selectively controlled to cause vibration of one or both of the plates so as to control the volume and velocity of a synthetic jet stream 60 expelled from the synthetic jet actuator 84.

(20) The first and second plates 52, 54 and actuator elements 56, 58 are positioned within an outer housing 62 having a plurality of walls 64 that surround the first and second plates 52, 54 and define a chamber or volume 66 within the synthetic jet actuator 84. The outer housing 62 includes therein one or more orifices 68 to place the chamber 66 within outer housing 62 in fluid communication with a surrounding, external environment 70. As shown in FIG. 5, a pair of orifices 68 is formed in outer housing 62 to allow for the drawing in and exhaustion of an ambient fluid into and out of the synthetic jet actuator 84. That is, as set forth above, the piezoelectric elements 56, 58 coupled to the first and second plates 52, 54 are selectively controlled to cause vibration of one or both of the plates so as to control the volume and velocity of synthetic jet stream 60 expelled from one or both of the orifices 68.

(21) The synthetic jet actuator 84 is secured within the housing 62 by way of a mounting device 86. In the embodiment of the invention shown in FIG. 5, mounting device 86 comprises an adhesive 88 applied to opposing internal surfaces 76 of the outer housing 62. Outward facing surfaces 90 (i.e., back surfaces) of the first and second plates 52, 54 are pressed onto the adhesive 88 such that the plates are secured within outer housing 62 and prevented from moving. As shown in FIG. 5, adhesive 88 acts to space first and second plates 52, 54 apart from the housing 62 in a suspended arrangement, such that no contact is made between the first and second plates 52, 54 and the housing 62 during deflection of the plates induced by actuator elements 56, 58, thus allows the plates to vibrate at their natural frequency and reduce noise generated by the synthetic jet actuator 84. Additionally, adhesive 88 is applied such that it covers only a portion of the back surface 90 of first and second plates 52, 54 and is formed as a flexible adhesive so as to allow for interference-free deflection of the first and second plates 52, 54. While shown as a continuous section of adhesive 88 in FIG. 5, it is also recognized that the adhesive could be in the form of a post or posts (i.e. discrete attach points vs. a continuous line of adhesive) or other suitable configurations. The exact configuration/shape of the applied adhesive 88 could be determined based on materials, frequency of operation of the synthetic jet actuator, manufacturability, and other factors.

(22) Another embodiment of the invention, is shown in FIG. 6 and shows a synthetic jet actuator 92 having first and second synthetic jet plate 52, 54 spaced apart by a flexible support structure 93 (i.e., wall or posts). Attached to at least one of the first and second plates 52, 54, or to both of the first and second plates as shown in FIG. 6, are actuator elements 56, 58 configured to cause displacement of the plates. It is recognized that the actuator elements 56, 58 coupled to the first and second plates 52, 54, respectively, can be selectively controlled to cause vibration of one or both of the plates so as to control the volume and velocity of a synthetic jet stream 60 expelled from the synthetic jet actuator 92.

(23) The first and second plates 52, 54 and actuator elements 56, 58 are positioned within an outer housing 94 that surrounds the first and second plates 52, 54 and define a chamber or volume 66 within the synthetic jet actuator 92. The outer housing 94 includes a pair of V-shaped walls 96 on opposing sides thereof and one or more orifices 68 to place the chamber 66 within outer housing 94 in fluid communication with a surrounding, external environment 70. The synthetic jet actuator 92 is secured within the housing 94 by way of cradles 98 that form a mounting device. Cradles 98 are mounted to an inner surface 100 of the V-shaped walls 96 such that they contact the first and second plates 52, 54. The V-shaped walls 96 allow for the structure formed by first and second plates 52, 54 and support structure 93 to be wedged between the V-shaped walls 96 and supported thereby in a point-contact fashion. This point-contact between plates 52, 54 and housing 94 allows the plates to vibrate at their natural frequency and reduce noise generated by the synthetic jet actuator 92.

(24) As set forth above with respect to FIGS. 4-6, a minimal-contact mounting arrangement of the first and second synthetic jet plates 52, 54 within an outer housing 62, 94 is provided. The housing 62, 94 of synthetic jet actuator 50, 84 provides protection from the surrounding environment 70, such that synthetic jet actuator 50, 84, 92 is protected from temperature extremes, moisture, and physical forces/impact from surrounding components. Additionally, the embodiments set forth above provide for a mounting structure of synthetic jet plates 52, 54 within outer housing 62, 94 that has a minimal impact on performance of the synthetic jet actuator 50, 84, as the suspension mounting arrangement prevents outer housing 62, 94 from interfering with the deflection and vibration of the plates 52, 54 of the synthetic jet actuator.

(25) While the synthetic jet actuators of FIGS. 4-6 are shown/described as having multiple orifices therein forming separate intake and exhaust orifices, it is also envisioned that embodiments of the invention could be used with single orifice synthetic jet actuators. Additionally, while the synthetic jet actuators of FIGS. 4-6 are shown/described as having an actuator element included on each of first and second plates, it is also envisioned that embodiments of the invention could include only a single actuator element positioned on one of the plates. Furthermore, it is also envisioned that the synthetic jet actuators set forth above could be circular/cylindrical in shape and that the synthetic jet plates and actuator elements therein be circular in shape and mount to the housing in one of the manners set forth above, rather than in a rectangular configuration.

(26) 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.

(27) Therefore, according to one embodiment of the invention, a synthetic jet actuator includes a first plate, a second plate spaced apart from the first plate and arranged parallelly thereto, and a housing positioned about the first and second plates and defining a chamber, the housing having at least one orifice therein such that the chamber is in fluid communication with an external environment. The synthetic jet actuator also includes a mounting mechanism configured to mount the first and second plates within the housing in a suspended arrangement and an actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof, thereby changing a volume within the chamber so that a series of fluid vortices are generated and projected to the external environment out from the at least one orifice of the housing.

(28) According to another embodiment of the invention, a method of manufacturing a synthetic jet actuator includes providing an outer housing having a plurality of walls defining a chamber and having an orifice formed in at least one of the plurality of walls and positioning a pair of synthetic jet plates within the outer housing and on opposite ends thereof The method also includes attaching the pair of synthetic jet plates to the outer housing such that the pair of synthetic jet plates are spaced apart from each of the plurality of walls.

(29) According to yet another embodiment of the invention, a synthetic jet actuator includes an outer housing defining a chamber and having at least one opening formed therein and a pair of synthetic jet plates positioned within the outer housing and on opposing sides thereof The synthetic jet actuator also includes a mounting device configured to affix the pair of synthetic jet plates to the outer housing such that the pair of synthetic jet plates are inwardly spaced from the outer housing so as not to be in contact therewith and at least one actuator element coupled to the pair of synthetic jet plates to selectively change a volume within the chamber so that a series of fluid vortices are generated and projected to an external environment out from the at least one opening in the outer housing.