Carbon nanotubes (CNTs) are carbon allotropes having a generally cylindrical nanostructure. They have unusual properties that make them valuable for many different technologies. For instance, some CNTs can have high thermal and electrical conductivity, making them suitable for replacing metal heating elements. Due to their much lighter mass, substituting CNTs for metal heating components can reduce the overall weight of a heating component significantly. This makes the use of CNTs of particular interest for applications where weight is critical, such as in aerospace and aviation technologies.
Carbon nanotubes are commercially available in several different forms. Forms include pure carbon nanotube nonwoven sheet material (CNT-NSM) and CNT-filled thermoplastic films. In a CNT-NSM, carbon nanotubes are arranged together to form a sheet. No adhesives or polymers are typically used to attach CNTs to one another in a CNT-NSM. Instead, CNT particles are attached to one another via Van der Waals forces. In a CNT-filled thermoplastic film, individual CNT particles are distributed throughout the film. Unfortunately, these commercially available CNT materials do not offer off-the-shelf electrical resistivities that allow for their use in different ice protection applications.
A heating element includes a first carbon nanotube (CNT) layer and a second CNT layer. At least a portion of the first CNT layer overlaps at least a portion of the second CNT layer, and the first CNT layer includes a first perforated region having a plurality of perforations.
A heating element includes a perforated CNT sheet.
A method of forming a heating element containing carbon nanotubes includes perforating a first CNT layer so that it includes a perforated region having a plurality of perforations and stacking the first CNT layer with a second CNT layer such that at least a portion of the first CNT layer overlaps at least a portion of the second CNT layer.
This disclosure provides the ability to tailor the resistivity of carbon nanotubes (CNT) to application-specific heating or ice protection needs by utilizing perforated CNT sheets or stacked CNT sheets or layers where at least one of the CNT layers is perforated. Using perforated CNT sheets or combining perforated and non-perforated CNT sheet layers in one heating element will allow the resistivity of the heating element to be varied to suit individual application heating, anti-icing and/or de-icing needs.
As shown in
In other embodiments, CNT layer 10 can be a CNT-filled thermoplastic film. Carbon nanotube-filled thermoplastic films include a thermoplastic matrix through which CNT particles are dispersed. The thermoplastic matrix is typically a solid at room temperature (˜25° C.). Examples of suitable materials for the thermoplastic matrix include epoxies, phenolic resins, bismaleimides, polyimides, polyesters, polyurethanes and polyether ether ketones. The electrical resistivity of CNT-filled thermoplastic films can vary depending on the uniformity of the distribution of CNT particles within the film. Where CNTs are generally uniformly distributed throughout the film, the electrical resistance is generally uniform throughout the film.
Carbon nanotube layer 10 can be attached or, in the case of composite components, embedded underneath an outer skin of a component (not shown) requiring ice protection (e.g., anti-icing and/or de-icing). An electric power source is connected to CNT layer 10. When electric current passes through CNT layer 10, heat is given off by the CNTs present within layer 10 by Joule heating. This heat provides ice protection to the component in which CNT layer 10 is attached, embedded or installed. In other embodiments, CNT layer 10 can be used in other heating applications, such as wind turbines, heated floor panels, local comfort heating applications, area heating, water tank heating blankets and other aerospace heating applications.
As described herein, whether a CNT sheet or a CNT-filled thermoplastic film, creating perforations within CNT layer 10 allows the electrical resistivity of CNT layer 10 to be modified to suit particular ice protection applications.
As shown in
In some embodiments, perforations 12 can have generally the same diameter. In other cases, some perforations 12 can have different diameters than others. Perforations 12 can be circular or perforations 12 can take other geometric shapes. In some embodiments, perforations 12 can be uniformly distributed throughout a region 14 of CNT layer 10. In some cases, CNT layer 10 can include a region with perforations and a region without perforations. The presence or absence of perforations is used to tailor the electrical resistivity of CNT layer 10. Perforating CNT layer 10 allows its use for heating applications in aerospace, marine and wind turbines and other related technologies.
As perforations 12 in CNT layer 10 all have essentially the same diameter, the perforation density increases, by region, from right to left across CNT layer 10 as shown in
In other embodiments, multiple CNT layers are used to tune the electrical resistivity of a CNT heating element.
More than two layers can be stacked together in a similar fashion to form a heating element. For example, the heating element could include one solid layer and two perforated layers, two solid layers and two perforated layers, two solid layers and one perforated layer, three perforated layers, and so on. The use of perforations 12 in one or more of the stacked layers alter the electrical resistance of one or more regions of the stack. In some embodiments, ten to fifteen CNT layers 10 can be stacked together. In this way, the overall electrical resistivity of a heating element made up of CNT layers can be modified based on how the CNT layers are stacked.
In the embodiment schematically illustrated in
While the instant disclosure refers particularly to carbon nanotubes, it is theorized that the resistivity of sheets and films containing other electrically conductive carbon allotropes (e.g., graphene nanoribbons) would behave in a similar fashion. Embodiments containing other suitable carbon allotropes are within the scope of the instant disclosure.
The methods disclosed herein provide means for reducing the resistivity of CNT-NSMs and CNT-filled films without increasing their mass or the chemical processes needed to add resistivity-reducing functional groups to the carbon backbone of the CNT materials. The disclosure allows commercially available CNT-NSMs and CNT-filled films to be useful for wind turbine, aerospace and aircraft heating, anti-icing and de-icing applications.
Discussion of Possible Embodiments
The following are non-exclusive descriptions of possible embodiments of the present invention.
A heating element can include a first carbon nanotube (CNT) layer and a second CNT layer where at least a portion of the first CNT layer overlaps at least a portion of the second CNT layer, and where the first CNT layer comprises a first perforated region having a plurality of perforations.
The heating element of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
The first perforated region of the first CNT layer can overlap with the portion of the second CNT layer.
The second CNT layer can include a second perforated region having a plurality of perforations.
The first perforated region of the first CNT layer can overlap with the second perforated region of the second CNT layer.
The perforations in the first perforated region can be arranged such that they do not overlap perforations in the second perforated region.
At least one of the plurality of perforations in the first perforated region can overlap at least one of the plurality of perforations in the second perforated region.
The first and second CNT layers can be formed from a folded CNT sheet.
The plurality of perforations in the first perforated region can make up about 10% to about 50% of the first perforated region surface area.
The plurality of perforations in the first perforated region can make up about 20% to about 40% of the first perforated region surface area.
The plurality of perforations in the first perforated region can have generally the same diameter.
The plurality of perforations in the first perforated region can be generally uniformly distributed.
A heating element can include a perforated CNT sheet.
The heating element of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
The CNT sheet can include a first perforated region having a plurality of perforations and a first perforation density and a second perforated region having a plurality of perforations and a second perforation density different from the first perforation density
The second perforated region can have a different number of perforations than the first perforated region.
The perforations in the second perforated region can have a different diameter than perforations in the first perforated region.
The plurality of perforations in the first perforated region can make up about 10% to about 50% of the first perforated region surface area, and the plurality of perforations in the second perforated region can make up about 10% to about 50% of the second perforated region surface area.
The plurality of perforations in the first perforated region can make up about 20% to about 40% of the first perforated region surface area, and the plurality of perforations in the second perforated region can make up about 20% to about 40% of the second perforated region surface area.
A method of forming a heating element containing carbon nanotubes can include perforating a first CNT layer so that it has a perforated region having a plurality of perforations and stacking the first CNT layer with a second CNT layer such that at least a portion of the first CNT layer overlaps at least a portion of the second CNT layer.
The method of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations and/or additional components:
The first and second CNT layers can be stacked such that the perforated region overlaps with the portion of the second CNT layer.
The method can further include perforating the second CNT layer so that it has a second perforated region having a plurality of perforations.
While the invention has been described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
7288490 | Delzeit | Oct 2007 | B1 |
7947145 | Wang | May 2011 | B2 |
8450930 | Liu | May 2013 | B2 |
8664573 | Shah et al. | Mar 2014 | B2 |
20050266766 | Wei | Dec 2005 | A1 |
20060172179 | Gu | Aug 2006 | A1 |
20100147829 | Liu | Jun 2010 | A1 |
20100176118 | Lee et al. | Jul 2010 | A1 |
20110240111 | Yamazaki | Oct 2011 | A1 |
20120171411 | Lashmore | Jul 2012 | A1 |
20140070054 | Burton et al. | Mar 2014 | A1 |
20140072778 | Feng | Mar 2014 | A1 |
20140209375 | Linow et al. | Jul 2014 | A1 |
20150189699 | Ploshikhin | Jul 2015 | A1 |
20150321147 | Fleming | Nov 2015 | A1 |
20160145784 | Schauer | May 2016 | A1 |
Number | Date | Country |
---|---|---|
1826119 | Aug 2007 | EP |
3013119 | Apr 2016 | EP |
WO2016081690 | May 2016 | WO |
WO2016126827 | Aug 2016 | WO |
WO2016144683 | Sep 2016 | WO |
Entry |
---|
Extended European Search Report for EP Serial No. 17205719.2, dated May 3, 2018, 7 Pages. |
Number | Date | Country | |
---|---|---|---|
20180168001 A1 | Jun 2018 | US |