US 4,377,266 AGranted

Electrical rotary joint apparatus for large space structures

AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration

InventorsRobert R. Belew, Richard J. Boehme

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Abstract

A structural array and electrical rotary joint for transmitting an electrical power between large space structures having relative rotational movement therebetween is disclosed as including large support framework structures A and B which rotate relative to one another about a common axis of rotation X. A rotary interface joint 14 is defined between the structures A and B. A cylindrical hub member C is carried by the structure A and a cylindrical hub member is carried by support structure B with hub member C being received concentrically within hub member D for relative rotation. Tension connecting cables connect hub member C and hub member D with their associated outer structures A and B whereby relative rotational movement between structures A and B is transmitted to the cylindrical hub members for unitary motion therewith. Electrical conductor brush members 18 are carried by the hub D and electrical contact rings 16 are carried by the hub member C in sliding electrical contact with the brushes for transmission of electrical power during relative rotational movement between the support structures A and B.

Claims7

Dependent claims

A structural array and electrical rotary joint apparatus for use in space structures and the like for transmitting power between large structures having relative rotational movement between each other comprising:

a first large structure having a supportive framework;
a second large structure having a supportive framework;
said first and second large structures being arranged for rotational movement relative to one another coaxially about a common axis of rotation;
a rotary interface defined at a rotary joint between said first and second structures;
a first cylindrical hub member carried centrally by said first structure;
a second cylindrical hub member carried centrally by said second structure;
connecting means connecting said first and second cylindrical hub members with said respective first and second structures in a generally rigid unitary manner whereby said relative rotational movement is transmitted from said first and second structures to said first and second cylindrical members, respectively;
said first and second cylindrical hub members being carried in a concentric relation with respect to one another;
first electrical conductor means carried by said first cylindrical hub member;
second electrical conductor means carried by said second cylindrical hub member, said first and second conductor means being carried in relative sliding contact for transmission of electrical power therebetween during said relative rotational movement;
a bearing support assembly rotatably connected between said first and second cylindrical members for connecting said cylindrical members and respective first and second structures during rotation and accommodating radial and axial loads on and between said cylindrical members;
said bearing assembly including a roller track carried by said first cylindrical member, a radial thrust roller rotatably carried by said second cylindrical member bearing against the outer cylindrical surface of said roller track acting against said radial loads, and a pair of axial thrust rollers rotatably carried by said second cylindrical member engaging sides of said roller track accommodating said axial loads;
and
drive means connected between framework of said first and second structures at an outer periphery of said rotary interface joint for rotating one of said structures relative to the other producing said relative rotational movement said drive means including means for interconnecting said first and second structures together as an integral structure as well as rotating said one structure.

11 more elements

A space structure for transmitting power in space which comprises:

a first space frame structure which carries a plurality of solar panels, having a first rotary hexagonal frame interface;
a second space frame structure which carries associated power equipment having a second rotary hexagonal frame interface;
said first and second rotary hexagonal frame interfaces providing a rotary joint between said first and second frame structures about which said structures rotate relative to one another about a common axis of rotation;
a first rotary hub member carried by said first structure at said rotary interface;
a second rotary hub member carried by said second frame structure at said rotary interface;
said first and second rotary hub members being concentric with one another with said first and second frame structures joined together at said rotary interfaces;
tension connecting means connecting said rotary hub members to said associated space frame structures such that each rotary hub member is connected to its associated space frame structure in a generally rigid unitary manner so that said rotary hub members move as a unit with the space frame structure to which it is connected;
said tension members being connected between said rotary hub members and structural node points of said hexagonal frame interface of each space frame structure;
an electrical rotary joint including a first electrical conductive surface carried by one of said rotary hub members and a second electrical conductive surface carried by the other of said rotary hub members, said conductive surfaces being in slidable electrical contact with one another for transferring electrical power from said solar panels carried on said first space frame structure to said associated power equipment carried on said second space frame structure;
a bearing support assembly connected between said first and second rotary hub members for accommodating radial and axial loads exerted on and between said rotary hub members due to the rotation of said first and second frame structures, said bearing support assembly including a circular track carried about the periphery of one of said rotary hub members and a plurality of wheel assemblies carried by the other of said rotary hub members, said wheel assemblies including a pair of rollers engaging vertical surfaces of said track and at least one roller engaging a horizontal surface of said track affording resistence against axial and radial forces acting on said rotary hub members;
and
a roller drive assembly connected between said first and second frame structures at an outer periphery of said rotary hexagonal frame interfaces for rotating one of said space frame structures relative to the other, said drive assembly including a track member carried by one of said space frame structures at said outer periphery having converging sides converging towards said frame structure and a drive surface bridging said converging sides at divergent ends thereof, a pair of interconnecting rollers engaging said converging sides to interconnect said space frame structure, and a driven roller in engagement with said drive surface to drive said driven space frame structure relative to said other space frame structure.

9 more elements

Dependencies are inferred from the claim text.