Waveguide hinge
View Patent ↗Waveguide hinges are provided that allow for a substantially continuous RF waveguide to be formed through the hinge when the hinge elements are in a particular relative rotational configuration with respect to one another; the substantially continuous RF waveguide is not formed when the hinge elements are in various other relative rotational configurations. Such waveguide hinges allow for waveguide elements to be repositioned during periods when RF energy is not being transmitted.
1. An apparatus, the apparatus comprising:
a first member;
a second member;
a first radio-frequency (RF) waveguide portion located within the first member; and
a second RF waveguide portion located within the second member, wherein:
the first member and the second member are rotatably coupled with one another relative to a rotational axis, thereby forming a hinge, and are transitionable between a first relative rotational configuration and a second relative rotational configuration,
in the first relative rotational configuration, the first RF waveguide portion and the second RF waveguide portion are aligned with one another to form a substantially continuous first waveguide through the first member and the second member, and
in the second relative rotational configuration, the first RF waveguide portion and the second RF waveguide portion are not aligned with one another to form the substantially continuous first waveguide through the first member and the second member.
2. The apparatus of claim 1 , wherein:
the first RF waveguide portion enters the first member along a direction substantially parallel to a first axis that is perpendicular to the rotational axis, and
the second RF waveguide portion exits the second member along a direction substantially parallel to a second axis that is also perpendicular to the rotational axis.
3. The apparatus of claim 1 , wherein:
the first RF waveguide portion enters the first member along a direction substantially parallel to a first axis that is perpendicular to the rotational axis, and
the second RF waveguide portion exits the second member along a direction substantially parallel to the rotational axis.
4. The apparatus of claim 1 , wherein the first RF waveguide portion enters the first member and the second RF waveguide portion enters the second member along directions substantially parallel to the rotational axis.
5. The apparatus of claim 1 , further comprising:
a third RF waveguide portion located in the first member; and
a fourth RF waveguide portion located in the second member, wherein:
the third RF waveguide portion and the fourth RF waveguide portion are aligned with one another to form a substantially continuous second waveguide through the first member and the second member when the first member and the second member are in the first relative rotational configuration, and
the third RF waveguide portion and the fourth RF waveguide portion are not aligned with one another to form the substantially continuous second waveguide through the first member and the second member when the first member and the second member are in the second relative rotational configuration.
6. The apparatus of claim 5 , wherein:
the first RF waveguide portion and the third RF waveguide portion enter the first member along directions substantially parallel to a first axis that is perpendicular to the rotational axis, and
the second RF waveguide portion and the fourth RF waveguide portion exit the second member along directions substantially parallel to a second axis that is also perpendicular to the rotational axis.
7. The apparatus of claim 5 , wherein:
the first RF waveguide portion and the third RF waveguide portion enter the first member along directions substantially parallel to a first axis that is perpendicular to the rotational axis,
the second RF waveguide portion exits the second member along a direction that is substantially parallel to the rotational axis, and
the fourth RF waveguide portion exits the second member along a direction substantially parallel to a second axis that is perpendicular to the rotational axis.
8. The apparatus of claim 1 , further comprising a positive locking mechanism that locks when the first member and the second member are transitioned into the first relative rotational configuration and that prevents the first member and the second member from rotating relative to one another when locked.
9. The apparatus of claim 1 , further comprising a drive mechanism, wherein the drive mechanism is configured to cause the apparatus to move from the second relative rotational configuration to the first relative rotational configuration.
10. The apparatus of claim 9 , wherein the drive mechanism is an item selected from the group consisting of: a torsion spring, a linear spring, and a motor.
11. The apparatus of claim 1 , wherein:
in the first relative rotational configuration, the first RF waveguide portion and the second RF waveguide portion provide a first path for RF energy, and
the first RF waveguide portion and the second RF waveguide portion both have rectangular cross-sections in planes perpendicular to the first path that are substantially the same.
12. The apparatus of claim 11 , wherein the rectangular cross-sections have an aspect ratio of between 1.8:1 and 2.2:1.
13. The apparatus of claim 1 , further comprising:
a plurality of first RF waveguide portions located in the first member, wherein the plurality of first RF waveguide portions includes the first RF waveguide portion; and
a plurality of second RF waveguide portions located in the second member, wherein the plurality of second RF waveguide portions includes the second RF waveguide portion, wherein:
each of the second RF waveguide portions corresponds to a corresponding one of the first RF waveguide portions,
in the first relative rotational configuration, each of the first RF waveguide portions and each of the corresponding second RF waveguide portions are aligned with one another to form a corresponding substantially continuous waveguide through the first member and the second member, and
in the second relative rotational configuration, each of the first RF waveguide portions and each of the second RF waveguide portions are not aligned with one another to form the corresponding substantially continuous waveguide through the first member and the second member.
14. The apparatus of claim 13 , wherein:
one or more of the first RF waveguide portions enters the first member along a direction substantially parallel to a first axis that is perpendicular to the rotational axis, and
one or more of the second RF waveguide portions exits the second member along a direction substantially perpendicular to a second axis that is also perpendicular to the rotational axis.
15. The apparatus of claim 13 , wherein:
one or more of the first RF waveguide portions enters the first member along a direction substantially parallel to a first axis that is perpendicular to the rotational axis, and
one or more of the second RF waveguide portions exits the second member along a direction substantially parallel to the rotational axis.
16. The apparatus of claim 13 , wherein one or more of the first RF waveguide portions enters the first member and one or more of the second RF waveguide portions exits the second member along a directions substantially parallel to the rotational axis.
17. The apparatus of claim 13 , wherein:
one or more of the first RF waveguide portions enters the first member along a direction substantially parallel to a first axis that is perpendicular to the rotational axis,
one or more of the second RF waveguide portions exits the second member along a direction substantially parallel to a second axis that is also perpendicular to the rotational axis, and
one or more of the second RF waveguide portions exits the second member along a direction substantially parallel to the rotational axis.
18. The apparatus of claim 1 , further comprising:
a deployable boom having a distal end and a proximal end;
a boom RF waveguide; and
a spacecraft main body having a main body RF source, wherein:
the proximal end of the deployable boom is connected with the second member and the boom RF waveguide is coupled with the second RF waveguide portion,
the boom RF waveguide extends from the proximal end of the deployable boom towards the distal end of the deployable boom,
the spacecraft main body is connected with the first member and the main body RF source is coupled with the first RF waveguide portion, and
the first member and the second member are configured to allow the deployable boom to be rotated about the rotational axis from a stowed configuration to a deployed configuration, wherein the first member and the second member are in the first relative rotational configuration in the deployed configuration and in the second relative rotational configuration in the stowed configuration.
19. The apparatus of claim 1 , further comprising a first RF routing panel and a spacecraft main body, wherein:
the first RF routing panel is mounted on or within the main body,
the hinge formed by the first member and the second member is configured to allow the first RF routing panel to be rotated relative to the main body,
in the first relative rotational configuration, the first RF routing panel is in a configuration in which RF components mounted to the first RF routing panel are operable to route RF power and the first waveguide is configured to route RF power from or to a first RF component of the RF components mounted to the first RF routing panel,
the first RF component is connected to the first member, and
in the second relative rotational configuration, the first RF routing panel is in a configuration in which the first waveguide is not operable to route RF power from or to the first RF component.
20. The apparatus of claim 19 , further comprising a second RF routing panel having additional RF components mounted thereon, wherein:
a second RF component of the additional RF components is connected with the second member,
when the first member and the second member are in the first relative rotational configuration:
the first waveguide is configured to route RF power between the first RF component and the second RF component, and
the first RF routing panel and the second RF routing panel are substantially parallel to one another, and
when the first member and the second member are in the second relative rotational configuration:
the first RF routing panel and the second RF routing panel are at a substantial angle to one another, and
the first waveguide is not configured to route RF power between the first RF component and the second RF component.
21. An apparatus comprising;
a rotary microwave coupling, the rotary microwave coupling including a stator having (a) a first waveguide port and (b) a rotor having a rigid waveguide channel, a distal end of the rigid waveguide channel forming a second waveguide port, wherein the first waveguide port, the waveguide channel, and the second waveguide port are generally disposed in a common plane;
a first waveguide coupled with the first waveguide port; and
a second waveguide coupled with the second waveguide port, wherein:
rotation of the rotor results in rotation of the second waveguide with respect to the first waveguide about an axis perpendicular to the common plane,
the apparatus is transitionable between a first configuration and a second configuration through rotation of the rotor,
a proximal end of the rigid waveguide channel is, in the first configuration, aligned with the first waveguide port such that the first waveguide, the first waveguide port, the rigid waveguide channel, the second waveguide port, and the second waveguide form a substantially continuous waveguide through the rotary microwave coupling, and
the proximal end of the rigid waveguide channel is, in the second configuration, misaligned with the first waveguide port such that the first waveguide, the first waveguide port, the rigid waveguide channel, the second waveguide port, and the second waveguide do not form the substantially continuous waveguide through the rotary microwave coupling.
22. The apparatus of claim 21 , wherein,
in the second configuration, the proximal end of the rigid waveguide channel is disposed at a substantial angular offset about the axis from the first waveguide port.