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US4037540A Expired / Lapsed US ⏱️ 0.0 years remaining

Directional antenna for a projectile or rocket detonator

Assignee: Telefunken Systemtechnik AG
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Filing: 1975-11-11
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Granted: 1977-07-26
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Expires: 1995-11-11
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Abstract

Abstract In a projectile or rocket having a metal outer shell and including a proximity or influence detonator which operates with electromagnetic waves, particularly according to the reflected beam principle, and a directional antenna with a rotationally symmetrical radiation diagram for said detonator, the antenna is constituted by a circular slot which is coaxial with the longitudinal axis of the projectile or rocket and the antenna is excited with a line or cavity resonator disposed in the projectile or rocket and connected between the detonator and the antenna.

Inventors

  • 👤 Wolfgang Keydel

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 10:08
CPC Classifications
H; H01; H01Q; H01Q13/00; H01Q13/10; H01Q13/18; F; F42; F42C; F42C13/00; H01Q1/00; H01Q1/27; H01Q1/28; H01Q1/281

Claims Analysis

Total Claims: 18
Claim 1
Independent Claim 96 words
In a projectile or rocket having a metal outer shell and including a proximity or influence detonator operating with electromagnetic waves, particularly according to the reflected beam principle, and a directional antenna having a rotationally symmetrical radiation diagram for said detonator, the improvement wherein said antenna is constituted by a circular slot which is formed in said outer shell and which is coaxial with the longitudinal axis of the said projectile or rocket; and further comprising resonator means disposed within said outer shell, and coupled between said antenna and said detonator for exciting said circular slot.
Claim 2
Dependent Claim 96 words
In a projectile or rocket having a metal outer shell and including a proximity or influence detonator operating with electromagnetic waves, particularly according to the reflected beam principle, and a directional antenna having a rotationally symmetrical radiation diagram for said detonator, the improvement wherein said antenna is constituted by a circular slot which is formed in said outer shell and which is coaxial with the longitudinal axis of the said projectile or rocket; and further comprising resonator means disposed within said outer shell, and coupled between said antenna and said detonator for exciting said circular slot.
Claim 3
Dependent Claim 17 words
Apparatus as defined in claim 1 wherein said antenna is dimensioned to operate as a resonator antenna.
Claim 4
Dependent Claim 14 words
Apparatus as defined in claim 1 wherein said resonator means is a line resonator.
Claim 5
Dependent Claim 15 words
Apparatus as defined in claim 3 wherein said resonator means is a cylindrical line resonator.
Claim 6
Dependent Claim 15 words
Apparatus as defined in claim 3 wherein said resonator means is a conical line resonator.
Claim 7
Dependent Claim 61 words
Apparatus as defined in claim 3 wherein: said line resonator is disposed between the tip of said projectile or rocket and said circular slot, with the major axis of said resonator coinciding with the longitudinal axis of said projectile or rocket; and means for coupling said detonator to said resonator at the end of said resonator disposed opposite said circular slot.
Claim 8
Dependent Claim 34 words
Apparatus as defined in claim 6 wherein said line resonator is conically designed and occupies the major portion of the structural volume between the tip of said projectile or rocket and said circular slot.
Claim 9
Dependent Claim 98 words
Apparatus as defined in claim 6 wherein: said outer shell is conical at the portion thereof approaching the tip of said projectile or rocket, said circular slot is formed on the conical portion of said outer shell, said shell is substantially hollow between said circular slot and the tip of said projectile or rocket and said line resonator is formed by a conductor extending along the longitudinal axis of said projectile or rocket and having one end connected to said detonator and its other end coupled to said outer shell at the tip of said projectile or rocket.
Claim 10
Dependent Claim 14 words
Apparatus as defined in claim 1 wherein said resonator means is a cavity resonator.
Claim 11
Dependent Claim 15 words
Apparatus as defined in claim 9 wherein said cavity resonator is a conical cavity resonator.
Claim 12
Dependent Claim 15 words
Apparatus as defined in claim 9 wherein said cavity resonator is a cylindrical cavity resonator.
Claim 13
Dependent Claim 62 words
Apparatus as defined in claim 9 wherein said cavity resonator is disposed between the tip of said projectile or rocket and said circular slot with the major axis of said resonator coinciding with the longitudinal axis of said projectile or rocket and means for coupling said detonator to said resonator at the end of said resonator which is adjacent said circular slot.
Claim 14
Dependent Claim 42 words
Apparatus as defined in claim 12 wherein said means for coupling comprises a coupling pin disposed along the longitudinal axis of said projectile and having one end connected to said detonator and its other end extending into the cavity of said resonator.
Claim 15
Dependent Claim 32 words
Apparatus as defined in claim 12 wherein said cavity resonator is conically designed and occupies the major portion of the structural volume between the tip of said projectile and said circular slot.
Claim 16
Dependent Claim 61 words
Apparatus as defined in claim 14 wherein said outer shell is conical at the portion thereof approaching the tip of said projectile or rocket, said circular slot is formed on the conical portion of said outer shell, and said outer shell is substantially hollow between said circular slot and the tip of said projectile or rocket to form said cavity resonator.
Claim 17
Dependent Claim 27 words
Apparatus as defined in claim 1 wherein said resonator means comprise means for exciting said antenna with a wave mode which is higher that the fundamental mode.
Claim 18
Dependent Claim 23 words
Apparatus as defined in claim 1 wherein said circular slot is spaced at a distance of λ/2 from the tip of said projectile.

References Cited (Backward Citations)

US2611865A Cited
US3074063A Cited
US2867803A Cited
US3127609A Cited
US3293645A Cited
US3346865A Cited
US3518685A Cited
US3914767A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-07-25 1981-01-24 1981-07-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-07-25 1985-01-24 1985-07-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-07-25 1989-01-24 1989-07-26 $7700.00 Window Closed / Lapsed

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