IP Library Granted Patent US 11,888,228
Granted Patent B2
US 11,888,228 · App. 17/943,895 · Granted Jan 30, 2024

Prism for repointing reflector antenna main beam

Inventors: Jeremiah P. Turpin (Linthicum, MD); John Finney (London, GB)
Assignee: All.Space Networks Limited
H01Q19/132H01Q1/247H01Q3/08H01Q3/20H01Q5/55H01Q15/04H01Q15/16H01Q19/191H04B7/18517
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Quick Facts
Patent No.
US 11,888,228
App. No.
17/943,895
Granted
Jan 30, 2024
Kind
B2
Abstract

A microwave prism is used to repoint an operational Direct-to-Home (DTH) or Very Small Aperture Terminal (VSAT) reflector antenna as part of a ground terminal to receive (or transmit) signals from a different satellite or orbital position without physically moving the reflector or the feed horn antenna. The microwave prism operates by shifting the radiated fields from the horn antenna generally perpendicular to the focal axis of the parabolic reflector in order to cause the main beam of the reflector to scan in response. For an existing reflector antenna receiving signals from an incumbent satellite, a prism has been designed to be snapped into place over the feed horn and shift the fields laterally by a calibrated distance. The structure of the prism is designed to be positioned and oriented correctly without the use of skilled labor. This system allows a satellite service provider to repoint their subscribers to a new satellite by shipping a self-install kit of the prism that is pre-configured to have the correct orientation and position on the feed antenna to correctly re-point the beam at a different satellite once the prism is applied. One benefit of the system is that unskilled labor, i.e., the subscribers themselves, can be used to repoint a large number of subscriber antennas in a satellite network rather than requiring the cost of a truck roll and a technician to visit every site. The microwave prisms to implement this functionality can be constructed in different ways, with homogeneous slabs or blocks, Gradient-Index (GRIN), multi-layered dielectric, geometric or graded-index Fresnel-zone, metasurface, or metamaterial prisms. The geometric and electrical constraints of the design are determined by the incumbent and target satellites, and the ground terminal location.

Claims (28)

1. A prism assembly comprising:

a prism arranged between a horn antenna and a reflector;

a mounting structure configured to moveably connect the prism to the horn antenna; and

two or more alignment features configured to indicate a corresponding position and orientation of the connected prism relative to the horn antenna, wherein the position and orientation of the prism indicated by each of the two or more alignment features has a corresponding effect on a beam from the horn antenna directed to the reflector, and the position and orientation of the prism is selectably adjusted to align with one of the two or more alignment features.

2. The assembly of claim 1 , wherein the horn antenna comprises a horn feed that outputs the main beam.

3. The assembly of claim 1 , wherein the prism redirects the main beam from a first satellite to a second satellite.

4. The assembly of claim 1 , wherein the prism is a parallel-plate prism.

5. The assembly of claim 1 , wherein the prism includes one or more layers of metamaterial.

6. The assembly of claim 1 , wherein the prism includes a graded-index structure.

7. The assembly of claim 1 , wherein the prism is substantially enclosed by a radome.

8. A system for repointing a main beam of a reflector antenna, comprising:

a prism configured to receive the main beam from a horn antenna and the prism configured to laterally shift the main beam from the horn antenna in a direction that is perpendicular to an axis of symmetry of a reflector that is parabolic, and to direct the laterally shifted main beam to the reflector; and

a mounting structure configured to connect the prism to the horn antenna.

9. The system of claim 8 , wherein the mounting structure releasably connects to the horn antenna.

10. The system of claim 8 , wherein the prism is configured to repoint the main beam from a first satellite to a second satellite.

11. The system of claim 8 , further comprising:

one or more alignment features configured to set a position of the prism and an orientation of the prism.

12. The system of claim 11 , wherein the one or more alignment features are adjustable.

13. A method for repointing a main beam of a reflector antenna, the method comprising:

determining an output direction of the main beam from a horn antenna and determining an exit point of the main beam from the horn antenna;

positioning a prism at the exit point to receive the main beam; and

mounting the prism on the horn antenna to shift the main beam, between the exit point from the horn antenna to an output of the prism directed to a reflector, laterally in a direction that is substantially perpendicular to an axis of symmetry of the reflector.

14. The method of claim 13 , further comprising:

one or more alignment features configured to set a position of the prism and an orientation of the prism.

15. The method of claim 14 , wherein the one or more alignment features are adjustable.

16. The method of claim 13 , wherein the prism is a parallel-plate prism.

17. The method of claim 13 , wherein the parallel-plate prism comprises a plurality of wedges.

18. The method of claim 13 , wherein the prism is substantially enclosed by a radome.

Assignments (3)
SECURITY INTEREST Recorded Oct 21, 2025
From: ALL.SPACE NETWORKS LIMITED
To: ACQUIOM AGENCY SERVICES LLC
Reel/Frame 072615/0927 →
CHANGE OF NAME Recorded Mar 28, 2023
From: ISOTROPIC SYSTEMS LTD
To: ALL.SPACE NETWORKS LIMITED
Reel/Frame 063125/0675 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 27, 2023
From: TURPIN, JEREMIAH P.; FINNEY, JOHN
To: ISOTROPIC SYSTEMS LTD
Reel/Frame 063104/0876 →
Continuity (3)
Continuation 17182992 · Feb 23, 2021
Provisional Application 62981367 · Feb 25, 2020
Related Publication 20230006358A1 · Jan 5, 2023