Multiband wireless data transmission between aircraft and ground systems
US-2016344467-A1 · Nov 24, 2016 · US
US9450311B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9450311-B2 |
| Application number | US-201313949505-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 24, 2013 |
| Priority date | Jul 24, 2013 |
| Publication date | Sep 20, 2016 |
| Grant date | Sep 20, 2016 |
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A rotationally polarized antenna includes a radiating element that is held in a skewed orientation with respect to an underlying polarization-dependent electromagnetic band gap (PDEBG) structure. The radiating element and the PDEBG structure are both housed within a conductive cavity. The radiating element, the PDEBG structure, and the cavity are designed together to achieve an antenna having improved operational characteristics (e.g., an enhanced circular polarization bandwidth, etc.). In some embodiments, the antenna may be implemented as a flush mounted or conformal antenna on an outer surface of a supporting platform.
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What is claimed is: 1. A rotationally polarized antenna comprising: a ground plane; a polarization dependent electromagnetic band gap (PDEBG) structure disposed above the ground plane, the PDEBG structure having a number of unit cells arranged in rows and columns; an orientable radiating element disposed above the PDEBG structure, the orientable radiating element having a long dimension and a short dimension; and a conductive cavity encompassing the PDEBG structure and the orientable radiating element, the conductive cavity being open on a radiating side of the antenna, wherein a distance between side walls of the conductive cavity and one or more outermost edges of the PDEBG structure produces an additional resonance in an electrical response of the antenna, the distance selected to increase (i) an effective aperture of the antenna and (ii) a bandwidth of the antenna, in relation to the effective aperture and bandwidth without the additional resonance; wherein the orientable radiating element is oriented at a non-zero angle with respect to the rows and columns of the PDEBG structure, the angle selected such that the orientable radiating element supports one of: (i) substantially equal horizontal and vertical electric field magnitudes for use with circularly polarized waves, and (ii) different horizontal and vertical electric field magnitudes for use with non-circular elliptically polarized waves. 2. The antenna of claim 1 , wherein: the antenna is configured for use with circularly polarized waves. 3. The antenna of claim 1 , wherein: the PDEBG structure, the orientable radiating element, and the conductive cavity are configured together to achieve an enhanced operational bandwidth. 4. The antenna of claim 1 , wherein: the orientable radiating element includes one of: a patch element, a dipole element, and a monopole element. 5. The antenna of claim 1 , further comprising: a feed coupled to the orientable radiating element through the ground plane and the PDEBG structure. 6. The antenna of claim 1 , wherein: the conductive cavity has a floor that serves as the ground plane of the antenna. 7. The antenna of claim 1 , further comprising: a radome layer covering an upper surface of the orientable radiating element. 8. The antenna of claim 7 , wherein: an upper surface of the radome layer is substantially flush with an upper edge of the conductive cavity. 9. The antenna of claim 1 , wherein: an upper surface of the orientable radiating element is substantially flush with an upper edge of the conductive cavity. 10. The antenna of claim 1 , wherein: the conductive cavity is formed within an outer skin of a vehicle; and an upper surface of the antenna is flush with the outer skin of the vehicle. 11. The antenna of claim 10 , wherein: the vehicle includes one of: a ground vehicle, a watercraft, an aircraft, and a spacecraft. 12. The antenna of claim 1 , wherein: a length, a width, and a height of the conductive cavity are each less than a wavelength at the center frequency of the antenna. 13. The antenna of claim 1 , wherein: the antenna is conformal to a curved surface of a mounting platform. 14. The antenna of claim 1 , wherein: the orientable radiating element is a first orientable radiating element; and the antenna further comprises a second orientable radiating element disposed above the PDEBG structure, the second orientable radiating element having a long dimension and a short dimension, the second orientable radiating element having an orientation that is orthogonal to an orientation of the first orientable radiating element, wherein the second orientable radiating element is on a different metal layer than the first orientable radiating element. 15. The rotationally polarized antenna of claim 1 , wherein the distance is selected by adjusting at least one of a length and a width of the conductive cavity relative to the PDEBG structure. 16. An antenna assembly for use in forming a rotationally polarized antenna, comprising: a polarization dependent electromagnetic band gap (PDEBG) structure having a plurality of unit cells arranged in rows and columns; and an orientable radiating element disposed above the PDEBG structure, the orientable radiating element having a long dimension and a short dimension, the orientable radiating element being held in a fixed position with respect to the PDEBG structure so that the long dimension of the orientable radiating element forms a non-zero angle with both the rows and columns of the PDEBG structure, the non-zero angle selected such that the orientable radiating element supports one of: (i) substantially equal horizontal and vertical electric field magnitudes for use with circularly polarized waves, and (ii) different horizontal and vertical electric field magnitudes for use with non-circular elliptically polarized waves; wherein the antenna assembly is configured for insertion into a conductive cavity having dimensions that are selected to form an antenna having radiation performance that is characteristic of a larger antenna, wherein a distance between side walls of the conductive cavity and one or more outermost edges of the PDEBG structure produces an additional resonance in an electrical response of the antenna, the distance selected to increase (i) an effective aperture of the antenna and (ii) a bandwidth of the antenna, in relation to the effective aperture and bandwidth without the additional resonance. 17. The antenna assembly of claim 16 , wherein: the PDEBG structure and the orientable radiating element are formed on printed circuit boards. 18. The antenna assembly of claim 16 , further comprising: a ground plane on an opposite side of the PDEBG structure from the orientable radiating element, the ground plane to contact a floor of the conductive cavity when the antenna assembly is installed therein. 19. The antenna assembly of claim 16 , further comprising: a feed coupled to the orientable radiating element through the PDEBG structure. 20. The antenna assembly of claim 16 , wherein: the orientable radiating element is a patch element. 21. The antenna assembly of claim 16 , wherein: the orientable radiating element is one of: a dipole element and a monopole element. 22. The antenna assembly of claim 16 , wherein: the antenna assembly is configured for insertion into a conductive cavity within an outer skin of a vehicle; and the antenna assembly has a height that allows the antenna assembly to be mounted in the conductive cavity substantially flush to the outer skin of the vehicle. 23. The antenna assembly of claim 16 , wherein: the orientable radiating element is a first orientable radiating element; and the antenna assembly further comprises a second orientable radiating element disposed above the PDEBG structure, the second orientable radiating element having a long dimension and a short dimension, the second orientable radiating element having an orientation that is orthogonal to an orientation of the first orientable radiating element, wherein the second orientable radiating element is on a different metal layer than the first orientable radiating element. 24. The antenna assembly of claim 16 , wherein the distance is selected by adjusting at least one of a length and a width of the conductive cavity relative to the PDEBG structure. 25. A method for designing a rotationally polarized antenna having at leas
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