Hot air de-icing of satellite antenna with cover

• US 5,729,238 A
• Filed: 07/16/1996
• Issued: 03/17/1998
• Est. Priority Date: 09/19/1995
• Status: Expired due to Term

• Current Assignee: William B. Walton Jr
• Original Assignee: William B. Walton Jr
• Inventors: Walton, William B. Jr.
• Primary Examiner(s): Le, Hoanganh T.
• Application Number:
  US08/680,777
• Time in Patent Office: 609 Days
• Field of Search: 343/704, 343/872, 392/420, 392/422, 392/431, 392/426
• 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

A system for preventing the interruption of satellite communications between an earth antenna and a satellite during inclement weather. The system is comprised of a cover, which covers the antenna and substantially prevents the accumulation of snow and precipitation on the antenna, and a heating system which provides heated air to a space between the cover and the antenna to inhibit snow from sticking to the cover and also to inhibit the formation of frozen moisture on the cover during freezing rain and freezing fog conditions. In one embodiment, the system has an electric, gas or oil heater and a blower system which draws air from the space between the cover and the antenna, heats this air and then recirculates the heated air back to the space. Further, the heating system is equipped with a temperature and moisture sensor unit and a controller. The sensor detects the ambient temperature and humidity conditions which are received by the controller to enable heater and blower system to operate within the predetermined temperature and humidity ranges.

Claims

1. A system for reducing accumulations of moisture on a front reflecting surface of a satellite antenna having an outer lip comprising:

a flexible cover having an opening which is dimensioned to mount on said outer lip of said antenna with the cover positioned over said front reflecting surface of said satellite antenna so as to define a space between said front reflecting surface of said antenna and said cover whereby said cover reduces accumulations of frozen precipitation on said front reflecting surface of said satellite antenna while permitting satellite signals to pass therethrough;

an air supply system which provides unheated air to said space between said cover and said front reflecting surface so as to induce positive pressure in said space with respect to said surrounding atmosphere so as to reduce the accumulation of moisture within said space;

a heating system that provides heat to said space between said front surface of said antenna and said cover so as to maintain said cover at a temperature sufficient to reduce accumulations of frozen precipitation on said cover;

a sensing system which senses the temperature and the presence of moisture of the atmosphere surrounding said satellite antenna; and

a controller which receives signals from said sensing system wherein said controller activates said air supply system upon said sensing system detecting the presence of a preselected quantity of moisture and wherein said controller activates said heating system upon detecting that said temperature of said atmosphere surrounding said satellite antenna is in a predetermined range of temperatures.

2. The system of claim 1, wherein said controller initiates said heating system upon said sensing system detecting that the temperature of atmosphere surrounding said satellite antenna is within said predetermined temperature range and wherein said predetermined temperature range has been selected to define a range wherein frozen precipitation will adhere to said cover.

3. The system of claim 2, wherein said predetermined temperature range is approximately 24°

-38°

F.

4. The system of claim 1, wherein said controller activates said air supply system upon detecting the presence of moisture in said preselected quantity so that a positive air pressure is induced in said space between said cover and said front reflecting surface of said antenna so as to reduce the likelihood of moisture entering said space.

5. The system of claim 4, wherein said cover is flexible and, when said air supply system is activated, said cover has a convex shape with respect to the outer surface of said front reflecting surface of said antenna and wherein said convex shape of said cover aids in the shedding of frozen precipitation from said cover.

6. The system of claim 1, wherein said heater system is activated only when both said sensing system detects the presence of moisture and also detects that the temperature of the atmosphere is within said predetermined temperature range at the time the presence of moisture is detected.

7. The system of claim 6, wherein said controller continues to induce said heating system to supply heat to said space when the temperature of the atmosphere drops from the temperature at the time moisture was detected to a temperature below said predetermined range.

8. A system for reducing accumulation of moisture on a front reflecting surface of a satellite antenna having an outer lip comprising:

a flexible cover having an opening which is dimensioned to mount on said outer lip of said antenna with the cover positioned over said front reflecting surface of said satellite antenna so as to define a space between said front reflecting surface of said antenna and said cover whereby said cover reduces accumulations of frozen precipitation on said front reflecting surface of said satellite antenna while permitting satellite signals to pass therethrough;

an air supply system which provides unheated air to said space between said cover and said from reflecting surface so as to induce positive pressure in said space with respect to said surrounding atmosphere so as to reduce accumulations of moisture in said space and so that said flexible cover deforms outward from the lip of the antenna so as to form a convex shape which facilitates in the shedding of moisture from said cover;

a heating system that provides heat to said space between said front surface of said antenna and said cover so as to maintain said cover at a temperature sufficient to reduce accumulations of frozen precipitation on said cover;

a sensing system which senses the temperature and the presence of moisture of the atmosphere surrounding said satellite antenna;

a controller which receives signals from said sensing system wherein said controller activates said air supply system upon said sensing system detecting the presence of moisture and wherein said controller activates said heating system upon detecting both the presence of moisture and that the temperature of the atmosphere surrounding said satellite antenna is in a predetermined range of temperatures at the time moisture was detected.

9. The system of claim 8, wherein said controller activates said heating system upon said sensing system detecting that the temperature of the atmosphere surrounding said satellite antenna with said predetermined range wherein said predetermined temperature range has been selected so as to define said range wherein frozen precipitation adheres to said cover.

10. The system of claim 9, wherein said predetermined temperature range is approximately 24°

-38°

F.

11. The system of claim 8, wherein said controller activates said air supply system upon detecting the presence of moisture so that a positive air pressure is induced in said space between said cover and said front reflecting surface of said antenna so as to reduce the likelihood of moisture entering said space.

12. The system of claim 11, wherein said cover is flexible and when said air supply system is activated, said cover has a convex shape with respect to the outer surface of said front reflecting surface of said antenna and wherein said convex shape of said cover aids in the shedding of frozen precipitation from said cover.

13. A method of preventing frozen precipitation from interrupting communications with a ground based satellite antenna comprising the steps of:

positioning a flexible cover on a lip of the antenna on a front concave side of said satellite antenna so as to define an enclosed space between said cover and a front reflecting surface of said antenna so as to reduce accumulations of frozen precipitation on said concave surface of said antenna while permitting satellite signals to pass therethrough;

sensing the presence or absence of moisture in the atmosphere surrounding said satellite antenna;

sensing the temperature of the atmosphere surrounding said satellite antenna;

supplying unheated air to said space between said cover and said front reflecting surface of said antenna so as to induce a positive air pressure within said space with respect to said atmosphere upon detecting the presence of a predetermined quantity of moisture in said atmosphere; and

supplying heat to said space between said cover and said front reflecting surface upon detecting that the temperature of said atmosphere is within a predetermined temperature range.

14. The method of claim 13, wherein heat is supplied when said temperature of said atmosphere is within a predetermined range of temperatures wherein frozen precipitation is likely to adhere to said cover.

15. The method of claim 13, wherein air is supplied to said space when moisture in said atmosphere is sensed in a quantity wherein precipitation is likely to be deposited on said cover.

16. The method of claim 14, wherein heat is supplied when said temperature of said atmosphere is in the approximate range of 24°

-38°

F.

17. The method of claim 13, wherein heat is supplied to said space only upon detecting that both said temperature of said atmosphere is within said range and also that a predetermined quantity is moisture is present within said atmosphere.

18. The method of claim 17, further comprising the steps of:

continuing to sense the presence and absence of moisture while said air supply system is operating; and

disabling said air supply system when said predetermined quantity of moisture is no longer present in said atmosphere.

19. The method of claim 18, further comprising the steps of:

continuing to sense the temperature of said atmosphere while said heating system is operating;

disabling said heating system when said temperature of said atmosphere increases to above said predetermined range; and

continuing to operate said heating system when said temperature falls below said range when moisture is present in said atmosphere in said predetermined quantity.