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US4360182A Expired / Lapsed US ⏱️ 0.0 years remaining

High-agility reflector support and drive system

Assignee: United States Department of the Navy
•
Filing: 1980-06-25
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Granted: 1982-11-23
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Expires: 2000-06-25
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Abstract

Abstract An apparatus for mounting a device defining a mounting plane so as to be ectively rotatable about mutually perpendicular axis with respect to a base member defining a base plane. The first axis is defined by a transverse pin fitted to the gimbal and rotatably secured to the base plane. The mounting plane is tilted about either axis by driving an associated, diagonally opposite pair of support arm members linearly so as to foreshorten one support arm member to the extent that the other is lengthened.

Inventors

  • 👤 James W. Titus

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 20:17
CPC Classifications
H; H01; H01Q; H01Q3/00; H01Q3/02; H01Q3/08; F; F16; F16M; F16M11/00; F16M11/02; F16M11/04; F16M11/06; F16M11/10; F24; F24S; F24S30/00; F24S30/40; F24S30/45; F24S30/452; G; G01; G01D; G01D11/00; G01D11/30; G09; G09B; G09B9/00; G09B9/02; G09B9/08; G09B9/12; G09B9/14; G09B9/16; G09B9/20; F16M2200/00; F16M2200/04; F16M2200/041; F24S2030/10; F24S2030/11; F24S2030/115; Y; Y02; Y02E; Y02E10/00; Y02E10/40; Y02E10/47

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 218 words
Apparatus for mounting a device defining a mounting plane so as to be selectively rotatable about mutually perpendicular axes with respect to a base defining a base plane and so as to be capable of being pointed with extreme accuracy and moved with high velocity or rapid acceleration, comprising: four suspension points lying in and defining each of the base and mounting planes, the suspension points in each of the planes arranged in like geometric symmetry and defining rhombi lying in each of the planes; four support-arm members joining the base and mounting planes and terminated at opposed pairs of suspension points in the planes, each support-arm member including a linear actuator and having first and second joints at its respective ends; a gimbal having a longitudinal rotation axis; means for rotatably mounting the gimbal to the mounting plane such that the longitudinal rotation axis of the gimbal passes through the first joints associated with one pair of diagonally opposite support-arm members; a pin fitted transversely to the gimbal and having a longitudinal rotation axis; and means for rotatably mounting the pin to the base lane such that the longitudinal rotation axis of the pin passes through the first joints associated with the other pair of digonally opposite support-arm members when the base and mounting planes are parallel.
Claim 2
Dependent Claim 218 words
Apparatus for mounting a device defining a mounting plane so as to be selectively rotatable about mutually perpendicular axes with respect to a base defining a base plane and so as to be capable of being pointed with extreme accuracy and moved with high velocity or rapid acceleration, comprising: four suspension points lying in and defining each of the base and mounting planes, the suspension points in each of the planes arranged in like geometric symmetry and defining rhombi lying in each of the planes; four support-arm members joining the base and mounting planes and terminated at opposed pairs of suspension points in the planes, each support-arm member including a linear actuator and having first and second joints at its respective ends; a gimbal having a longitudinal rotation axis; means for rotatably mounting the gimbal to the mounting plane such that the longitudinal rotation axis of the gimbal passes through the first joints associated with one pair of diagonally opposite support-arm members; a pin fitted transversely to the gimbal and having a longitudinal rotation axis; and means for rotatably mounting the pin to the base lane such that the longitudinal rotation axis of the pin passes through the first joints associated with the other pair of digonally opposite support-arm members when the base and mounting planes are parallel.
Claim 3
Dependent Claim 37 words
The apparatus recited in claim 1 including: control means for simultaneously increasing the length of one of the linear actuators in a diagonally opposite pair of support-arm members while diminishing the length of the other linear actuator.
Claim 4
Dependent Claim 23 words
The apparatus recited in claim 1 wherein the gimbal-mounting means includes: a pair of depending brackets on the mounting plane engaging the gimbal.
Claim 5
Dependent Claim 23 words
The apparatus recited in claim 1 wherein the pin-mounting means includes: an upstanding bearing secured to the base plane and engaging the pin.
Claim 6
Dependent Claim 19 words
The apparatus recited in claim 1 wherein the linear actuator includes: a cylinder; and a piston in the cylinder.
Claim 7
Dependent Claim 15 words
The apparatus recited in claim 2 wherein the control means includes: an electrohydraulic control system.
Claim 8
Dependent Claim 15 words
The apparatus recited in claim 1 including: an angular motion transducer coupled to the gimbal.
Claim 9
Dependent Claim 15 words
The apparatus recited in claim 1 including: an angular motion transducer coupled to the pin.

References Cited (Backward Citations)

US1280092A Cited
US2099857A Cited
US2585579A Cited
US2524238A Cited
US2683588A Cited
US2975993A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-11-22 1986-05-24 1986-11-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-11-22 1990-05-24 1990-11-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-11-22 1994-05-24 1994-11-23 $7700.00 Window Closed / Lapsed

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