High-agility reflector support and drive system

• US 4,360,182 A
• Filed: 06/25/1980
• Issued: 11/23/1982
• Est. Priority Date: 06/25/1980
• Status: Expired due to Term

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Titus, James W.
• Primary Examiner(s): Foss, J. Franklin
• Application Number:
  US06/163,000
• Time in Patent Office: 881 Days
• Field of Search: 248/371, 248/393, 248/184, 248/550, 248/663, 248/653, 248/654, 248/396, 434/55, 434/58, 343/878, 343/880
• US Class Current: 248/371
• CPC Class Codes: F16M 11/10 around a horizontal axis F16M11/12 takes precedence
• CPC Class Codes: F16M 2200/041 for balancing rotational movement of the head
• CPC Class Codes: F24S 2030/115 Linear actuators, e.g. pneumatic cylinders
• CPC Class Codes: F24S 30/452 Vertical primary axis
• CPC Class Codes: G01D 11/30 Supports specially adapted for an instrument; Supports specially adapted for a set of instruments
• CPC Class Codes: G09B 9/14 controlled by fluid actuated piston or cylinder ram
• CPC Class Codes: G09B 9/20 Simulation or indication of aircraft attitude
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation
• CPC Class Codes: Y02E 10/47 Mountings or tracking

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.

Claims

1. 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.

2. 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.

3. The apparatus recited in claim 1 wherein the gimbal-mounting means includes:

a pair of depending brackets on the mounting plane engaging the gimbal.

4. The apparatus recited in claim 1 wherein the pin-mounting means includes:

an upstanding bearing secured to the base plane and engaging the pin.

5. The apparatus recited in claim 1 wherein the linear actuator includes:

a cylinder; and

a piston in the cylinder.

6. The apparatus recited in claim 2 wherein the control means includes:

an electrohydraulic control system.

7. The apparatus recited in claim 1 including:

an angular motion transducer coupled to the gimbal.

8. The apparatus recited in claim 1 including:

an angular motion transducer coupled to the pin.