Gravity gradiometer

• US 9,038,456 B2
• Filed: 07/02/2012
• Issued: 05/26/2015
• Est. Priority Date: 07/02/2012
• Status: Active Grant

• Current Assignee: SRC, Inc.
• Original Assignee: SRC, Inc.
• Inventors: DiStasio, Marcello M., Nicolaescu, Ion V.
• Primary Examiner(s): McCall, Eric S
• Assistant Examiner(s): Megna Fuentes, Anthony W
• Application Number:
  US13/539,988
• Publication Number:
  US 20140000362A1
• Time in Patent Office: 1,058 Days
• Field of Search: 733/82.R, 733/83, 733/82.G, 7351401-51402, 735/041.2, 7350402-50404
• US Class Current: 73/382.G
• CPC Class Codes: G01V 7/00 Measuring gravitational fields or waves; Gravimetric prospecting or detecting
• CPC Class Codes: G01V 7/16 specially adapted for use on moving platforms, e.g. ship, aircraft

Abstract

A gravity gradiometer having at least three differential accelerometers with a low response to linear accelerations and at least six angular accelerometers that give it the capability of measuring angular rates by integrating the angular accelerations. Both types of accelerometers are based on a compliant mechanism with very low and adjustable stiffness that is achieved by using flexures under compressive load that contribute a negative stiffness to the total elastic response of the mechanism. Both types of accelerometers are operated in a servo-compensation feedback mode so that at no time is the mechanism far from its equilibrium position.

Claims

1. A planar compliant mechanism, comprising:

a rigid frame;

first, second, third and fourth nodes interconnected by first, second, third, and fourth beams and forming a quadrilateral having one of said nodes at each corner and one of said beams interconnecting two of said nodes;

first, second, third and fourth suspensions interconnected to said frame and to each of said first, second, third and fourth nodes, respectively, wherein each of said suspensions constrain each of said nodes to rectilinear movement;

an actuator for loading at least one of said suspensions with a compressive force; and

an adjustment screw associated with said actuator for modifying the compressive force.

2. The planar compliant mechanism of claim 1, wherein said first, second, third and fourth suspensions each comprise a double parallelogram mechanism.

3. The planar compliant mechanism of claim 2, wherein said first, second, third, and fourth beams comprise a rigid portion located between two flexible portions.

4. The planar compliant mechanism of claim 1, further comprising a displacement sensor associated with at least one of said nodes.

5. The planar compliant mechanism of claim 4, further comprising an actuator configured to apply a force to at least one of said nodes.

6. A differential accelerometer, comprising

a rigid frame;

first, second, third and fourth nodes interconnected by first, second, third, and fourth beams and forming a quadrilateral having one of said nodes at each corner and one of said beams interconnecting two of said nodes;

first, second, third and fourth suspensions interconnected to said frame and to each of said first, second, third and fourth nodes, respectively, wherein each of said suspensions constrain each of said nodes to rectilinear movement;

two equal test masses interconnected to an opposing pair of said first, second, third and fourth nodes; and

four balancing blocks, each having a plurality of adjustment screws of various sizes and placed at different orientations and each being attached to one of said beams

7. The differential accelerometer of claim 6, further comprising an electronics package that is programmed to implement a control loop with negative feedback for maintaining the equilibrium position of said accelerometer.

8. An angular accelerometer, comprising

a rigid frame;

first, second, third and fourth nodes interconnected by first, second, third, and fourth beams and forming a quadrilateral having one of said node at each corner and one of said beams interconnecting any two of said nodes;

first, second, third and fourth suspensions interconnected to said frame and to each of said first, second, third and fourth nodes, respectively, wherein each of said suspensions constrain each of said nodes to rectilinear movement; and

two equal test masses interconnected to a midpoint of each of an opposing pair of said first, second, third, and fourth beams, wherein said two equal test masses include a plurality of adjustment screws of various size and placed at different orientations.

9. The angular accelerometer of claim 8, further comprising an electronics package programmed to implement a control loop with negative feedback for maintaining the equilibrium position of said accelerometer.

10. A gravity gradiometer comprising:

a plurality of differential accelerometers, each of which comprises

a first rigid frame,

first, second, third and fourth nodes interconnected by first, second, third, and fourth beams and forming a quadrilateral having one of said node at each corner and one of said beams interconnecting two of said nodes,

first, second, third and fourth suspensions interconnected to said first frame and to each of said first, second, third and fourth nodes, respectively, wherein each of said suspensions constrain each of said nodes to rectilinear movement, and

two equal test masses interconnected to an opposing pair of said first, second, third and fourth nodes;

a plurality of angular accelerometers, each of which comprises

a second rigid frame,

fifth, sixth, seventh, and eight nodes interconnected by fifth, sixth, seventh, and eight beams and forming a quadrilateral having one of said nodes at each corner and one of said beams interconnecting two of said nodes,

fifth, sixth, seventh, and eight suspensions interconnected to said frame and to each of said fifth, sixth, seventh, and eight nodes, respectively, wherein each of said suspensions constrain each of said nodes to rectilinear movement,

and two equal test masses interconnected to a midpoint of each of an opposing pair of said fifth, sixth, seventh, and eight beams;

an electronic package programmed to calculate a gradient tensor based on angular accelerations and acquiring off-diagonal elements by obtaining the calculated gradient sensor; and

three pairs of said angular accelerometers and three pairs of said differential accelerometers.

11. The gravity gradiometer of claim 10, wherein each of said three differential accelerometers is positioned at right angles to each other of said differential accelerometers.

12. The gravity gradiometer of claim 11, wherein each of said three pairs of said angular accelerometers comprise first and second angular accelerometers, each of which extends along a plane that is parallel to and spaced apart from the plane of the other accelerometer.

13. The gravity gradiometer of claim 11, wherein each of said three pairs of said angular accelerometers are positioned at right angles to each other pair.