Securing ring and assemblies

1. A securing apparatus comprising:

a curvilinear body defining an opening and having a gap that defines confronting ring ends that are separable to receive at least one curvilinear device within the opening, the curvilinear body including an outer surface and opposing first and second side walls that define a slot therebetween, wherein the slot is configured for receiving the curvilinear device, and wherein the outer surface, the first wall and the second wall provide a clamping force on the curvilinear device in the slot when the confronting ring ends are drawn together, the clamping force securing the curvilinear device within the slot; and

a locking mechanism coupled to the confronting ring ends and configured to releasably engage the confronting ring ends to secure the confronting ring ends together;

wherein the curvilinear device comprises a satellite antenna reflector.

2. The securing apparatus of claim 1 , wherein the slot has an inside diameter equal to or greater than an outside diameter of the curvilinear device to prevent distortion thereof.

3. The securing apparatus of claim 1 , wherein the locking mechanism is configured to provide an adjustable clamping force depending on a shape of the at least one curvilinear device.

4. The securing apparatus of claim 3 , wherein the locking mechanism comprises:

a first threaded hole coupled to a first of the confronting ring ends;

a second threaded hole coupled to a second of the confronting ring ends and positioned to confront the first threaded hole; and

a screw that engages both the first threaded hole and the second threaded hole to secure the confronting ring ends together.

5. The securing apparatus of claim 1 , wherein the locking mechanism comprises a pivoted tension lever.

6. The securing apparatus of claim 1 , wherein the first wall engages a back surface of the satellite antenna reflector and the second wall engages a front surface of a satellite antenna reflector cover.

7. The securing apparatus of claim 6 , wherein the second wall comprises a knurled pattern that matingly engages the satellite antenna reflector cover.

8. The securing apparatus of claim 6 , wherein a distance between the first wall and the second wall is sized based upon a total thickness of the satellite antenna reflector and the satellite reflector cover when the satellite reflector cover engages a front surface of the satellite antenna reflector.

9. An assembly comprising:

a satellite antenna reflector having a concave cross sectional shape, an outside diameter and a first thickness;

a satellite reflector cover configured to cover the reflector having a second thickness;

a securing ring configured to attach the cover to the reflector that comprises opposing segments separated by a gap, an opening diameter that is less than the outside diameter of the reflector, and a slot around the opening having an inside diameter corresponding to the outside diameter of the reflector and a width corresponding to the first thickness and the second thickness combined;

a locking mechanism attached to the ring operable to close the gap and secure the reflector to the cover; and

the ring movable to an open position wherein the gap is formed for assembling the cover on the reflector or to a closed position wherein the gap is closed for attaching the cover to the reflector with a clamping force exerted on the ring.

10. The assembly of claim 9 , wherein the opposing segments comprises a unitary body.

11. The assembly of claim 9 , wherein the opposing segments are coupled by a hinge.

12. The assembly of claim 9 , wherein the outside diameter of the reflector and the opening in the ring are substantially circular.

13. The assembly of claim 9 , wherein the outside diameter of the reflector and the opening in the ring are substantially elliptical.

14. The assembly of claim 9 , wherein the locking mechanism comprises a pivoted tension lever.

15. The assembly of claim 9 , wherein the locking mechanism is configured to provide a first clamping force if the satellite antenna reflector has a circular shape, and wherein the locking mechanism is configured to provide a second clamping force if the satellite antenna reflector has an elliptical shape.

16. The assembly of claim 15 , wherein the locking mechanism comprises:

a first threaded hole coupled to a first of the confronting ring ends;

a second threaded hole coupled to a second of the confronting ring ends and positioned to confront the first threaded hole; and

a screw that engages both the first threaded hole and the second threaded hole to secure the confronting ring ends together.

17. The securing apparatus of claim 9 , wherein the second wall comprises a knurled pattern that matingly engages the satellite antenna reflector cover.

18. A securing apparatus comprising:

a curvilinear body having at least two segments coupled together by a hinge, the at least two segments defining an opening and having a gap that defines confronting ring ends of the segments that are separable to receive at least one curvilinear device within the opening, the curvilinear body including an outer surface and opposing first and second side walls that define a slot therebetween, wherein the slot is configured for receiving the curvilinear device, and wherein the outer surface, the first wall and the second wall provide a clamping force on the curvilinear device in the slot when the confronting ring ends are drawn together, the clamping force securing the curvilinear device within the slot; and

a locking mechanism coupled to the, confronting ring ends and configured to releasably engage the confronting ring ends to secure the confronting ring ends together;

wherein the curvilinear device comprises a satellite antenna reflector.

19. The securing ring of claim 18 , wherein the locking mechanism comprises a pivoted tension lever.