IP Library Granted Patent US 7,081,861
Granted Patent B2
US 7,081,861 · App. 10/512,650 · Granted Jul 25, 2006

Phased array antenna

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Quick Facts
Patent No.
US 7,081,861
App. No.
10/512,650
Granted
Jul 25, 2006
Kind
B2
Abstract

The invention discloses an antenna system, which includes an array structure provided with a plurality of radiator elements being adapted to transmit and receive radiated electromagnetic waves. Each of the radiator elements are provided with at least two transverse interconnecting slots forming an aperture. An array feed network is operatively associated with each radiator element and is adapted to transmit a signal to and receive a signal from each radiator element and is further adapted to provide at least one common feed point for the array structure. A phase shifting unit operatively joins each radiator element to its associated feed point, the phase shifting unit being adapted to selectively adjust a phase of the electromagnetic waves associated with each radiator element. Operation of each phase shifting unit is regulated by control means for controlling the generation of a radiation pattern.

Claims (43)

1. An antenna system which includes

a) an array structure provided with a plurality of radiator elements being adapted to transmit and receive radiated electromagnetic waves;

b) each radiator element being provided with at least two transverse interconnecting slots forming an aperture;

c) an array feed network operatively associated with each radiator element and being adapted to transmit a signal to and receive a signal from each radiator element and further being adapted to provide at least one common feed point for the array structure;

d) a phase shifting unit operatively joining each radiator element to its associated feed point, the phase shifting unit being adapted to selectively adjust a phase of the electromagnetic waves associated with each radiator element; and

e) control means for regulating operation of each phase shifting unit and thereby controlling generation of a radiation pattern.

2. An antenna system as claimed in claim 1 , in which the radiation pattern is a travelling wave array formation being adapted to enhance gain performance in lower elevation regions.

3. An antenna system as claimed in claim 2 , in which the gain performance is enhanced when the travelling wave array formation is directed to within 30 degrees of its horizon.

4. An antenna system as claimed in claim 1 , in which the array structure is substantially in the form of a hexagonal grid wherein adjacent radiator elements are spaced apart by less than half a wavelength of the electromagnetic waves.

5. An antenna system as claimed in claim 1 , in which each radiator element is adapted to be circularly polarized and is further adapted to generate circularly polarized electromagnetic waves.

6. An antenna system as claimed in claim 1 , in which each radiator element includes a shell forming a conductive cavity, the shell extending above a conductive ground plane.

7. An antenna system as claimed in claim 6 , in which the ground plane is planar or non-planar.

8. An antenna system as claimed in claim 6 , in which the conductive cavity has a depth less than a quarter of a wavelength of the electromagnetic waves.

9. An antenna system as claimed in claim 6 , in which the conductive cavity has a diameter less than a half of a wavelength of the electromagnetic waves.

10. An antenna system as claimed in claim 1 , in which the conductive cavity is circular cylindrical or hexagonal cylindrical in shape.

11. An antenna system as claimed in claim 1 , in which each transverse slot has a length less than a half of a wavelength of the electromagnetic waves.

12. An antenna system as claimed in claim 1 , in which each transverse slot is adapted to be operatively excited with at least one excitation point provided at least one end of each slot.

13. An antenna system as claimed in claim 1 , in which each transverse slot is radially offset relative to each other associated slot and each slot being adapted to be excited with an appropriate phase relative to each other so as to generate circular polarization.

14. An antenna system as claimed in claim 13 , in which two transverse slots are provided, one slot being orthogonally orientated relative to the other slot and the slots being adapted to be excited out of phase by 90 relative to each other so as to generate circular polarization.

15. An antenna system as claimed in claim 1 , in which each radiator element includes a feed structure being adapted to excite each transverse slot.

16. An antenna system as claimed in claim 15 , in which each feed structure includes a reactive transmission line circuit.

17. antenna system as claimed in claim 16 , in which the transmission line circuit includes various transmission lines with different characteristics being adapted to achieve optimal circular polarisation of the radiation pattern when the array structure is directed to below 30 of its horizon.

18. An antenna system as claimed in claim 15 , in which each feed structure is located within the conductive cavity of its associated radiator element.

19. An antenna system as claimed in claim 1 , in which the array feed network includes a corporate configuration, a series configuration, or combination of a corporate and a series configuration.

20. An antenna system as claimed in claim 1 , in which the phase shifting unit is adapted to permit spatial steering of the radiation pattern.

21. An antenna system as claimed in claim 1 , in which each radiator element includes an operatively associated parasitic element.

22. An antenna system as claimed in claim 21 , in which each parasitic element is located above the transverse slots of its associated radiator element.

23. An antenna system as claimed in claim 21 , in which each parasitic element is provided in one of the following shapes: circular disc or ring, elliptical disc, square, spiral and which is formed into a planar, cylindrical, conical, spherical or saddle shape.

24. An antenna system as claimed in claim 21 , in which the parasitic element size, shape and spacing is selected for suitably manipulating mutual electromagnetic coupling prevalent between adjacent radiator elements to thereby obtain a desired radiation pattern.

25. An antenna system as claimed in claim 1 , which includes capacitive or inductive elements located between adjacent radiator elements and being adapted to manipulate mutual electromagnetic coupling prevalent between adjacent radiator elements to thereby obtain a desired radiation pattern.

26. An antenna system as claimed in claim 1 , which includes capacitive or inductive elements located along an outer perimeter of the array structure and being adapted to manipulate mutual electromagnetic coupling prevalent between adjacent radiator elements to thereby obtain a desired radiation pattern.

27. A radiator element for use in an antenna system and being adapted to receive radiated electromagnetic waves, which radiator element includes a conductive ground plane; a shell forming a conductive cavity, the shell extending above the conductive ground plane and forming a wall spaced apart from the ground plane; at least two transverse slots provided in the wall and being adapted to form a crossed-slot aperture; and a parasitic element operatively associated with the transverse slots, wherein the radiator element is adapted to be circularly polarized and to generate circularly polarized electromagnetic waves, the ground plane is planar or non-planar, the conductive cavity has a depth less than a quarter of a wavelength of the electromagnetic waves, and the conductive cavity has a diameter less than a half of a wavelength of the electromagnetic waves.

28. A radiator element as claimed in claim 27 , in which the conductive cavity is circular cylindrical or hexagonal cylindrical in shape.

29. A radiator element as claimed in claim 27 , in which each transverse slot has a length less than a half of a wavelength of the electromagnetic waves.

30. A radiator element as claimed in claim 27 , in which each transverse slot is adapted to be operatively excited with at least one excitation point provided at at least one end of each slot.

31. A radiator element as claimed in claim 27 , in which each slot is radially offset relative to each other associated slot and each slot being adapted to be excited with an appropriate phase relative to each other so as to generate circular polarization.

32. A radiator element as claimed in claim 31 , in which two transverse slots are provided, one slot being orthogonally orientated relative to the other slot and the slots being adapted to be excited out of phase by 90 relative to each other so as to generate circular polarization.

33. A radiator element as claimed in claim 27 , which is provided with a feed structure being adapted to excite each transverse slot.

34. A radiator element as claimed in claim 33 , in which each feed structure includes a reactive transmission line circuit.

35. A radiator element as claimed in claim 34 , in which the transmission line circuit includes various transmission lines with varying characteristics obtained by varying the lengths of the transmission lines.

36. A radiator element as claimed in claim 33 , in which each feed structure is located within the conductive cavity.

37. A radiator element as claimed in claim 27 , in which the parasitic element is located above the transverse slots.

38. A radiator element as claimed in claim 27 , in which the parasitic element is provided in one of the following shapes: circular disc or ring, elliptical disc, square, spiral, and which is formed into a planar, cylindrical, conical, spherical or saddle shape.

Assignments (6)
RELEASE OF PATENT SECURITY AGREEMENT RECORDED FEBRUARY 5, 2021 AT REEL/FRAME 055165/0001 Recorded Jun 6, 2024
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; AEROSONIC LLC; MOUNTAINTOP TECHNOLOGIES, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; SHIELD RESTRAINT SYSTEMS, INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS, INC.; AEROSONIC CORPORATION; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE INC.; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; PURE TECHNOLOGIES LTD.; HARCO LABORATORIES, INC.; HARCO LLC; HARCO TECHNOLOGIES CORPORATION; CORRPRO COMPANIES, INC.; HARCO CORPORATION; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL GMBH; TELAIR INTERNATIONAL AB; NORDISK AVIATION PRODUCTS AS; TURNTIME TECHNOLOGIES AB; AEROCONTROLEX GROUP, INC.; TRANSICOIL INC.; SOUTHCO, INC.; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS COMPANY; JOSLYN SUNBANK COMPANY LLC; LEACH INTERNATIONAL CORPORATION; SOURIAU USA, INC.; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; ROLLS-ROYCE PLC; MEMTRON TECHNOLOGIES CO.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.; AERO-INSTRUMENTS CO., LLC; AIRBORNE SYSTEMS NA, INC.; HARCOSEMCO LLC; HARCO, LLC (N/K/A HARCOSEMCO LLC); PEXCO AEROSPACE, INC.; TELAIR US LLC; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; ADAMS RITE AEROSPACE, INC.; ACME AEROSPACE, INC.; SCHNELLER, INC.; CEF INDUSTRIES, INC.
Reel/Frame 067640/0327 →
RELEASE OF SECURITY INTEREST Recorded Apr 19, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TA AEROSPACE CO.; TRANSDIGM, INC.; TRANSDIGM GROUP INCORPORATED; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECH TYEE, INC.; BEAM'S INDUSTRIES; BREEZE EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INC.; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; LEACH INTERNATIONAL CORPORATION; NMC GROUP INC.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.
Reel/Frame 063363/0753 →
SECURITY INTEREST Recorded Feb 5, 2021
From: CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.)
To: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS AGENT
Reel/Frame 055164/0945 →
SECURITY INTEREST Recorded Feb 5, 2021
From: CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.)
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 055165/0001 →
SECURITY INTEREST Recorded Feb 5, 2021
From: CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.)
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 055165/0027 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 25, 2004
From: STEYN, PIERRE; GEORGE, WILLIAM IAN; PRETORIUS, JOHANNES ARNOLDUS; BIRCH, MAX LARIVIERE
To: CHELTON, INC.
Reel/Frame 016419/0901 →