Modular supertile array antenna

• US 5,666,128 A
• Filed: 03/26/1996
• Issued: 09/09/1997
• Est. Priority Date: 03/26/1996
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Foley, James Paul, Stuart, Thomas MacKenzie, Weiss, Fred Manfred, Murray, Bronson
• Primary Examiner(s): Hajec, Donald T.
• Assistant Examiner(s): PHAN, THO GIA
• Application Number:
  US08/622,725
• Time in Patent Office: 532 Days
• Field of Search: 343/878, 343/879, 343/700 MS, 343/705, 343/725, 343/880, 343/881, 343/915, 343/DIG. 2
• US Class Current: 343/878
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 21/0087 Apparatus or processes specially adapted for manufacturing antenna arrays manufacturing waveguides H01P11/00
• CPC Class Codes: Y10S 343/02 Satellite-mounted antenna

Abstract

An array antenna especially adapted for spacecraft use includes a support frame made up of intersecting beams which form an "eggcrate" of square openings. A plurality of subarrays or radiating tiles are dimensioned to fit within the openings. Distortion of the support frame due to external forces, or due to expansion and contraction of the radiating tiles, is accommodated andor resisted by a four-point mounting arrangement for each tile. Each mounting is located on the center of the sides of the radiating tile, and the corresponding center of the side of the opening in which it fits. Each mounting consists of a thin, flexible mounting beam, extending parallel to the associated support beam, and fastened to the support beam at the ends of the mounting beam. The center of the side of the tile is fastened to the center of the flexible support beam, so expansion and contraction of the tile are compensated by bending of the flexible beam. Mutually opposing external forces acting parallel to the elements of the support frame are resisted by the longitudinal stiffness of the flexible beam and the diagonal stiffness of the tile.

Claims

1. An array antenna, comprising:

a frame including a plurality of straight, elongated support beams, interconnected in two mutually orthogonal sets so as to, together, define a rectangular two-dimensional array of a first plurality of mutually identical rectangular openings, said frame being subject to distortion in response to forces acting on said frame parallel to said support beams;

a second plurality, which is no greater than said first plurality, of rectangular, electromagnetically radiating tiles, each of said radiating tiles having length and width dimensions selected to fit within said openings, and having a thickness dimension much less than either of said length and width dimensions;

mounting means affixed to each of said tiles and to the associated ones of said openings in said frame, for holding each tile in an associated opening of said frame, each of said mounting means including four mounts, each of said mounts being affixed to the center of one of the sides of the associated one of said radiating tiles and to the center of one of said support beams defining an edge of said associated one of said openings, each of said mounts including (a) an elongated flex beam defining a thickness dimension, a width dimension greater than said thickness dimension, and a length dimension greater than said width dimension, (b) spacing means coupled to said flex beam and to said associated one of said support beams, whereby the center of said flex beam may deflect toward and away from the center of said associated one of said support beams, and (c) further connection means connecting the associated side of said radiating tile to said flex beam, whereby expansion and contraction of said radiating tile cause said center of said flex beams to deflect toward and away from, respectively, their associated support beams, whereby each of said radiating tiles remains centered in its associated opening, and whereby the combination of said four mounts, and the longitudinal stiffness provided by said flex beam, together with the stiffness of said radiating tile along its diagonals, provides triangle-like support of said rectangular opening, to enhance the structural strength of said frame against forces directed parallel with said support beams.

2. An antenna according to claim 1, wherein said spacing means coupled to said flex beam and to said associated one of said support beams comprises a pair of spacers, each of which is affixed to an end of its associated flex beam and to the side of said associated one of said support beams.

3. An antenna according to claim 2, wherein said support beam includes a web and a flange, and said pair of spacers is affixed to said web.

4. An antenna according to claim 1, wherein each of said radiating tiles includes an array of radiating elements.

5. An antenna according to claim 1, wherein said rectangular openings are square, and said radiating tiles are square.

6. An antenna according to claim 1, wherein at least one of said radiating tiles of said array operates in a first frequency range, and another of said radiating tiles operates in a second frequency range, different from said first frequency range.

7. An antenna according to claim 6, wherein a plurality of said radiating tiles of said array radiate in said first frequency range, and a plurality of said radiating tiles of said array radiate in said second frequency range.

8. An antenna according to claim 1, wherein said frame lies essentially in a plane, and the plane of said tile is parallel to said plane of said frame.

9. An array antenna according to claim 1, wherein

said spacing means comprises first and second spacers coupled to the ends of said flex beam and to said associated one of said support beams, whereby a center portion of said flex beam is not supported by a spacer, and may deflect toward and away from the associated one of said support beams;

and

said further connection means connecting the associated side of said radiating tile to said flex beam comprises means for connecting the center portion of said associated side of said radiating tile to said center portion of said flex beam.

10. A spacecraft, comprising:

a plurality of array antennas, each of said array antennas comprising;

a frame including a plurality of straight, elongated support beams, interconnected in two mutually orthogonal sets so as to, together, define a rectangular two-dimensional array of a first plurality of mutually identical rectangular openings, said frame being subject to distortion in response to forces acting on said frame;

a second plurality, which is no greater than said first plurality, of rectangular, electromagnetically radiating tiles, each of said radiating tiles having length and width dimensions selected to fit within said openings, and having a thickness dimension much less than either of said length and width dimensions;

mounting means affixed to each of said tiles and to the associated ones of said openings in said frame, for holding each tile in an associated opening of said frame, each of said mounting means including four mounts, each of said mounts being affixed to the center of one of the sides of the associated one of said radiating tiles and to the center of one of said support beams defining an edge of said associated one of said openings, each of said mounts including (a) an elongated flex beam defining a thickness dimension, a width dimension greater than said thickness dimension, and a length dimension greater than said width dimension, (b) a pair of spacers, each of which is affixed to an end of its associated flex beam and to the side of said associated one of said support beams, whereby the center of said flex beam may deflect toward and away from the center of said associated one of said support beams, and (c) further connection means connecting the center of the associated side of said radiating tile to the center of said flex beam, whereby expansion and contraction of said radiating tile cause said center of said flex beams to deflect toward and away from, respectively, their associated support beams, whereby each of said radiating tiles remains centered in its associated opening, and whereby the combination of said four mounts, and the longitudinal stiffness provided by said flex beam, together with the stiffness of said radiating tile along its diagonals, provides triangle-like support of said rectangular opening, to enhance the structural strength of said frame.