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US4167739A Expired / Lapsed US ⏱️ 0.0 years remaining

Instrument landing system glidepath antenna array and drive therefor

Assignee: The University of Sydney
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Filing: 1977-11-04
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Granted: 1979-09-11
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Expires: 1997-11-04
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Abstract

Abstract An instrument landing system (ILS) glidepath antenna array and drive therefor which provides for lower susceptibility to above-ground interference and higher stability than the known M-array system. The antenna array also provides for a shorter image ground requirement than the known null reference and sideband reference systems. The antenna array comprises a four-element structure, two of which are driven with CBS only signals having relatively different amplitude and phase, and the other two elements of which are driven with SBO only signals having relatively different amplitude and phase.

Inventors

  • 👤 James G. Lucas
  • 👤 Alan C. Young

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 06:32
CPC Classifications
G; G01; G01S; G01S1/00; G01S1/02; G01S1/08; G01S1/14; G01S1/18; H; H01; H01Q; H01Q21/00; H01Q21/06; H01Q21/08; H01Q21/22

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 134 words
An instrument landing system for providing lower susceptibility to above ground interference and comprising an antenna array having four substantially equi-spaced elements arrayed one above another above a ground plane, the lowermost element and the centre one of the upper three elements being arranged to be driven to radiate CSB energy alone, and the uppermost element and the centre one of the lower three elements being arranged to be driven to radiate SOB energy alone, the relative amplitudes and phases of the drive signals being to the lowermost element, CSB 3/180°, to the centre of one of uppeer three elements, CSB 1/0°, to the uppermost element, SBO 1/0°, to the centre one of lower three elements, SBO 2/180°, the drive magnitudes being variable by ±15%, and by the phase angles being variable by +10°.
Claim 2
Dependent Claim 134 words
An instrument landing system for providing lower susceptibility to above ground interference and comprising an antenna array having four substantially equi-spaced elements arrayed one above another above a ground plane, the lowermost element and the centre one of the upper three elements being arranged to be driven to radiate CSB energy alone, and the uppermost element and the centre one of the lower three elements being arranged to be driven to radiate SOB energy alone, the relative amplitudes and phases of the drive signals being to the lowermost element, CSB 3/180°, to the centre of one of uppeer three elements, CSB 1/0°, to the uppermost element, SBO 1/0°, to the centre one of lower three elements, SBO 2/180°, the drive magnitudes being variable by ±15%, and by the phase angles being variable by +10°.
Claim 3
Dependent Claim 31 words
An instrument landing system as claimed in claim 1, wherein the lowermost element is spaced from the ground plane by a distance substantially equal to the spacing between the array elements.

References Cited (Backward Citations)

GB1053232A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-09-10 1983-03-12 1983-09-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-09-10 1987-03-12 1987-09-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-09-10 1991-03-12 1991-09-11 $7700.00 Window Closed / Lapsed

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