Foldable antenna for reconfigurable radar system

• US 8,446,326 B2
• Filed: 04/25/2008
• Issued: 05/21/2013
• Est. Priority Date: 04/25/2008
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Tietjen, Byron W.
• Primary Examiner(s): Wimer, Michael C
• Application Number:
  US12/109,874
• Publication Number:
  US 20090267835A1
• Time in Patent Office: 1,852 Days
• Field of Search: 343/700.MS, 343/757, 343/880, 343/881, 343/882, 343/792.5, 343/758
• US Class Current: 343/757
• CPC Class Codes: H01Q 1/084 Pivotable antennas
• CPC Class Codes: H01Q 1/3233 particular used as part of a sensor or in a security system, e.g. for automotive radar, navigation systems
• CPC Class Codes: H01Q 3/02 using mechanical movement of antenna or antenna system as a whole
• CPC Class Codes: H01Q 9/12 adapted for adjustment of angle between elements

Abstract

The invention provides for phased array radar system that mechanically reconfigures its antenna array from a single faced aperture into two geometrically opposed arrays.

Claims

1. A reconfigurable phased array radar system, comprising:

a base,

a plurality of antenna radiating elements positioned on a foldable frame in a main array, said main array having a given aperture when said frame is positioned in a single plane,

an assembly positioned on said frame to mechanically fold and separate into a first frame portion having a first plurality of said elements thereon defining a first sub-array and a second frame portion having a second plurality of said elements thereon defining a second sub-array, said first frame portion rotatably connected to said base via a coupling and provides a first aperture less than said given aperture to enable antenna radiation in a first direction and said second frame portion provides a second aperture also less than said given aperture to enable radiation in a second direction, and

wherein rotating said first frame portion with respect to said base via said coupling in a first mode, causes the elevation angle of the main array to be altered with respect to said base while maintaining said frame in a single plane, and in a second mode, causes said frame to be folded and separated into said first frame portion and said second frame portion.

2. The reconfigurable phased array radar system according to claim 1, wherein,

said first and second pluralities of antenna elements are equal in number with each plurality being one half of said given plurality, with said first and second apertures being one-half of said given aperture.

3. The reconfigurable phased array radar system according to claim 1, wherein said assembly comprises a hinge member positioned centrally on said frame to fold said frame into an inverted “

V”

shape, wherein said first and second apertures face opposite directions.

4. The reconfigurable phased array radar system according to claim 3, further including means coupled to said frame to lock said frame in said folded position.

5. The reconfigurable phased array radar system according to claim 1, wherein said first and second pluralities of antenna elements are unequal in number, providing first and second unequal antenna apertures.

6. The reconfigurable phased array radar system according to claim 1, wherein said first and second apertures are coupled to electronic means for independently steering said sub-apertures.

7. The reconfigurable phased array radar system according to claim 1, further comprising a rotating assembly coupled to said frame for rotating said foldable frame.

8. The reconfigurable phased array radar system according to claim 1, wherein said back-to-back arrays are adapted for short range target detection.

9. The reconfigurable phased array radar system according to claim 1, wherein said main array is adapted for long range target detection.

10. The reconfigurable phased array radar system according to claim 1, wherein the elevation angle of the main array may be altered between a generally vertical orientation and a generally horizontal orientation while maintaining said frame in said single plane.

11. The reconfigurable phased array radar system according to claim 1, wherein the elevation angle of the main array may be altered while maintaining said frame in said single plane by a drive assembly.

12. A reconfigurable phased array radar system comprising:

a base,

a latchably secured hinged antenna frame having a first portion pivotally connected to said base by a coupling and a second portion hingedly connected to said first portion, said frame having an assembly for varying the elevation and directional orientation of one or more array apertures contained therein and which apertures are electronically combined and independently steered for detecting one or more targets, said antenna frame operative in a first mode wherein said first and second portions are arranged as a single face antenna array aperture when said frame is positioned in a single plane, and in a second mode as a dual faced multi-aperture antenna array,

wherein the elevation angle of said antenna frame in the first mode may be altered with respect to said base by pivoting said first portion via said coupling while maintaining said frame as said single face antenna array in a single plane, and

wherein when in the second mode, pivoting said first portion via said coupling alters the orientation of said second portion with respect to said first portion.

13. The system of claim 12, wherein the at least two apertures are geometrically opposed.

14. The system of claim 12, wherein the system is rotable through 360°

degrees.

15. The system of claim 12, wherein in said second mode, said frame is operated to fold at a hinge when a latch is operated to cause said frame to be positioned in an inverted “

V”

configuration, wherein one array associated with one folded portion of said frame provides an aperture which is one half of said single faced aperture and with said other folded portion providing another aperture which is also one half of said single faced aperture.

16. A method for reconfiguring a phased array radar system, comprising the steps of:

placing a plurality of antenna elements on a frame having a hinge which enables said frame to fold,

positioning said frame in a vertical direction by pivoting said frame with respect to a base about a coupling,

energizing said elements to cause said array to emit a radiation pattern for tracking long range targets, said vertical antenna array being a full aperture array,

folding said frame about said hinge by pivoting at least a portion of said frame about said coupling to cause said frame to assume an inverted “

V”

configuration with a first plurality of said elements located on a first folded frame portion and a second plurality of elements located on a second folded frame portion,

energizing said first and second plurality of elements to cause said elements to emit at least a radiation pattern from said first folded portion and a second radiation pattern from said second folded portion for tracking short range targets.

17. The method according to claim 16, further including the step of placing said hinge on said frame relatively at the center of said frame to separate said frame into relatively equal first and second portions, each portion having the same number of antenna elements to thereby provide two geometrically opposed arrays, each of which is one half the full array aperture.

18. A reconfigurable phased array antenna system comprising:

a base,

a foldable frame pivotally attached to said base via a coupling having positioned thereon a plurality of radiating elements which when energized when said frame is not folded provide a radiation pattern with said radiating elements forming a single face aperture antenna, and

means coupled to said frame for selectively securing said foldable frame in an unfolded position, thereby forming said single face aperture, and selectively permitting folding said single face aperture into two geometrically opposed apertures, each geometrically opposed aperture smaller than said single face aperture,

wherein pivoting said frame via said coupling alters the elevation angle of said single face aperture antenna with respect to said base when said frame is secured in the unfolded position, and

wherein pivoting said frame via said coupling folds said single face aperture into said two geometrically opposed apertures when said frame is not secured in the unfolded position.

19. The reconfigurable phased array radar system according to claim 18, wherein said means includes a fold line positioned near the center of said frame to separate said frame into a first and a second portion, a hinge joining said first and second portions at said fold line to enable said frame to assume a generally inverted “

V”

configuration, one of said two geometrically opposed apertures associated with one of said first and second frame portions, and the other one of said two geometrically opposed apertures associated with the other one of said first and second frame portions.

20. The array according to claim 18, further including means coupled to said frame for rotating the same about a vertical axis.

21. A reconfigurable antenna comprising:

a base;

a radar array having a single faced aperture and a mechanical assembly coupled to said array to reconfigure said single faced aperture into two geometrically opposed apertures,

the mechanical assembly comprising;

a first frame portion pivotally attached to said base on a first end thereof, and

a second frame portion having a first end pivotally coupled to a second end of said first frame portion about a common pivoting axis and movably supported on a second end thereof by a surface of said base when said single faced aperture is configured as two geometrically opposed apertures,

wherein said single faced aperture is movable between a plurality of elevation angles with respect to said base, and wherein reconfiguring said single faced aperture into two geometrically opposed apertures alters the position of said common pivoting axis with respect to said base.

22. The reconfigurable antenna according to claim 21, wherein each geometrically opposed aperture is one half said single faced aperture in size.

23. The reconfigurable antenna according to claim 21, wherein said base comprises a planar surface along which said second end of said second frame portion is moveably supported.