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US4384294A Expired / Lapsed US ⏱️ 0.0 years remaining

Stabilized antenna arrangement

Assignee: BAE Systems Electronics Ltd
•
Filing: 1981-05-01
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Granted: 1983-05-17
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Expires: 2001-05-01
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Abstract

Abstract A stabilized ship borne antenna arrangement is provided with an antenna which is stabilized against pitching and rolling motions of the ship on which it is mounted. The antenna is intended to rotate in azimuth about a stabilized vertical axis and it is mounted on a rotatable member which rotates about an unstabilized axis, which is fixed relative to the ship. Linear actuators link the antenna to the rotatable member with the lengths of the actuators being adjusted so as to maintain the vertical axis of the antenna as it rotates. The stabilized portion of the antenna arrangement is relatively light with a low center of gravity.

Inventors

  • 👤 Richard W. Crook
  • 👤 Ian Coghill
  • 👤 David R. James

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 13:40
CPC Classifications
H; H01; H01Q; H01Q1/00; H01Q1/12; H01Q1/18

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 221 words
A stabilised ship borne antenna arrangement comprising: a rotatable member arranged to rotate about an unstabilised axis which, in use, is fixed relative to the ship; a directional antenna mounted on said rotatable member so as to be rotatable therewith; an azimuth drive linkage arranged to transfer rotational motion from said rotatable member to said antenna, said linkage including at least two pin joints each rotatable about one of two mutually perpendicular axes, one of said at least two pin joints coupling said linkage to said rotatable member, and another of said at least two pin joints coupling said linkage to said antenna; a multi-axis joint mounting said antenna, the weight of said antenna being substantially wholly transmitted to said rotatable member via said multi-axis joint and said multi-axis joint permitting rotational movement about at least said two mutually perpendicular axes; two controllable actuators coupled between said rotatable member and said antenna for stabilising the azimuth axis of said antenna against pitch and roll motions of the ship, said actuators being positioned so that when they act in the same sense they cause movement of said antenna about a first predetermined axis, and when said two actuators act in mutually opposite senses they cause movement of said antenna about a second predetermined axis that is perpendicular to said first predetermined axis.
Claim 2
Dependent Claim 221 words
A stabilised ship borne antenna arrangement comprising: a rotatable member arranged to rotate about an unstabilised axis which, in use, is fixed relative to the ship; a directional antenna mounted on said rotatable member so as to be rotatable therewith; an azimuth drive linkage arranged to transfer rotational motion from said rotatable member to said antenna, said linkage including at least two pin joints each rotatable about one of two mutually perpendicular axes, one of said at least two pin joints coupling said linkage to said rotatable member, and another of said at least two pin joints coupling said linkage to said antenna; a multi-axis joint mounting said antenna, the weight of said antenna being substantially wholly transmitted to said rotatable member via said multi-axis joint and said multi-axis joint permitting rotational movement about at least said two mutually perpendicular axes; two controllable actuators coupled between said rotatable member and said antenna for stabilising the azimuth axis of said antenna against pitch and roll motions of the ship, said actuators being positioned so that when they act in the same sense they cause movement of said antenna about a first predetermined axis, and when said two actuators act in mutually opposite senses they cause movement of said antenna about a second predetermined axis that is perpendicular to said first predetermined axis.
Claim 3
Dependent Claim 26 words
An antenna arrangement as claimed in claim 1 and wherein each said actuator is constituted by an elongate device whose effective length can be controllably altered.
Claim 4
Dependent Claim 27 words
An antenna arrangement as claimed in claim 1 and wherein said multi-axis joint is provided separately of said pin joints and is constituted by a ball joint.
Claim 5
Dependent Claim 20 words
An antenna arrangement as claimed in claim 3 and wherein said ball joint is mounted directly on said rotatable member.
Claim 6
Dependent Claim 48 words
An antenna arrangement as claimed in claim 3 and wherein said antenna has a main elevation axis and said antenna is arranged to rotate about said main elevation axis by two of said at least two pin joints which are positioned on opposite sides of said ball joint.
Claim 7
Dependent Claim 66 words
An antenna arrangement as claimed in claim 5 and wherein said antenna has a cross elevation axis, said at least two pin joints includes a third pin joint and said antenna is arranged to rotate about said cross elevation axis by means of said third pin joint which is aligned with said cross elevation axis which passes through the center of rotation of said ball joint.
Claim 8
Dependent Claim 22 words
An antenna arrangement as claimed in claim 6 and wherein said first and second predetermined axes comprise the two said elevation axes.
Claim 9
Dependent Claim 46 words
An antenna arrangement as claimed in claim 7 and wherein said linkage includes a rigid V-shaped linkage having two arms between which said ball joint is located and said third pin joint is linked to said first two pin joints by means of said V-shaped linkage.
Claim 10
Dependent Claim 36 words
An antenna arrangement as claimed in claim 1 and wherein said antenna is mounted on a frame having a node point and said actuators each have an end connected to said node point of said frame.
Claim 11
Dependent Claim 30 words
An antenna as claimed in claim 9 and wherein said rotatable member has a base and said actuators each have another end connected to said base of said rotatable member.

References Cited (Backward Citations)

GB723951A Cited
GB766344A Cited
FR2247829B3 Cited
FR2248623B1 Cited
US4197548A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-05-16 1986-11-15 1987-05-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-05-16 1990-11-15 1991-05-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-05-16 1994-11-15 1995-05-17 $7700.00 Window Closed / Lapsed

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