Gravity-Stabilized Sensor Mount for Moving Platform

• US 20120305741A1
• Filed: 04/27/2012
• Published: 12/06/2012
• Est. Priority Date: 05/31/2011
• Status: Abandoned Application

• Current Assignee: PFG Ip, LLC
• Original Assignee: ISC8 Incorporated
• Inventors: Sapir, Itzhak
• Application Number:
  US13/457,566
• Publication Number:
  US 20120305741A1
• Time in Patent Office: Days
• US Class Current: 248/636
• CPC Class Codes: B63B 2017/0072 Seaway compensators
• CPC Class Codes: F16M 11/123 the axis of rotation intersecting in a single point, e.g. by using gimbals
• CPC Class Codes: G01D 11/02 Bearings or suspensions for moving parts
• CPC Class Codes: G02B 27/644 compensating for large deviations, e.g. maintaining a fixed line of sight while a vehicle on which the system is mounted changes course
• CPC Class Codes: G02B 7/001 Counterbalanced structures, e.g. surgical microscopes

Abstract

A gravity-stabilized sensor mount is disclosed having a base member pivotably coupled to a multi-axis gimbal with damping means disposed between the base member and one or more gimbal elements. The gimbal assembly is coupled to a connecting member which may, in turn, be coupled to a moving platform such as a land vehicle, aircraft or marine vessel. The base member may have a payload such as a sensor system mounted on it and is provided with counter-balances so that the base member remains level in two horizontal axes with respect to the surface of the Earth regardless of the vertical orientation of the connecting member.

Claims

1. A sensor mount comprising:

a base member,

a multi-axis gimbal assembly defining a first vertical axis,

the base member pivotably coupled to the gimbal assembly whereby the net gravitational forces acting on the base member have zero moment about the first vertical axis irrespective of the angle of the first vertical axis.

2. A sensor mount comprising:

a base member,

a multi-axis gimbal assembly defining a first vertical axis,

damper means disposed between the base member and the gimbal assembly for absorbing kinetic energy,

the base member pivotably coupled to the gimbal assembly whereby the net gravitational forces acting on the base member have zero moment about the first vertical axis irrespective of the angle of the first vertical axis.

3. The sensor mount of claim 2 further comprising a payload having a first mass, and,

payload counter-balance means for providing a second mass at one or more predetermined positions on the base member whereby the net gravitational forces acting on the base member have zero moment about the first vertical axis irrespective of the angle of the first vertical axis.

4. The sensor mount of claim 3 wherein the payload comprises at least one electro-optical sensor for generating an electrical output in response to an input of a predetermined range of the electromagnetic spectrum.

5. The sensor mount of claim 3 wherein the damper means is a hydraulic damper.

6. The sensor mount of claim 3 wherein the damper means is a pneumatic damper.

7. The sensor mount of claim 3 wherein the damper means is a friction damper.