Dynamically adjusting width of beam based on altitude
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H01Q-001/28
H01Q-019/13
H01Q-001/12
출원번호
US-0892161
(2013-05-10)
등록번호
US-9093754
(2015-07-28)
발명자
/ 주소
Behroozi, Cyrus
Teller, Eric
DeVaul, Richard Wayne
출원인 / 주소
Google Inc.
대리인 / 주소
McDonnell Boehen Hulbert & Berghoff LLP
인용정보
피인용 횟수 :
5인용 특허 :
3
초록▼
An antenna includes a radiator and a reflector and has a radiation pattern that is based at least in part on a separation distance between the radiator and the reflector. The antenna includes a linkage configured to adjust the separation distance based at least in part on the altitude of the antenna
An antenna includes a radiator and a reflector and has a radiation pattern that is based at least in part on a separation distance between the radiator and the reflector. The antenna includes a linkage configured to adjust the separation distance based at least in part on the altitude of the antenna. The resulting radiation pattern can be dynamically adjusted based on altitude of the antenna such that, while the antenna is aloft and the antenna is ground-facing, variations in geographic boundaries and intensity of the radiation received at ground level are at least partially compensated for by the dynamic adjustments to the radiation pattern.
대표청구항▼
1. An antenna configured to be mounted to a high altitude platform, the antenna comprising: a radiator configured to emit radiation according to a feed signal;a reflector configured to direct radiation emitted from the radiator such that reflected radiation is characterized by an emission pattern de
1. An antenna configured to be mounted to a high altitude platform, the antenna comprising: a radiator configured to emit radiation according to a feed signal;a reflector configured to direct radiation emitted from the radiator such that reflected radiation is characterized by an emission pattern determined at least in part by a separation distance between the radiator and the reflector, wherein the reflector is configured to be situated such that the emission pattern is directed in a ground-facing direction while the high altitude platform is aloft; anda linkage configured to adjust the separation distance between the radiator and the reflector according to an altitude of the high altitude platform. 2. The antenna according to claim 1, wherein the linkage includes a vessel arranged such that a change in volume of the vessel causes a corresponding change in the separation distance between the radiator and the reflector. 3. The antenna according to claim 2, wherein the vessel is configured such that the volume of the vessel is based on ambient pressure, thereby causing the separation distance to be based at least in part on the ambient pressure. 4. The antenna according to claim 2, wherein the vessel includes end caps connected between one or more sidewalls having a plurality of ribs to allow the vessel to change volume, in response to changes in ambient pressure, substantially by expanding or contracting a length of the one or more sidewalls, via the plurality of ribs, thereby changing a distance between the end caps, andwherein the end caps are connected such that the separation distance between the radiator and the reflector corresponds to the distance between the end caps. 5. The antenna according to claim 4, wherein the vessel includes a generally cylindrically-shaped aneroid with at least partially corrugated metallic sidewalls, andwherein an internal chamber of the vessel is substantially evacuated. 6. The antenna according to claim 1, further comprising a controller configured to: (i) determine the altitude of the high altitude platform, and (ii) cause the linkage to adjust the separation distance between the radiator and the reflector based on the determined altitude. 7. The antenna according to claim 1, wherein the linkage is further configured to dynamically adjust the separation distance between the radiator and the reflector by: (i) reducing the separation distance responsive to an increase in altitude of the antenna, and (ii) increasing the separation distance responsive to a decrease in altitude of the antenna. 8. The antenna according to claim 1, wherein the separation distance is dynamically adjusted such that, in a geographical region receiving the emitted radiation at ground level, variations in intensity of the received radiation at ground level due to variations in altitude of the high altitude platform are at least partially compensated for. 9. The antenna according to claim 1, wherein the separation distance is dynamically adjusted such that, in a geographical region receiving the emitted radiation at ground level, variations in a boundary of the geographical region receiving the radiation due to variations in altitude of the high altitude platform are at least partially compensated for. 10. The antenna according to claim 1, wherein the antenna is further configured to receive radiation from a region defined by the emission pattern. 11. The antenna according to claim 1, wherein the antenna is further configured to transmit signals to radio stations at ground level. 12. A balloon comprising: an envelope;a payload configured to be suspended from the envelope; andan antenna mounted to the payload and situated so as to be ground-facing while the balloon is aloft, the antenna including: (i) a radiator configured to emit radiation according to feed signals; (ii) a reflector configured to direct the radiation emitted from the radiator according to a radiation pattern determined at least in part according to a separation distance between the radiator and the reflector; and (iii) a linkage configured to adjust the separation distance between the radiator and the reflector according to an altitude of the balloon. 13. The balloon according to claim 12, wherein the linkage includes a vessel arranged such that a change in volume of the vessel causes a corresponding change in the separation distance between the radiator and the reflector. 14. The balloon according to claim 13, wherein the vessel is configured such that the volume of the vessel is based on ambient pressure, thereby causing the separation distance to be based, at least in part, on the ambient pressure. 15. The balloon according to claim 13, wherein the vessel includes end caps connected between one or more sidewalls having a plurality of ribs to allow the vessel to change volume, in response to changes in ambient pressure, substantially by expanding or contracting a length of the one or more sidewalls, via the plurality of ribs, thereby changing a distance between the end caps,wherein the end caps and the one or more sidewalls enclose an inner chamber that is substantially evacuated, andwherein the end caps are connected such that the separation distance between the radiator and the reflector corresponds to the distance between the end caps. 16. The balloon according to claim 12, further comprising a controller configured to: (i) determine the altitude of the balloon, and (ii) cause the linkage to adjust the separation distance between the radiator and the reflector based on the determined altitude. 17. The balloon according to claim 12, wherein the linkage is further configured to dynamically adjust the separation distance between the radiator and the reflector by: (i) reducing the separation distance responsive to an increase in altitude of the balloon, and (ii) increasing the separation distance responsive to a decrease in altitude of the balloon. 18. A method comprising: emitting radiation from an antenna configured to be mounted to a payload of an associated balloon, wherein the antenna has an emission pattern determined at least in part by a separation distance between a radiator and a reflector of the antenna, and wherein the antenna is configured to be situated such that the emission pattern is directed in a ground-facing direction while the associated balloon is aloft and the antenna is mounted to the payload;decreasing the separation distance between the radiator and the reflector responsive to a decrease in altitude of the associated balloon; andincreasing the separation distance between the radiator and the reflector responsive to an increase in altitude of the associated balloon. 19. The method according to claim 18, further comprising: determining the altitude of the associated balloon; andcausing the linkage to adjust the separation distance between the radiator and the reflector based on the determined altitude. 20. The method according to claim 18, wherein the linkage includes a vessel arranged such that a change in volume of the vessel causes a corresponding change in the separation distance between the radiator and the reflector; andwherein the vessel is configured such that the volume of the vessel is based on ambient pressure, thereby causing the separation distance to be based, at least in part, on the ambient pressure.
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