This disclosure relates to the emissivity of materials, and in particular to materials having a variable emissivity.
Various coatings for controlling the emissivity of a surface have been described. U.S. Pat. No. 4,131,593 to Mar et al. describes a low infrared emissivity paint, which can be utilized as a protective medium against the harmful effects of a nuclear explosion. U.S. Pat. No. 4,462,883 to Hart describes a low emissivity coating on a transparent substrate of glass or plastic. U.S. Pat. No. 6,974,629 to Krisko et al. describes a low emissivity, soil resistant coating for glass surfaces.
These U.S. Patents describe how to lower the emissivity of a surface. However, they do not describe how to dynamically vary the emissivity, so that, for example, a material or surface has a relatively high emissivity at one time and has a relatively low emissivity at another time.
What is needed is a material for which the emissivity can be controlled to dynamically vary. Also needed is a way of controlling the operational wavelengths over which the emissivity of the material can be controlled, including the infrared wavelengths. The embodiments of the present disclosure answer these and other needs.
In a first embodiment disclosed herein, a material includes a first metallic layer having a first aperture, a second metallic layer having a second aperture, and a variable dielectric layer interposed between the first metallic layer and the second metallic layer.
In another embodiment disclosed herein, a method for manufacturing a variable emissivity material includes selecting a first metallic layer having a first aperture, selecting a second metallic layer having a second aperture, and joining the first and second metallic layers to a variable dielectric layer interposed between the first metallic layer and the second metallic layer.
In another embodiment disclosed herein, a method for creating a variable emissivity material includes selecting a first metallic layer having a first aperture, selecting a second metallic layer having a second aperture, joining the first and second metallic layers to a variable dielectric layer interposed between the first metallic layer and the second metallic layer, and applying an electric field between the first metallic layer and the second metallic layer.
In another embodiment disclosed herein, a method for creating a variable emissivity material includes selecting a first metallic layer having a first aperture, selecting a second metallic layer having a second aperture, joining the first and second metallic layers to a variable dielectric layer interposed between the first metallic layer and the second metallic layer and providing a temperature change in the range of about 50 to 100 degrees centigrade to the variable dielectric layer.
These and other features and advantages will become further apparent from the detailed description and accompanying figures that follow. In the figures and description, numerals indicate the various features, like numerals referring to like features throughout both the drawings and the description.
Referring to
The variable dielectric layer 20 can be selected from the family of ferroelectric materials, and one such ferroelectric material is vanadium oxide. The internal electric dipoles of a ferroelectric material are physically tied to the ferroelectric material lattice so that anything that changes the physical lattice will change the strength of the dipoles and change the conductivity of the ferroelectric material. Two stimuli that will change the lattice dimensions and hence the conductivity of a ferroelectric material are voltage and temperature. Voltage creates an electric field that affect the dipoles.
The variable dielectric layer 20 is separated from the first and second metallic layers 12 and 16 by first dielectric layer 22 and second dielectric layer 24, respectively. First dielectric layer 22 and second dielectric layer 24 are specifically not made of ferroelectric materials, but rather are nearly inert dielectric materials that have low permittivity. In contrast, the variable dielectric layer 20 has a variable permittivity, such that in the activated state the variable dielectric layer 20 has a high permittivity compared to the first dielectric layer 22 and second dielectric layer 24. In the deactivated state the permittivity of the variable dielectric layer 20 changes to a lower permittivity compared to the high permittivity of the activated state.
Also in the activated state the variable dielectric layer 20 is more conductive than in the deactivated state. Thus, in the activated state the variable dielectric layer 20 has conductive properties similar to a metallic layer, and therefore more incident radiation is reflected from the variable dielectric layer 20, which results in the variable emissivity material 10 having a low emissivity. In the deactivated state the variable dielectric layer 20 is less conductive and therefore less incident radiation is reflected from the variable dielectric layer 20. Thus, in the deactivated state the variable emissivity material 10 has a relatively high emissivity.
Below the second metallic layer 16 is a third dielectric layer 26 and below the third dielectric layer 26 is a third metallic layer 30, which is provided to act as a ground plane. The third dielectric layer 26 is similar in material composition to first dielectric layer 22 and second dielectric layer 24 and is also a nearly inert dielectric with low permittivity.
In one embodiment, first and second metallic layers 12 and 16 may be about 100 nm thick, first and second dielectric layers 22 and 24 may be each about 200 nm thick, third dielectric layer 26 may be about 400 nm thick, and variable dielectric layer 20 may be about 100 nm thick. The resulting material is therefore very thin and can be manufactured as a film, which can then be applied to a surface.
The emissivity of a material is defined as the ratio of energy radiated by the material to energy radiated by a black body at the same temperature. It is a measure of a material's ability to absorb incident radiation and radiate energy. For an object in thermal equilibrium, emissivity equals absorptivity. Thus, an object that absorbs less incident radiation will also emit less radiation than an ideal black body. A true black body has an emissivity equal to 1 while any real object has an emissivity less than 1, because a black body is an object that absorbs all incident radiation, including light that falls on it. Because no light is reflected or transmitted, the object appears black when it is at zero degrees Kelvin. Because a real object reflects some light, a high reflected power from a material indicates a low emissivity, while a low reflected power from a material indicates a higher emissivity.
The variable dielectric layer 20 of the variable emissivity material 10 can be activated to cause the material to evince a comparatively lower emissivity by applying a voltage across the first and second metallic layers 12 and 16. In one nonlimiting example, variable dielectric layer 20 can be activated by applying a voltage in the range of 5 to 100 volts across the first metallic layer 12 and the second metallic layer 16. Alternatively, in another nonlimiting example, the variable dielectric layer 20 can be activated by a causing a temperature change to the variable dielectric layer 20 in the range of 50 to 100 degrees centigrade. As discussed above, in the activated state the variable dielectric layer 20 is more conductive than in the deactivated state. Thus, in the activated state the variable dielectric layer 20 has conductive properties similar to a metallic layer, and therefore more incident radiation is reflected from the variable dielectric layer 20, which results in the variable emissivity material 10 having a low emissivity. In the deactivated state the variable dielectric layer 20 is less conductive and therefore less incident radiation is reflected from the variable dielectric layer 20. Thus, in the deactivated state the variable emissivity material 10 has a relatively high emissivity.
The wavelengths for which the emissivity of the material can be controlled, which are referred to herein as the operational wavelengths, depend on the spacing of the apertures in the array and on the width of the apertures, as well as other factors.
As shown in
As shown in
The operational wavelength range of the material is wider for a relatively wide aperture, because in the deactivated state the reflected power is lower and the emissivity higher over a wider range of bandwidths; however, the difference in the reflected power or the difference in the emissivity of the variable emissivity material 10 between the activated and deactivated states is greater for the relatively narrower aperture. The selection of aperture width is therefore a tradeoff and depends on the application for the variable emissivity material.
There are many shapes of apertures that can be used in the first and second metallic layers 12 and 16.
Another shape of aperture is shown in
The pitch of the periodically spaced apertures or the spacing between the midpoints of adjacent apertures can vary; however, for infrared applications the pitch of the apertures is typically in the range of about 5 to 20 microns.
The variable emissivity material 10 can be laminated on a surface and thereby change the emissivity of the surface. Applications include military applications. In one nonlimiting example, the variable emissivity material 10 can be laminated onto a surface such as the skin of a missile or an airplane, which would allow the effective emissivity of the missile or airplane to be varied. Thus at one time the variable emissivity material 10 can be caused to have a high emissivity, which would give the missile or airplane a high emissivity and thus reduce the reflection of incident radiation from the missile or airplane. At another time the variable emissivity material 10 can be caused to have a low emissivity, which would give the missile or airplane a low emissivity and thus increase the reflection of incident radiation from the missile or airplane. This might create confusion to a sensor that is trying to track such an object.
Commercial applications may include applications where it is desirable to vary the emissivity of a surface. Thus at one time the variable emissivity material 10 laminated on the surface can be caused to have a high emissivity and the surface would absorb more radiation and thus, as a nonlimiting example, be warmer. At another time the variable emissivity material 10 can be caused to have a low emissivity and the surface would reflect more radiation, and thus, as a nonlimiting example, be cooler.
Having now described the invention in accordance with the requirements of the patent statutes, those skilled in this art will understand how to make changes and modifications to the present invention to meet their specific requirements or conditions. Such changes and modifications may be made without departing from the scope and spirit of the invention as disclosed herein.
The foregoing Detailed Description of exemplary and preferred embodiments is presented for purposes of illustration and disclosure in accordance with the requirements of the law. It is not intended to be exhaustive nor to limit the invention to the precise form(s) described, but only to enable others skilled in the art to understand how the invention may be suited for a particular use or implementation. The possibility of modifications and variations will be apparent to practitioners skilled in the art. No limitation is intended by the description of exemplary embodiments which may have included tolerances, feature dimensions, specific operating conditions, engineering specifications, or the like, and which may vary between implementations or with changes to the state of the art, and no limitation should be implied therefrom. Applicant has made this disclosure with respect to the current state of the art, but also contemplates advancements and that adaptations in the future may take into consideration of those advancements, namely in accordance with the then current state of the art. It is intended that the scope of the invention be defined by the Claims as written and equivalents as applicable. Reference to a claim element in the singular is not intended to mean “one and only one” unless explicitly so stated. Moreover, no element, component, nor method or process step in this disclosure is intended to be dedicated to the public regardless of whether the element, component, or step is explicitly recited in the Claims. No claim element herein is to be construed under the provisions of 35 U.S.C. Sec. 112, sixth paragraph, unless the element is expressly recited using the phrase “means for . . . ” and no method or process step herein is to be construed under those provisions unless the step, or steps, are expressly recited using the phrase “comprising the step(s) of . . . . ”
Number | Name | Date | Kind |
---|---|---|---|
2992426 | Borcherdt | Jul 1961 | A |
3174537 | Meyer | Mar 1965 | A |
3540047 | Hach et al. | Nov 1970 | A |
3733606 | Johansson | May 1973 | A |
4038660 | Connolly et al. | Jul 1977 | A |
4131593 | Mar | Dec 1978 | A |
4462883 | Hart | Jul 1984 | A |
4640851 | Pusch | Feb 1987 | A |
4863245 | Roxlo | Sep 1989 | A |
4987418 | Kosowsky et al. | Jan 1991 | A |
5081455 | Inui et al. | Jan 1992 | A |
5103103 | Radford et al. | Apr 1992 | A |
5214432 | Kasevich et al. | May 1993 | A |
5274241 | Radford et al. | Dec 1993 | A |
5385623 | Diaz | Jan 1995 | A |
5627541 | Haley et al. | May 1997 | A |
5976666 | Narang et al. | Nov 1999 | A |
6225939 | Lind | May 2001 | B1 |
6335699 | Honma | Jan 2002 | B1 |
6549114 | Whitney et al. | Apr 2003 | B2 |
6753075 | Leupolz et al. | Jun 2004 | B1 |
6897820 | Frenkel | May 2005 | B2 |
6974629 | Krisko | Dec 2005 | B1 |
7903040 | Gevorgian et al. | Mar 2011 | B2 |
20020037421 | Arnaud et al. | Mar 2002 | A1 |
20020080089 | Bergstedt et al. | Jun 2002 | A1 |
20060012508 | Messano | Jan 2006 | A1 |
20080192331 | Wang et al. | Aug 2008 | A1 |