Full aperture interleaved space duplexed beamshaped microstrip antenna system

• US 5,333,002 A
• Filed: 05/14/1993
• Issued: 07/26/1994
• Est. Priority Date: 05/14/1993
• Status: Expired due to Term

• Current Assignee: Gec-Marconi Electronics Systems Corporation
• Original Assignee: Gec-Marconi Electronics Systems Corporation
• Inventors: Schwartz, Leonard, Gans, Lawrence S.
• Primary Examiner(s): Hajec, Donald
• Assistant Examiner(s): LE, HOANGANH T
• Application Number:
  US08/062,061
• Time in Patent Office: 438 Days
• Field of Search: 343/700 MS, 343/705, 343/853, 343/737, 343/771, 343/731, 343/739, 343/893
• US Class Current: 343/700.0MS
• CPC Class Codes: H01Q 1/525 between emitting and receiving antennas
• CPC Class Codes: H01Q 25/004 providing two or four symmetrical beams for Janus application

Abstract

A full aperture interleaved space duplexed beamshaped microstrip antenna system wherein the separate transmit and receive microstrip antennas each has respective arrays of radiating patch elements. Each of the antennas is fed from a single end thereof so that each antenna creates four beams. Beam pitch angles are introduced into each antenna so as to reduce the coupling between adjacent lines to allow the gap within each connected line pair to be reduced. This gap reduction provides room for the antennas to be interleaved within a common rectangular aperture so that the separate feeds are at opposite ends of the aperture. Each antenna then utilizes the entire aperture. Isolation elements are provided between the lines of the transmit and receive antennas so as to reduce the mutual coupling therebetween and maintain the minimum required sixty dB isolation.

Claims

1. A planar microstrip antenna system for a Doppler radar navigation system of aircraft having separate arrays of radiating patch elements for the transmit and receive functions and which is compensated for temperature, frequency and overwater shifts, said antenna system filling a defined rectangular aperture having a pair of sides parallel to a defined direction of forward travel of the aircraft, said antenna system comprising:

a transmit antenna including;

a first array group including a first plurality of parallel lines of serially interconnected radiating rectangular patch elements wherein each of the first plurality of lines is parallel to the defined direction;

a second array group including a second plurality of parallel lines of serially interconnected radiating rectangular patch elements wherein each of the second plurality of lines is parallel to the defined direction, the second plurality of lines of said second array group being interleaved with the first plurality of lines of said first array group, with each of the second plurality of lines being connected at a first end to a first end of a corresponding adjacent one of said first plurality of lines; and

transmit antenna feed means for feeding said first and second array groups from the second end of each of said first and second pluralities of lines to create a pair of forwardly directed beams and a pair of rearwardly directed beams; and

a receive antenna including;

a third array group including a third plurality of parallel lines of serially interconnected radiating rectangular patch elements wherein each of the third plurality of lines is parallel to the defined direction;

a fourth array group including a fourth plurality of parallel lines of serially interconnected radiating rectangular patch elements wherein each of the fourth plurality of lines is parallel to the defined direction, the fourth plurality of lines of said fourth array group being interleaved with the third plurality of lines of said third array group, with each of the fourth plurality of lines being connected at a first end to a first end of a corresponding adjacent one of said third plurality of lines; and

receive antenna feed means for feeding said third and fourth array groups from the second end of each of said third and fourth pluralities of lines to create a pair of forwardly directed beams and a pair of rearwardly directed beams;

wherein said transmit and receive antennas are interleaved so that between adjacent connected pairs of lines of said transmit antenna there is a connected pair of lines of said receive antenna, said transmit antenna feed means is adjacent the first end of the receive antenna lines, and said receive antenna feed means is adjacent the first end of the transmit antenna lines; and

wherein the antenna system further comprises;

isolation means positioned between the lines of the transmit and receive antennas for reducing the mutual coupling between the transmit and receive antennas.

2. The antenna system according to claim 1 wherein the isolation means includes resistive material forming a continuous line between the lines of the transmit and receive antennas.

3. The antenna system according to claim 1 wherein:

said first array group of said transmit antenna is phased differently from said second array group of said transmit antenna so as to provide a predetermined pitch angle to the four transmit antenna beams and to reduce the coupling between said first and second array groups; and

said third array group of said receive antenna is phased differently from said fourth array group of said receive antenna so as to provide said predetermined pitch angle to the four receive antenna beams in the same direction as the pitch angle of the four transmit antenna beams and to reduce the coupling between said third and fourth array groups.

4. The antenna system according to claim 3 wherein said predetermined pitch angle is approximately 3°

toward the forward direction of travel.

5. The antenna system according to claim 3 wherein each of said transmit antenna feed means and said receive antenna feed means includes a respective crossover feed structure having a four port branch-arm hybrid structure and wherein the spacing between adjacent connected lines within each antenna is less than the spacing between adjacent non-connected lines within each antenna so that connected line pairs of the transmit and receive antennas may be interleaved within the spacing defined by the length of the diagonal of the hybrid structure, whereby two complete space duplexed antennas are contained within a common aperture with each antenna utilizing the entire common aperture.

6. The antenna system according to claim 5 wherein said predetermined pitch angle is approximately 3°

toward the forward direction of travel.

7. The antenna system according to claim 5 wherein the isolation means includes resistive material forming a continuous line between the lines of the transmit and receive antennas.