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US3708795A Expired / Lapsed US ⏱️ 0.0 years remaining

Cassegrain antenna mounted in aircraft nose cone

Assignee: BAE Systems PLC
•
Filing: 1971-02-10
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Granted: 1973-01-02
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Expires: 1991-02-10
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Abstract

Abstract A forward-facing aircraft antenna of modified Cassegrain configuration, having a flat plate main dish and a sub-dish which has a reflecting surface chosen from among surfaces of revolution that require two or more reflections to bring a wave parallel to the axis of revolution to a substantial point focus.

Inventors

  • 👤 J Lyons

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 18:45
CPC Classifications
H; H01; H01Q; H01Q1/00; H01Q1/27; H01Q1/28; H01Q1/281; H01Q19/00; H01Q19/10; H01Q19/18; H01Q19/19; H01Q19/195

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 95 words
A forward-looking aircraft antenna of substantially Cassegrain configuration, comprising a main dish in flat plate form, and a sub-dish forward of the main dish with a reflecting surface in the form of a surface of revolution generated about a fore-and-aft axis passing through the center of the main dish, said sub-dish surface being chosen from the class of surfaces of revolution that require more than a single reflection at said sub-dish to bring a wave approaching from said main dish anD parallel to said axis of revolution to a substantial point focus on said axis.
Claim 2
Dependent Claim 95 words
A forward-looking aircraft antenna of substantially Cassegrain configuration, comprising a main dish in flat plate form, and a sub-dish forward of the main dish with a reflecting surface in the form of a surface of revolution generated about a fore-and-aft axis passing through the center of the main dish, said sub-dish surface being chosen from the class of surfaces of revolution that require more than a single reflection at said sub-dish to bring a wave approaching from said main dish anD parallel to said axis of revolution to a substantial point focus on said axis.
Claim 3
Dependent Claim 15 words
An antenna according to claim 1, wherein the sub-dish also constitutes the external aircraft radome.
Claim 4
Dependent Claim 19 words
An antenna according to claim 1, wherein the chosen surface requires two reflections to achieve a substantial point focus.
Claim 5
Dependent Claim 33 words
An antenna according to claim 3, wherein the sub-dish surface has an equation of the form: x/F (1 - (y/2F)2) - (y/F) Square Root 1 + (y/2F)2 where F is the focal length.
Claim 6
Dependent Claim 30 words
An antenna according to claim 4, wherein the angular spread of the feed to the sub-dish, measured from the axis of revolution of the sub-dish surface, is substantially 36* .
Claim 7
Dependent Claim 51 words
An antenna according to claim 1, wherein the chosen surface requires more than two reflections to achieve a substantial point focus and has an equation of the form: y A(1 - x) + B (1 - x2) where A and B are empirically determined constants for any particular number of reflections.
Claim 8
Dependent Claim 18 words
An antenna according to claim 6, wherein the number of reflections is three, A 1.4226 and B 0.0774.
Claim 9
Dependent Claim 18 words
An antenna according to claim 6, wherein the number of reflections is four, A 0.3358 and B 0.0392.
Claim 10
Dependent Claim 18 words
An antenna according to claim 6, wherein the number of reflections is five, A 0.2751 and B 0.0249.

References Cited (Backward Citations)

US3084342A Cited
US3231893A Cited
US3414904A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-01-02 1976-07-03 1977-01-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-01-02 1980-07-03 1981-01-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-01-02 1984-07-03 1985-01-02 $7700.00 Window Closed / Lapsed

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