US4115777A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft landing systems
Assignee: BAE Systems Electronics Ltd
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Filing: 1976-10-27
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Granted: 1978-09-19
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Expires: 1996-10-27
Abstract
Abstract A dual I.L.S. glide slope system for allowing a normal 3° descent path plus an additional 6° descent path which can be used for noise abatement procedures etc. In accordance with the present invention these glide slopes are provided on a single assigned R.F. channel with no inverted courses interposed. The first signal null will occur at 9° elevation when all signals will be zero, producing a "flag" alarm.
Inventors
- 👤 Frank Howard Taylor
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 06:00
CPC Classifications
G; G01; G01S; G01S1/00; G01S1/02; G01S1/08; G01S1/14; G01S1/18
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
101 words
An aircraft landing system for aircraft having I.L.S. equipment, including a glide slope antenna system which comprises two antennae mounted on a support structure at respective heights above ground in the ratio of 3:2 and signal generating and distribution means for generating and feeding respective signals to said antennae so that the antennae provide in combination a multi-lobe radiation pattern which produces resultant signals just below and just above slope paths at 3° and 6° angles to the ground for generating in an approaching aircraft "fly-up" and "fly-down" signals, respectively, thereby providing for glide slope approaches by aircraft at said angles.
Claim 2
Dependent Claim
101 words
An aircraft landing system for aircraft having I.L.S. equipment, including a glide slope antenna system which comprises two antennae mounted on a support structure at respective heights above ground in the ratio of 3:2 and signal generating and distribution means for generating and feeding respective signals to said antennae so that the antennae provide in combination a multi-lobe radiation pattern which produces resultant signals just below and just above slope paths at 3° and 6° angles to the ground for generating in an approaching aircraft "fly-up" and "fly-down" signals, respectively, thereby providing for glide slope approaches by aircraft at said angles.
Claim 3
Dependent Claim
22 words
An aircraft landing system as claimed in claim 1, in which the glide slope antenna system is of the "null reference" type.
Claim 4
Dependent Claim
45 words
An aircraft landing system as claimed in claim 2, in which the lower antenna of the glide slope antenna system is fed with an R.F. carrier plus double sideband signals and in which the upper antenna is fed with sideband signals without said R.F. carrier.
Claim 5
Dependent Claim
70 words
An aircraft landing system as claimed in claim 1, in which the glide slope antenna system is located at a position offset to one side of the centre line of the runway near the approach or threshold end of the runway and in which a localiser antenna system for affording guidance of an aircraft along the centre line of the runway is located at the far end of said runway.
Claim 6
Dependent Claim
139 words
An aircraft landing system as claimed in claim 1, in which the antennae of a glide slope antenna system are located at 28 feet and 18 feet 8 inches, respectively, above ground, the signal fed to the lower antenna being a double sideband carrier with the carrier being within the band 328-336MHz and the sidebands being separated from the carrier by 90Hz and 150Hz but whose mean frequency components are in phase with the carrier, and the signal fed to the upper antenna being a double sideband signal with the sidebands separated by 90Hz and 150Hz, the mean frequency components of the 150Hz sideband being 180° out of phase with the mean frequency components of the 90Hz sideband and the mean frequency components of the 90Hz sidebands being in phase with the carrier of said double sideband carrier signal.
Claim 7
Dependent Claim
30 words
An aircraft landing system for helicopters as claimed in claim 1, in which the glide slope antenna system is combined with an I.L.S. localiser antenna system adjacent a landing pad.
References Cited (Backward Citations)
No citation records indexed.
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-09-18 | 1982-03-20 | 1982-09-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-09-18 | 1986-03-20 | 1986-09-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-09-18 | 1990-03-20 | 1990-09-19 | $7700.00 | Window Closed / Lapsed |