APPARATUS AND SYSTEMS FOR HEATING A SATELLITE ANTENNA REFLECTOR

• US 20100328167A1
• Filed: 06/25/2009
• Published: 12/30/2010
• Est. Priority Date: 06/25/2009
• Status: Abandoned Application

• Current Assignee: Echostar UK Holdings Ltd (Echostar Corporation)
• Original Assignee: Eldon Technology Limited (Dish Network Corporation)
• Inventors: Stephens, Mark Benedict
• Application Number:
  US12/492,038
• Publication Number:
  US 20100328167A1
• Time in Patent Office: Days
• US Class Current: 343/704
• CPC Class Codes: H01Q 1/02 Arrangements for de-icing; Arrangements for drying-out ; Arrangements for cooling; Arrangements for preventing corrosion

Abstract

Apparatus and systems are described herein for heating a satellite antenna reflector to remove snow and ice from the reflector surface. A satellite heating system includes a heating element attached to the satellite antenna reflector and a battery associated with the heating element. A satellite receiver provides a satellite antenna with a supply voltage over cabling communicatively coupling the satellite receiver and the satellite antenna. The supply voltage is further utilized to charge the battery. The heating element may then utilize the power supplied by the battery to heat the surface of the reflector, removing ice and snow from the reflector surface.

Claims

1. A satellite dish heating system comprising:

a heating element that attaches to a satellite antenna reflector;

a battery;

a switch operable to communicatively couple and decouple the heating element and the battery;

control logic operable to command the switch to communicatively couple the heating element and the battery, the heating element drawing power from the battery to heat the surface of the satellite antenna reflector; and

cabling communicatively coupling the battery, the control logic and a satellite antenna to a satellite receiver, the satellite antenna exchanging signals with the satellite receiver over the cabling, the cabling further carrying power from the satellite receiver to the battery, the satellite antenna and the control logic, the battery operable to trickle charge using the power supplied by the satellite receiver.

2. The satellite dish heating system of claim 1, wherein the battery is attached to the satellite antenna reflector.

3. The satellite dish heating system of claim 1, wherein the battery is attached to a mounting mast for the satellite antenna reflector.

4. The satellite dish heating system of claim 1, wherein the control logic is further operable to receive a request from the satellite receiver requesting heating of the satellite antenna reflector, the control logic operable to command the switch to communicatively couple the heating element and the battery responsive to the request.

5. The satellite dish heating system of claim 1, further comprising:

a sensor operable to detect snow and ice on the surface of the satellite antenna reflector;

the control logic operable to command the switch to communicatively couple the heating element and the battery based on input from the sensor.

6. The satellite dish heating system of claim 5, wherein the sensor comprises a light sensor.

7. The satellite dish heating system of claim 6, further comprising an electronic temperature sensor operable to detect a temperature of the ambient air around the satellite antenna reflector, the control logic further operable to command the switch to communicatively couple the heating element and the battery based on the temperature.

8. The satellite dish heating system of claim 6, wherein the control logic is further operable to command the switch to communicatively couple the heating element and the battery based on a time of day.

9. The satellite dish heating system of claim 1, wherein the heating element comprises heating tape attached to a surface of the satellite antenna reflector.

10. The satellite dish heating system of claim 9, wherein the heating element comprises heating wires embedded within the satellite antenna reflector.

11. A system comprising:

a satellite antenna reflector;

a satellite antenna operable to receive a signal reflected from the satellite antenna reflector;

a heating element that attaches to the satellite antenna reflector;

a battery mounted proximate the satellite antenna reflector;

a switch operable to communicatively couple and decouple the heating element and the battery;

control logic operable to command the switch to communicatively couple the heating element and the battery, the heating element drawing power from the battery to heat the surface of the satellite antenna reflector; and

cabling communicatively coupling the battery, the control logic and a satellite antenna to a satellite receiver, the satellite antenna exchanging information with the satellite receiver over the cabling based on the signal, the cabling further carrying power from the satellite receiver to the battery, the satellite antenna and the control logic, the battery operable to trickle charge using the power supplied by the satellite receiver.

12. The system of claim 11, wherein the battery is attached to the satellite antenna reflector or a mounting mast for the satellite antenna reflector.

13. The system of claim 11, wherein the control logic is further operable to receive a request from the satellite receiver to heat the satellite antenna reflector, the control logic operable to command the switch to communicatively couple the heating element and the battery responsive to the request.

14. The system of claim 11, further comprising:

a light sensor operable to detect snow and ice on the surface of the satellite antenna reflector;

the control logic operable to command the switch to communicatively couple the heating element and the battery based on input from the sensor.

15. The system of claim 14, further comprising an electronic temperature sensor operable to detect a temperature of the ambient air around the satellite antenna reflector, the control logic further operable to command the switch to communicatively couple the heating element and the battery based on the temperature.

16. The system of claim 14, wherein the control logic is further operable to command the switch to communicatively couple the heating element and the battery based on a time of day.

17. The system of claim 11, wherein the heating element comprises heating tape attached to a surface of the satellite antenna reflector.

18. The system of claim 11, wherein the heating element comprises heating wires embedded within the satellite antenna reflector.

19. A satellite dish heating system comprising:

a heating element that attaches to a satellite antenna reflector;

a battery;

a switch operable to communicatively couple and decouple the heating element and the battery;

a light sensor operable to detect snow and ice on the surface of the satellite antenna reflector;

an electronic temperature sensor operable to detect a temperature of the ambient air around the satellite antenna reflector;

a clock;

control logic operable to command the switch to communicatively couple the heating element and the battery based on input from the light sensor and at least one of the electronic temperature sensor and the clock, the heating element drawing power from the battery to heat the surface of the satellite antenna reflector; and

cabling communicatively coupling the battery, the control logic and a satellite antenna to a satellite receiver, the satellite antenna exchanging signals with the satellite receiver over the cabling, the cabling further carrying power from the satellite receiver to the battery, the satellite antenna and the control logic, the battery operable to trickle charge using the power supplied by the satellite receiver.

20. The satellite dish heating system of claim 19, wherein the control logic is integrated with the satellite antenna.