Compact spacecraft antenna field aperture load coupler

• US 9,470,732 B2
• Filed: 05/08/2014
• Issued: 10/18/2016
• Est. Priority Date: 05/08/2014
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Reynolds, Robert L., Barker, James M., Kerekes, Robert Daniel, Bieti, Martin W.
• Primary Examiner(s): Purvis, Sue A
• Assistant Examiner(s): HOLECEK, PATRICK R
• Application Number:
  US14/273,329
• Publication Number:
  US 20150323581A1
• Time in Patent Office: 894 Days
• Field of Search: 343/703, 343/786
• US Class Current: 1/1
• CPC Class Codes: G01R 29/10 Radiation diagrams of antennas
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 13/02 Waveguide horns

Abstract

An apparatus, method, and system are disclosed that can be used to reduce the peak radiated flux density of a horn antenna or for testing the electronics associated with a horn antenna. A horn antenna with narrow and wide ends can have disposed within it a surrogate waveguide. The surrogate waveguide has a wide end smaller than the wide end of the horn antenna, and the wide end of surrogate waveguide extending to or beyond the wide end of the horn antenna. A mounting plate or face plate covers a portion of the wide end of the horn antenna.

Claims

1. An apparatus adapted to reduce a peak radiated flux density of a horn antenna, comprising:

a surrogate waveguide comprising;

a first section having a first end configured to be disposed within a waveguide portion of the horn antenna;

a second section having a second end configured to extend to or beyond a wide end of the horn antenna, wherein the second section of the surrogate waveguide comprises a flared aperture where the flare ends at or outside the wide end of the horn antenna and expands to a maximum cross-sectional dimension that is smaller than the largest cross-sectional dimension of the wide end of the horn antenna; and

a face plate at and inside the wide end of the horn antenna through which the surrogate waveguide passes.

2. The apparatus of claim 1, wherein the surrogate waveguide has a circular or rectangular cross-section.

3. The apparatus of claim 1, wherein the face plate is perforated outside the surrogate waveguide with at least one hole having a diameter larger than half a wavelength of energy radiated by the horn antenna.

4. The apparatus of claim 1, wherein the surrogate waveguide is composed at least in part of hard anodized aluminum.

5. The apparatus of claim 1, wherein:

the surrogate waveguide comprises an electric field probe (E-probe) directional coupler outside the horn antenna between the face plate and the second end.

6. The apparatus of claim 5, wherein the surrogate waveguide is aligned with a rotation such that the E-probe directional coupler is aligned to equally couple multiple polarizations of an electromagnetic field radiated by the horn antenna.

7. The apparatus of claim 5, wherein the E-probe directional coupler comprises:

two electric field probes spaced by an odd order quarter of a wavelength of a broadcast or received signal and aligned along a length of the surrogate waveguide; and

a 90°

hybrid coupler attached to the two electric field probes where the electric field probes comprise connectors configured to equally couple multiple polarizations of electric field.

8. The apparatus of claim 1, wherein the surrogate waveguide comprises a multimode pipe coupler inside the horn antenna between the first section and the face plate, the multimode pipe coupler comprising:

a cylindrical waveguide aligned and centered along a center axis of the surrogate waveguide; and

two rectangular waveguides aligned and adjacent to the cylindrical waveguide, and positioned on opposite sides of the cylindrical waveguide to couple equally multiple polarizations of electric field.

9. The apparatus of claim 8, wherein the surrogate waveguide is aligned with a rotation such that pipe coupler is aligned to equally couple multiple polarizations of an electromagnetic field radiated by the horn antenna.

10. The apparatus of claim 1, wherein the length of the surrogate waveguide from the first end to at least the face plate has a uniform cross-sectional shape and dimension.

11. The apparatus of claim 1, further comprising a material and a coating on an outer portion of the surrogate waveguide, wherein the material and coating on the outer portion of the surrogate waveguide is thermally emissive and electrically decoupling.

12. The apparatus of claim 1, further comprising:

a radiation absorbing surface on an actively cooled aluminum plate surrounded by a thin aluminum shroud in a field aperture load configuration, where the radiation absorbing surface is positioned facing a primary direction of energy propagation from the front of the horn antenna.

13. A system for testing electronics associated with a horn antenna, comprising:

the horn antenna having a narrow end and an wide end;

a circular surrogate waveguide inserted into the horn with a straight end and an aperture end, wherein;

the surrogate waveguide is aluminum with an anodized exterior surface;

the straight end is slip-fitted into the narrow end of the horn;

the aperture end extends to or beyond the end of the wide end of the horn;

the diameter of the surrogate waveguide is constant from the narrow end near an exit of the wide end of the horn; and

the aperture of the aperture end of the surrogate waveguide is smaller than the aperture of the horn;

a mounting plate of anodized aluminum that;

is mounted at the wide end of the horn;

supports the surrogate waveguide which runs through the center of the mounting plate;

thermally couples with the surrogate waveguide; and

contains at least one perforation outside of the surrogate waveguide with diameter large enough to be above a cutoff for a signal generated by the horn; and

a radiation absorbing surface on an actively cooled aluminum plate surrounded by a thin aluminum shroud in a field aperture load configuration, where the radiation absorbing surface is positioned facing a primary direction of energy propagation from the front of the horn.

14. The system of claim 13, wherein the surrogate waveguide comprises an E-probe directional coupler outside the horn between the mounting plate and the aperture end, and wherein the E-probe comprises a 90°

hybrid coupler.

15. The system of claim 13, wherein the surrogate waveguide comprises a multimode pipe coupler inside the horn between the straight end and the mounting plate, and the multimode pipe coupler comprises a cylindrical waveguide aligned and centered along the center axis of the surrogate waveguide with two rectangular waveguides aligned to the surrogate waveguide and positioned to equally couple multiple polarizations of electric field opposite each other and adjacent to the cylindrical waveguide.

16. A method for testing electronics associated with a horn antenna having a narrow end and a wide end, a surrogate waveguide with a straight end and an aperture end, the method comprising:

attaching the surrogate waveguide to the center of a mounting plate, wherein the shape and dimensions of the mounting plate are substantially the same as the shape and dimensions of the wide end of the horn, wherein the mounting plate comprises at least one perforation outside of the surrogate waveguide having a diameter that is above a cutoff for a signal generated by the horn;

inserting the surrogate waveguide into the horn until the straight end of the surrogate waveguide slip-fits into the narrow end of the horn;

attaching the mounting plate to the wide end of the horn; and

conducting one or more tests using a probe or directional coupler to detect or insert transmissions.

17. The method of claim 16, further comprising:

aligning the surrogate waveguide with a rotation such that a probe or directional coupler attached to the surrogate waveguide is aligned to equally couple multiple polarizations of an electromagnetic field radiated by the horn.

18. The method of claim 16, further comprising:

positioning a radiation absorbing pad in a path of radiation from the aperture end of the surrogate waveguide.

19. The method of claim 18, further comprising:

surrounding a portion of the space between the radiation absorbing pad and the aperture end of the surrogate waveguide with a conductive metal shroud in a field aperture load configuration.

20. The method of claim 16, wherein the conducting comprises sampling or inserting a first signal in a first frequency range at a first port of a hybrid directional coupler, and sampling or inserting a second signal in a second frequency range at a second port of the hybrid directional coupler.