The present invention relates in general to thermal management, and in particular to thermal and electrical contact structures and methods for nano-engineered materials.
Electronic devices such as microprocessors generate heat as they operate, and excessive heat can lead to device failure. Heat sinks are frequently employed to transfer heat away from the device into the surrounding environment, thereby maintaining the device temperature within operational limits. A typical heat sink is constructed of copper or another metal with high thermal conductivity and has one flat surface for contacting the heat source (e.g., the top surface of the device package) and an opposing surface that includes fins or similar features to increase the surface area exposed to the environment. A thermally conductive adhesive is often used to bond the heat sink to the device package for improved heat transfer into the heat sink. Heat sinks can be further supplemented with fans that keep air flowing across the exposed surface area while the device is operating.
This conventional thermal management technology, which has been effective for many years, has its limitations. As the number and density of heat-generating elements (e.g., transistors) packed into devices has increased, the problem of heat dissipation has become a critical consideration in device and system design. It would therefore be desirable to provide improved thermal management technologies suitable for use with electronic devices.
The present invention relates in general to thermal management, and in particular to thermal and electrical contact structures and methods for nano-engineered materials. Embodiments of the present invention provide structures and methods for improving the thermal and/or electrical contact between nano-engineered materials and other materials with which the nano-engineered materials are coupled.
According to one aspect of the present invention, a method for enhancing contact between a nanotube and a first material is provided. The method includes providing a nanotube with ends and treating at least one of the ends of the nanotube. In one embodiment, the contact is thermal contact. In another embodiment, the contact is electrical contact. In a particular embodiment, the treating step includes exposing the nanotube to an oxygen plasma and/or energetic oxygen. In a specific embodiment, the treating step includes opening at least one of the ends of the nanotube.
According to another aspect of the present invention, a nano-engineered material includes a base material and a nanostructure coupled to the base material, wherein the nanostructure is treated to enhance thermal contact. The nano-engineered material also includes a contact-enhancing material coupled to the nanostructure. In a particular embodiment, the treatment of the nanostructure includes exposing the nanostructure to an oxygen plasma and/or energetic oxygen. In a specific embodiment, the treatment of the nanostructure includes opening a portion of the nanostructure.
According to yet another aspect of the present invention, a nano-composite material includes a matrix material and a nanostructure incorporated into said matrix material, wherein said nanostructure is treated to enhance thermal contact.
A wide variety of thermal transfer devices may incorporate aspects of the present invention. Examples include heat sinks for electronic, optical or mechanical devices; device packaging; printed circuit boards; and semiconductor device layers.
The following detailed description together with the accompanying drawings will provide a better understanding of the nature and advantages of the present invention.
The present invention relates in general to thermal management, and in particular to thermal and electrical contact structures and methods for nano-engineered materials. Embodiments of the present invention provide structures and methods for improving the thermal and/or electrical contact between nano-engineered materials and other materials with which the nano-engineered materials are coupled.
The term “nanostructure,” or nanoscale structure is used herein to refer to a structure with at least one dimension that is on the order of nanometers (e.g., from about 1 to 100 nm); one or more of the other dimensions may be larger and may be microscopic (from about 10 nm to a few hundred micrometers) or macroscopic (larger than a few hundred micrometers). Specific embodiments use nanotubes (e.g., carbon or boron nitride nanotubes). However, other embodiments can use nanostructures such as nanorods, nanofibers, nanocrystals, fullerenes, and other nanoscale structures such as diamond dust made from crystalline or CVD diamond flecks, as well as chains of nanocrystals or fullerenes.
The term “nano-engineered material” is used herein to refer a material that includes (or possibly consists essentially of) nanostructures. Nano-engineered materials include, for example, mats of nanostructures, groupings of nanostructures deposited on a patterned layer using deposition techniques, and nano-composite materials.
The term “nano-composite material” is used herein to refer to a composite material comprising a base, or matrix, material into which are incorporated nanostructures. In some embodiments, the nanostructures are dispersed into the base material. In other embodiments, the nano-composite material has a layered structure in which some layers are made of a base material while other layers are made entirely or predominantly of nanostructures. Nano-composite materials may incorporate one or more different kinds of nanostructures, with the nanostructures being selected for high thermal conductivity or other desirable thermal properties in some applications. Additional details regarding nano-composite materials are found in the above-referenced co-pending application Ser. No. ______,(Attorney Docket No. 022353-000110US).
For thermal management applications, nanostructures having higher thermal conductivity than the base material are advantageously used to enhance the thermal conductivity of the base material so that the resulting nano-composite material has higher thermal conductivity than the base material. In preferred embodiments, the nanostructures include nanotubes having very high thermal conductivity. Nanotubes are best described as long, thin cylindrically shaped, discrete fibril structures whose diameters are on the order of nanometers. Nanotubes can exhibit lengths up to several hundred microns; thus their aspect ratios can exceed 1000. The aspect ratio can be well controlled using process conditions as is known in the art. The terms “single-wall” or “multi-wall” as used to describe nanotubes refer to nanotube structures having one or more layers of continuously ordered atoms where each layer is substantially concentric with the cylindrical axis of the structure; the nanotubes referred to herein may include single-walled and/or multi-walled nanotubes.
Nanotubes have theoretically and experimentally been shown to have high thermal conductivity along the axis of the nanotube. The thermal conductivity of carbon nanotubes, for example, has been measured at around 3000 W/m*K (theoretical calculations indicating conductivities as high as 6000 W/m*K might be achievable), as compared to conventional thermal management materials such as aluminum (247 W/m*K) or copper (398 W/m*K).
Nanotubes for a nano-composite material may be made of a variety of materials including carbon. In one embodiment, boron nitride (BN) nanotubes are used. The electrical properties of BN nanotubes are particularly well suited to applications where a heat transfer device is required to provide electrical isolation as well as thermal conduction because all chiralities of BN nanotubes are semiconductors with a very large bandgap that can act as electrical insulators in many applications. It will be appreciated that other materials may also be substituted.
Nanotubes can be synthesized in various ways including arc-discharge, laser ablation, or chemical vapor deposition (CVD) processes and the like. Particular synthesis techniques are not critical to the present invention. As is known in the art, many of these techniques involve depositing a catalyst material onto a substrate and growing a cluster or bundle of nanotubes where catalyst material is present. Thus, while the present description refers to nanotubes, it is to be understood that clusters or bundles of nanotubes may be used to realize aspects of the invention.
As described more fully in the above-referenced co-pending application Ser. No. ______(Attorney Docket No. 022353-000110US), laminate nano-composite materials can be formed by depositing (or growing) alternating layers of matrix material and nanotubes.
Nano-composite material 100 can be formed, e.g., by depositing a layer of a matrix material with a desired thickness on a substrate (not explicitly shown in
One factor that will impact the thermal conductivity of the laminate structure is the thermal contact resistance between adjacent layers. At the interface between the matrix material 102 and the nanotubes in film layer 106, the thermal contact resistance will be reduced because the nanotubes are grown directly on the surface of the matrix material. The same result will be present at the interface between the matrix material 104 and the nanotubes in film layer 108. This is not necessarily the case at interface 106/104.
The relative proportions of matrix material and nanotubes making up the laminate nano-composite material can be varied, for instance by varying the relative thicknesses of nanotube films 106, 108 and matrix material layers 102, 104. In one embodiment, the nanotubes are around 100 μm long, while the matrix material sheets are about 50-100 angstroms (Å) (i.e., 5-10 nm) thick. In some embodiments, the matrix material is flexible or malleable, and the resulting nano-composite material may also be flexible or malleable.
Although the embodiment of the present invention shown in
In some embodiments, the “free” ends of the nanotubes are advantageously treated prior to depositing the next layer of base material in order to improve thermal contact between the layers.
At step 210, nanotubes are grown (e.g., using CVD or other conventional processes) or deposited onto a substrate or base material. After nanotube growth or deposition, a “treating” step 215 is performed to open the ends of the nanotubes and reduce variations in the lengths of the nanotubes. In one embodiment, step 215 includes exposing the nanotubes to an oxygen plasma or energetic oxygen at a suitable temperature (e.g., 700° C.) so that carbon near the tips is converted to CO and/or CO2. Although some embodiments utilize a treating step in which the ends of the nanotubes are opened as carbon near the tip is converted to CO and/or CO2, this is not required by the present invention. Alternative embodiments expose the nanotubes to an oxygen plasma or energetic oxygen in an environment in which residual carbon atoms not bonded in the nanotube lattice are removed while the ends of the nanotubes remain closed.
Once the nanotubes have been treated, a film of contact-enhancing material is optionally deposited (step 220) over the ends of the nanotubes in substantially uniform. thermal contact with the nanotubes. The contact-enhancing material is advantageously selected for high thermal conductivity; for example, copper, silver, aluminum, indium, or other metals are used in specific embodiments. In some embodiments, the contact-enhancing material is deposited in situ so that the tip of the opened or closed nanotube is not exposed to an ambient environment. In a particular embodiment, nanotubes with open ends are filled with the contact-enhancing material, although this is not required by the present invention. Filling of the nanotubes with the contact-enhancing material can increase the thermal contact between the nanotubes and the film of contact-enhancing material, thereby increasing the thermal conductivity of the structure.
At step 225, device fabrication continues as appropriate. In some embodiments, the film deposited at step 220 is used as the next base material layer for a laminate structure as illustrated in
Although the foregoing discussion relates to treatment of nanotubes in a laminate structure, this is not required by the present invention. “Treating” of portions of the nanotubes other than the ends of the nanotubes is performed in alternative embodiments. For example, nano-composite materials in which the nanotubes are randomly oriented and uniformly mixed into a matrix of amorphous material can be treated on an upper surface, opening the portions of the nanotubes lying in the plane of the upper surface. As a result, in a particular embodiment, ends or sides of the nanotubes lying in the plane of the upper surface come in contact with the oxygen plasma or energetic oxygen so that carbon lying in and near the upper surface is converted to CO and/or CO2. Subsequent deposition of a film of contact-enhancing material is performed as discussed in relation to the laminate structures. As discussed previously, deposition of contact-enhancing material can result in filling of the nanotubes with contact-enhancing material. In some embodiments, the contact-enhancing material filling the nanotubes and the film of contact-enhancing material are in physical contact. In other embodiments, the contact-enhancing material makes contact with the exposed portions of the nanotubes lying in the plane of the upper surface but does not fill the nanotubes.
The method of
In an alternative embodiment, testing of thermal properties is performed as part of the treatment process.
Although the laminate structure illustrated in
Moreover, although the treatment of nanotubes has been discussed in the context of a laminate nano-composite material, this is not required by the present invention. In some embodiments, the thermal contact system of the present invention will be useful to decrease the contact resistance between nanotubes and adjacent materials in other contexts, e.g., as described above.
As noted above, step 310 of process 300 (
The laser pulses may be incident on the material in a sequential or simultaneous manner, as desired by the operator. Of course, other radiation sources, including electron beams, could be utilized in place of the laser beams to provide a controllable source of incident radiation. In a specific embodiment, a single laser source is used with a moveable mirror to direct the laser pulses to predetermined locations on the sample. In this specific embodiment, laser pulses are directed to impinge on the material with a lateral spacing (x-axis) of about 1 cm and a longitudinal spacing (y-axis) of about 1 cm. Generally, the density of laser pulses is approximately equal to 1 pulse per square centimeter. The spacing between laser pulses can be larger for larger samples in a manufacturing environment or for optimizing manufacturing depending on the application. Of course, the distribution of the laser pulses need not be uniform. In this specific embodiment, the material is translated along the x and y-axes, providing for laser pulses impinging on the material in a two-dimensional pattern. In another embodiment, the laser source is translated. In alternative embodiments, multiple laser sources or optical beamsplitters are utilized to create simultaneous laser pulses incident on the material in either a linear arrangement of pulses or a two-dimensional arrangement of pulses.
In a particular embodiment, the wavelength and intensity of the laser pulses 210 is predetermined and matched to the absorption coefficient of the nano-engineered material to define a desired thermal profile. The intensity of the laser pulse can be increased by increasing the laser power or decreasing the spot size of the laser at the surface of the nano-engineered material. In this particular embodiment, the radiation will be absorbed in a small region surrounding the point where the pulse impinges on the lower surface of the nano-engineered material. In one embodiment, the laser spot size at the surface of the nano-engineered material ranges from 0.1 m-100 m. Absorption of the laser radiation will create a thermal gradient between the lower and upper surfaces of the material and result in dissipation of the absorbed energy through the upper surface of the material. Operation of the laser pulses in a simultaneous manner provides the operator with a means to establish initial thermal gradients that vary as a function of position. Merely by way of example, simultaneous laser pulses incident near the periphery of the material will establish a different thermal profile than a single laser pulse incident near the center of the material.
In the embodiment of the nano-engineered material 205 illustrated (not to scale) in
It will be appreciated that process 200 and 300 are illustrative and that variations and modifications are possible. Steps described as sequential may be executed in parallel, order of steps may be varied, and steps may be modified or combined. A variety of materials may be used for enhancing thermal contact, including copper, silver, aluminum, indium, other metals, or alloys. The treating step may include exposure to a variety of other etchants or gases.
In yet another alternative embodiment, the material selected for use in depositing the film of contact-enhancing material is chosen with a view to enhancing electrical conductivity in addition to or instead of thermal conductivity.
At step 610, nanotubes are grown (e.g., using CVD or other conventional processes) or deposited onto a substrate or base material. After nanotube growth or deposition, a “treating” step 615 is performed to open the ends of the nanotubes and reduce variations in the lengths of the nanotubes. In one embodiment, treating the nanotubes includes exposing the nanotubes to an oxygen plasma or energetic oxygen at a suitable temperature (e.g., 700° C.) so that carbon near the tips is converted to CO and/or CO2.
Once the nanotubes have been treated, a film of contact-enhancing material is deposited (step 620) over the ends of the nanotubes in substantially uniform electrical contact with the nanotubes. The contact-enhancing material is advantageously selected for high electrical conductivity; for example, gold, copper, silver, aluminum, indium, or other metals are used in specific embodiments.
At step 625, electrical conductivity testing is performed as part of the treatment process. As part of step 625, the uniformity of the electrical conductivity and the absolute values of electrical conductivity as a function of position are measured in some embodiments. Next, at step 630, device fabrication continues as appropriate. In some embodiments, the film deposited at step 620 is used as the next base material layer for a laminate structure as illustrated in
Thus, although the invention has been described with respect to specific embodiments, it will be appreciated that the invention is intended to cover all modifications and equivalents within the scope of the following Claims.
This application claims the benefit of the following provisional U.S. patent applications: Application No. 60/503,638, filed Sep. 16, 2003, entitled “System for Developing Production Nano-Material”; and Application No. 60/503,613, filed Sep. 16, 2003, entitled “Nano-Material Thermal and Electrical Contact System.” This application incorporates by reference for all purposes the entire disclosures of the following seven provisional U.S. patent applications: Application No. 60/503,591, filed Sep. 16, 2003, entitled “Nano-Material for System Thermal Management”; Application No. 60/503,612, filed Sep. 16, 2003, entitled “Oriented Nano-Material for System Thermal Management”; Application No. 60/503,638, filed Sep. 16, 2003, entitled “System for Developing Production Nano-Material”; Application No. 60/503,613, filed Sep. 16, 2003, entitled “Nano-Material Thermal and Electrical Contact System”; Application No. 60/532,244, filed Dec. 23, 2003, entitled “Nanotube Augmentation of Heat Exchange Structure”; Application No. 60/544,709, filed Feb. 13, 2004, entitled “Nano-Material Thermal Management System”; and Application No. 60/560,180, filed Apr. 6, 2004, entitled “Heat Transfer Structure.” The following five regular U.S. patent applications (including this one) are being filed concurrently, and the entire disclosures of the other four are incorporated by reference into this application for all purposes. Application Ser. No. ______, filed Sep. 16, 2004, entitled “Nano-Composite Materials for Thermal Management Applications” (Attorney Docket No. 022353-000110US); Application Ser. No. ______, filed Sep. 16, 2004, entitled “Nanostructure Augmentation of Surfaces for Enhanced Thermal Transfer with Increased Surface Area” (Attorney Docket No. 022353-000210US); Application Ser. No. ______, filed Sep. 16, 2004, entitled “Nanostructure Augmentation of Surfaces for Enhanced Thermal Transfer with Improved Contact” (Attorney Docket No. 022353-000220US); Application Ser. No. ______, filed Sep. 16, 2004, entitled “System for Developing Production Nano-Material” (Attorney Docket No. 022353-000310US); and Application Ser. No. ______, filed Sep. 16, 2004, entitled “Nano-Material Thermal and Electrical Contact System” (Attorney Docket No. 022353-000410US).
Number | Date | Country | |
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60503638 | Sep 2003 | US | |
60503613 | Sep 2003 | US |