Category Archives: Synthetic Jet

Technology Review: Spray Cooling

Qpedia continues its review of technologies developed for electronics cooling applications. We are presenting selected patents that were awarded to developers around the world to address cooling challenges. After reading the series, you will be more aware of both the historic developments and the latest breakthroughs in both product design and applications.

Spray Cooling
This Technology Review will focus on recent developments in spray cooling technology. (Wiklmedia Commons)

We are specifically focusing on patented technologies to show the breadth of development in thermal management product sectors. Please note that there are many patents within these areas. Limited by article space, we are presenting a small number to offer a representation of the entire field. You are encouraged to do your own patent investigation.

Further, if you have been awarded a patent and would like to have it included in these reviews, please send us your patent number or patent application.

In this issue our spotlight is on spray cooling for electronics thermal management.

There are several US patents in this area of technology, and those presented here are among the more recent. These patents show some of the salient features that are the focus of different inventors.

Full Coverage Spray and Drainage System and Method for Orientation-Independent Removal of High Heat Flux

 US 8550372 B2 – Timothy A. Shedd and Adam G. Pautsch

A cooling system and method that significantly improves spray evaporative cooling by using arrays of slot or plane sprays to create coverage of the entire heated surface to be cooled without allowing interaction between plumes that are spraying from the nozzles. The sprays are directed at an angle to the surface to take advantage of the high droplet momentum possessed by the spray to direct a flow of coolant fluid across the surface toward desired draining points, thereby enabling drainage regardless of the orientation of the unit.

The present invention provides a spray cooling system and method that significantly improves spray evaporative cooling by creating a directed momentum flow of cooling fluid across a surface to be cooled. In accordance with the present invention, a spray of cooling fluid is directed directly onto the surface of a work piece to be cooled at an angle with respect to the work piece surface so as to create a flow of cooling fluid in a substantially single direction along the work piece surface. The spray of cooling fluid preferably may be delivered via a plurality of generally fan shaped sprays. The sprays are positioned and aligned to create cooling fluid coverage of the entire heated surface to be cooled without allowing interaction between the spray plumes in a manner that may cause areas of cooling fluid stagnation on the surface.

A full coverage spray and drainage system in accordance with the present invention may be implemented in an otherwise conventional spray cooling system including a reservoir of an appropriate cooling fluid (e.g., Fluorinert-72 for the cooling of electronic circuitry, preferably saturated with a non-condensable inert gas, such as nitrogen), a pump for delivering the cooling fluid under pressure from the reservoir to a spray chamber to be sprayed therein from nozzles onto the work piece to be cooled, and appropriate filtering, metering, and control systems. Cooling fluid is returned from the spray chamber to the coolant reservoir via a drainage point or points in the spray chamber.

In accordance with the present invention, the drainage point or points in the spray chamber may be positioned with respect to the coolant spray such that the flow of cooling fluid directed in a substantially single direction along the work piece surface also is directed toward the drainage point or points. Thus, the cooling fluid momentum directs the fluid toward the drainage point, thereby assuring proper drainage of the cooling fluid despite changes in the orientation of the cooling system.

Directly Injected Forced Convection Cooling for Electronics

US 8824146 B2 – Gerrit Johannes Hendrikus Maria Brok, Wessel Willems Wits, Jan Hendrik Mannak and Rob Legtenberg

Electronic circuitry includes a circuit board and at least one component mounted on the circuit board, with the at least one component generating heat while in use. The circuit board includes one or more apertures aligned with one or more respective components, and the electronic circuitry is configured to provide, while in use, a path for coolant fluid to flow through each aperture and past the respective component.

By providing at least one aperture aligned with a component that generates heat in use, improved cooling of the electronic circuitry may be provided, as cooling effects can more efficiently be targeted at those parts of the circuitry that generate or dissipate heat.

Each aperture may be, but is not necessarily positioned at that point or within that region of the circuit board that is a minimum distance from the component or a respective one of the components.

The central axis of each aperture may be, but is not necessarily, perpendicular to the plane of the circuit board and at least one component. Preferably each aperture is arranged such that a straight line extending out of the aperture along the central axis of the aperture would pass through the component with which the aperture is aligned. Preferably each aperture is arranged such that, in use, coolant fluid exits the aperture towards the component with which the aperture is aligned.

The coolant fluid may be liquid or gas. The coolant fluid may be water. The coolant fluid may comprise a dielectric fluid, for example poly-alpha-olefin (PAO), or an inert gas, for instance nitrogen. Preferably the coolant fluid is air. In some circumstances, the coolant fluid may be supplied from a pressurized source, for instance a pressurized gas cylinder.

The position of each aperture may be such that, in use, coolant fluid passing through the aperture approaches the surface of the component with which the aperture is aligned from a perpendicular direction.

Thereby a jet impingement effect may be provided such that, preferably, the coolant fluid breaks through a respective thermal boundary layer next to the or each at least one heat generating component. Such thermal boundary layers are stable layers of air or other fluid which may build up next to the or each component and which exhibit a temperature gradient away from the component. The presence of such thermal boundary layers can reduce convective cooling effects.

Narrow Gap Spray Cooling in a Globally Cooled Enclosure

US 8174828 B2 – Charles L. Tilton, Donald E. Tilton, Randall T. Palmer, William J. Beasley, Douglas W. Miller and Norman O. Alder

Electronic circuit boards are arranged as respective parallel pairs defining a narrow gap there between. One or more such pairs of boards are supported within a hermitically sealable housing and cooled by way of spraying an atomized liquid coolant from a plurality of nozzles into each narrow gap. Transfer of heat from the circuit boards results in vaporization of at least some of the atomized liquid within the narrow gap. The housing further serves to guide a circulation of vapors out of each narrow gap, back toward the nozzles, and back into each narrow gap. A heat exchanger exhausts heat from the housing and overall system, wherein vapor is condensed back to liquid phase during contact and heat transfer therewith. Condensed liquid is collected and re-pressurized for delivery back to the nozzles such that a sustained cooling operation is performed.

One embodiment provides for a system, including a first entity and a second entity that are respectively disposed such that they define a narrow gap between them. The system also includes at least one nozzle, wherein the nozzle is configured to spray an atomized liquid so that a flow of the atomized liquid and a vapor is induced through the narrow gap. The system also includes a heat exchanger that is configured to condense some of the vapor to liquid, the condensed vapor defining a condensate. The system further includes a housing configured to guide a circulation of at least some of the vapor, which is flowing out of the narrow gap, away from the heat exchanger and into proximity with the at least one nozzle.

Another embodiment provides for a system, the system comprising a housing configured to selectively open-ably enclose a plurality of electronic circuit boards. The system further includes a plurality of electronic circuit boards supported in the housing, wherein at least some of the electronic circuit boards are arranged to define respective pairs of boards. At least one pair of boards defines a narrow gap there between. The system also includes at least one nozzle associated with each narrow gap, each nozzle being configured to spray an atomized liquid into the narrow gap defined by the associated pair of boards. The housing is also configured to guide a circulation of a vapor exiting each narrow gap into proximity with the at least one nozzle associated with the at least one narrow gap.

Still another embodiment provides an apparatus. The apparatus includes a nozzle configured to spray an atomized liquid in a generally conical distribution pattern. The apparatus further includes a re-shaper that is configured to reform the spray of atomized liquid into a generally planar distribution pattern.

Enhanced Spray Cooling Technique for Wedge Cooling

US 8729752 B2 – Balwinder Singh Birdi, Simon Waddell and William Scherzinger  

The present invention relates to apparatus and methods for heat removal and, more particularly, apparatus and methods for spray cooling a wedge of a generator rotor.

In generators, electromagnetic losses occur in the magnetic iron and the copper. These losses result in production of heat which must be removed to maintain overall temperature below that allowable for the copper coating and the insulation used in the construction of the generators. The rotor core, which is made of magnetic iron, can be conduction cooled by flowing fluid through the rotor shaft. However, the removal of heat from copper is better managed if oil is passed through the hollow wedges. Due to lower thermal resistance, the flow of fluid in the vicinity of copper is much more effective in removing heat from the copper and in keeping the overall temperature below the allowable limit. This is done with conduction mode of heat removal.

Since the heat transfer coefficient (HTC) depends upon the velocity of the fluid, the removal of heat is not very efficient, and a very high flow is needed to create a reasonable HTC for conduction cooling. Further, because the rotor is a rotating component, having a large amount of fluid at a radius away from the rotor shaft is not desirable, especially for high powered larger diameter and high-speed machines.

In one aspect of the present invention, a spray cooling manifold comprises a manifold ferrule adapted to circumscribe a shaft of a rotating machine; a manifold pipe having a bend of about 90 degrees having a first end attached to the manifold ferrule and a second, opposite end; a cooling fluid channel running from an inside surface of the manifold ferrule to the second, opposite end of the manifold pipe; and a pipe extending from the second, opposite end of the manifold pipe, the pipe adapted to extend into a wedge of the rotating machine, the pipe having a plurality of holes formed there along.

In another aspect of the present invention, a rotating machine rotor comprises a shaft; a plurality of coils disposed on the shaft; a plurality of wedges disposed between the coils; bands securing the wedges on the rotor; and a manifold comprising a manifold ferrule adapted to circumscribe the shaft; a plurality of manifold pipes, each having a bend of about 90 degrees, each having a first end attached to the manifold ferrule and a second, opposite end attached to a wedge pipe extending into the wedges; a cooling fluid channel running from an inside surface of the manifold ferrule to the wedge pipe; and a plurality of holes disposed along the wedge pipe.


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How to Use Synthetic Jets for Local Thermal Management

As todays electronics generate more heat inside ever smaller spaces, engineers are challenged to find new ways to effectively cool the components [1]. There have been continued advances in high heat flux technologies [2], but commercial, consumer-oriented systems continue to focus on air cooling for its reliability, acoustics, cost and portability [3]. To support the increasing power dissipation of components and systems, designers must evaluate different cooling solutions within the dimensional constraints of the system. Available cooling solutions have their own advantages and disadvantages, such as reliability and noise. In this article, we discuss synthetic jets, an air cooling technology that can provide a high local heat transfer coefficient at a low flow rate with low acoustics and high reliability [1].

Synthetic Jets

Synthetic jets are formed by the periodic suction and ejection of fluid out of an orifice bounding a cavity by the periodic motion of a diaphragm built into one of the walls of the cavity [1], as shown in Figure 1. The operation of a synthetic jet can be divided into two phases. First is the ejection phase, which is shown in Figure 1 (a) to (c). Second is the suction phase, which is shown in Figure 1 (d) and (e). A coherent vortex is created and convected downstream from the jet exit in the ejection phases. The vortex is created by the movement of the diaphragm, which forces air to exit through an orifice. The suction phase occurs once the vortex flow has propagated well downstream. The diaphragm moves back, thereby entraining the ambient fluid from the vicinity of the orifice into the diaphragm volume.

When the bulk of the high speed air has moved away from the orifice, avoiding re-entrainment, ambient air from around the orifice is drawn into the orifice [1]. Thus, a synthetic jet is a zero-mass-flux jet comprised entirely of the ambient fluid. It can be conveniently integrated with the surfaces that require cooling without the need for complex plumbing. The periodic motion of the synthetic jet diaphragm can be achieved using several techniques, including piezoelectric, electromagnetic, electrostatic and combustion driven pistons [1]. The most commonly used actuators are piezoelectric and electromagnetic. For a given form factor, piezoelectric diaphragms hold an advantage in weight and power consumption, while electromagnetic actuators have better noise and reliability performance [1].

particle image velocimetry data formation of a synthetic jet

Figure 1. Particle Image Velocimetry Data Formation of a Synthetic Jet Showing the Ejection Phase (a) to (c); and Entrainment (d) to (e) [1].

The principle of jet ejectors or jet pumps [4] has been known for several decades. A jet ejector consists of a primary high momentum jet that drives a secondary airflow through a channel as shown in Figure 2 (a). The low pressure created by a primary jet discharging into the channel results in entrainment of quiescent ambient flow, thus creating an increase in overall flow rate at the channel exit. This is also shown in Figure 2 (b) where the computed induced flow is plotted as a function of channel width in a channel flow driven by a high momentum jet. The overall flow rate can be an order of magnitude higher than the jet flow itself, depending on the operating conditions [1].

 

Principle of Operation of a Jet Ejector

Figure 2. Principle of Operation of a Jet Ejector (a) and Calculation of Ratio of Induced Secondary Channel Flow to Jet Flow in a Jet Ejector (b) [1].

In conventional jet ejectors, the primary jet is created using a pressure source ducted into the entry of a channel [1]. The use of synthetic jets as the primary jet is an attractive option since the only input to the primary jet is electrical, requiring no plumbing or pressure supplies. During the ejection phase of the synthetic jet, the jet ejector phenomenon is similar to steady jet ejectors, wherein a primary high momentum jet creates a low pressure in a channel resulting in the entrainment of fluid from the ambient [1]. During the suction phase, the low pressure in the jet cavity results in additional flow entrainment, which is forced out during the subsequent blowing stroke.

Application to Electronics Thermal Management

Synthetic jets have two main areas of application in the thermal management of electronics. The first is when a heat sink is designed with integrated synthetic jets. The second is when synthetic jet is used in conjunction with a fan.

When a heat sink is integrated with synthetic jets, it offers a number of advantages over heat sinks designed for use either with fans or without fans. Natural convection sinks are normally much larger than synthetic jet heat sinks that provide the same thermal performance [5]. Table 1 shows published data  comparing LED cooling solutions for natural convection and for synthetic jet heat sinks. Along with providing a smaller size solution, the synthetic jet is an active solution which gives more design freedom to the final product. A natural convection heat sinks thermal performance is directly influenced by the heat sink shape and orientation. As an active solution, the synthetic jet enables an orientation independent design [5]. Some synthetic jet integrated solutions are shown in Figure 3.

Comparison of a Synthetic Jet Cooled Heat Sink and Natural Convection Heat Sinks

Table 1. Comparison of a Synthetic Jet Cooled Heat Sink and Natural Convection Heat Sinks. Data Adapted from [5].

Note that Cheung, et al. used a straight fin passive heat sink. To reduce the thermal resistance, they further increased the height of an already tall heat sink. This is not a very effective method because the air is already warm at the original heat sink height. Through proper design and material property choices, natural convection heat sinks can be excellent alternatives to synthetic jet heat sinks, although they will be limited in form, orientation and size compared to active heat sinks.

Heat Sink Designs with Integrated Synthetic Jets

Figure 3. Heat Sink Designs with Integrated Synthetic Jets. Shown are the SynJet® MR16 (a) [6] and the SynJet® Low Profile Cooler with Heat Sink (b) [7].

Mahalingam et al. have published data for comparing a synthetic jet based PCI-E half-height graphics card cooler and a fan-sink equivalent [1]. They found that the A-weighted sound pressure level (SPL) was significantly lower for the synthetic jet, as shown in Figure 4. Also, for an SPL-A of 40 dBA, the synthetic jet solution had a 12% better thermal performance than the fan-sink. In additional tests conducted at a 2 K/W thermal resistance for both solutions, the power consumption for the synthetic jet solution was 640 mW, while the power consumption for the fan solution was 672 mW.

Plot of the Acoustic Performance of a Synthetic Jet

Figure 4. Plot of the Acoustic Performance of a Synthetic Jet and Fan-Sink Plotted Against the Thermal Resistance [1].

When a synthetic jet is used in conjunction with a fan, it can decrease the thermal resistance and noise, and increase the reliability of fan cooled systems [1]. The synthetic jet achieves this by reducing flow bypass of a heat sink and increasing the local heat transfer coefficient of the heat sinks. Mahalingam et al. [1] have published data on where synthetic jets were applied to a server. They found that augmention resulted in a reduction in the thermal resistance as well as a reduction in the power needed to run the fans. Using the synthetic jets, the fan speed was reduced from 9000 to 5500 RPM and resulted in a reduction in power consumption from 108 to 48 W. This further reduced the cooling required.

Advantages and Disadvantages of Synthetic Jets

The cooling solution design for a product is a combination of various factors. These include mass, volume, thermal resistance, ambient temperature, component temperature, cooling method used, reliability, life time, cost, transport cost and performance of electronics. Most of these factors are dependent on each other; however they all influence the final design of the product.

It has been shown that the synthetic jet cooling method can reduce the heat sink size and therefore the heat sink mass without sacrificing thermal performance. Because a synthetic jet is an active cooling solution, the heat sinks thermal performance is better than similarly sized natural convection heat sinks. This means greater design freedom which is critical for LED consumer products. The industrial (visual) design of a lamp is very important in the buying impulse of a consumer.

A factor that has not been discussed is the reliability of a synthetic jet. Jones [8] has published a white paper for the reliability for the Nuventix SynJet, in which it was compared to data published by leading fan manufacturers. It was found that many vendors fail to specify reliability data for fans at high ambient temperature. For small fans, it was found that the L10 reliability at 60ºC is around 50,000 hours, while for the Nuventix SynJet is at least 300,000 hours at 60ºC.

L10 Reliability to Other Leading Air Movers

Figure 5. Comparison of SynJet L10 Reliability to Other Leading Air Movers [8].

For a comparison of natural convection, fan-based and synthetic jet cooling solutions, Table 2 shows the results based on the noise, reliability, thermal resistance, cost, power consumption and size of the aforementioned cooling solutions. The cooling solutions from Table 2 are compared via an X system, where the higher the count, the better.

Comparison of Natural Convection, Fan and Synthetic Jet Cooling Solutions

Table 2. Comparison of Natural Convection, Fan and Synthetic Jet Cooling Solutions.

Summary

This article has discussed the operational principle of a synthetic jet. The use of synthetic jets offers advantages in thermal performance, orientation, form factor of the final product, size and mass. Power consumption and noise are also small for a synthetic jet. However, the advantages of synthetic jets must be weighed against the unit price of a synthetic jet module.

References

1. Mahalingam, R., Heffington. S., Jones, L. and Williams, R, Synthetic Jets for Forced Air Cooling of Electronics, Electronics Cooling, May 2007

 

2. Lasance, C. and Simons, R., Advances in High-Performance Cooling for Electronics, Electronics Cooling, November 2005.

 

3. Bar-Cohen, A., Computer-Related Thermal Packaging at the Millennial Divide, Electronics Cooling, January 2000.

 

4. Gosline, J. and OBrien, M., The Water Jet Pump, Univ. of California Publ. Engrg., 1934.

 

5. Cheung, C., Noska, B. and van der Heide, K., Comparison of Passive and Active Cooling Effectiveness, LED Professional Review Magazine, Sep-Oct 2009.

 

6. Synjet® MR16 LED Cooler with HS, Nuventix Data Sheet, http://www.nuventix.com/files/uploaded_files/pf_SM16S-CM005-xxx%20MR_16%20%20Rev_2.3.pdf, 2009.

 

7. SynJet® Low Profile Cooler with HS, Nuventix Data Sheet, http://www.nuventix.com/files/uploaded_files/pf_SSCCS-CM005-xxx%20Low%20Profile%20cooler%20Rev2%203%20datasheet.pdf, 2009.

 

8. Jones, L., Nuventix SynJet Ultra-High Reliability Cooling White Paper, http://www.nuventix.com/technology/papers/high-reliability-cooling/, 2009.