Gravity gradiometer

• US 8,074,515 B2
• Filed: 03/01/2010
• Issued: 12/13/2011
• Est. Priority Date: 10/06/2005
• Status: Active Grant

• Current Assignee: Technological Resources Pty. Ltd. (Rio Tinto Limited)
• Original Assignee: Technological Resources Pty. Ltd. (Rio Tinto Limited)
• Inventors: Van Kann, Frank Joachim, Winterflood, John
• Primary Examiner(s): Williams, Hezron E
• Assistant Examiner(s): Shah, Samir M
• Application Number:
  US12/714,634
• Publication Number:
  US 20100154537A1
• Time in Patent Office: 652 Days
• Field of Search: 733/82.G, 733/82.R, 333/662.5, 333/661.1, 333/661.3, 333/662.6
• US Class Current: 73/382.G
• CPC Class Codes: G01V 7/16 specially adapted for use on moving platforms, e.g. ship, aircraft

Abstract

A gravity gradiometer is disclosed which has a sensor in the form of bars (41 and 42) which are supported on a mounting (5) which has a first mount section (10) and a second mount section (20). A first flexure web (33) pivotally couples the first and second mount sections about a first axis. The second mount has a first part (25), a second part (26) and a third part (27). The parts (25 and 26) are connected by a second flexure web (37) and the parts (26 and 27) are connected by a third flexure web (35). The bars (41 and 42) are located in housings (45 and 47) and form a monolithic structure with the housings (45 and 47) respectively. The housings (45 and 47) are connected to opposite sides of the second mount section 20. The bars (41 and 42) are connected to their respective housings by flexure webs (59). Transducers (71) are located in proximity to the bars for detecting movement of the bars to in turn enable the gravitational gradient tensor to be measured.

Claims

1. A gravity gradiometer for measuring components of the gravity gradient tensor, comprising:

a sensor for measuring the components of the gravity gradient tensor;

a mounting supporting the sensor for rotation about three substantially orthogonal axes;

a stabilizing mechanism for stabilizing the mounting by adjusting the mounting about at least one of the axes; and

an angular accelerometer for providing a signal indicative of a rotation of the sensor to cause the stabilizing mechanism to apply a force to the mounting to counteract that rotation of the sensor and stabilize the mounting and the sensor,

wherein the sensor is an orthogonal quadrupole responder comprising two sensor bars arranged orthogonal to one another, each sensor bar being supported on the mounting for pivoting movement about one of the axes, and

wherein the angular accelerometer is supported on the mounting for movement with the sensor and comprises a pivoting accelerometer mass having a zero quadrupole moment so the accelerometer mass is not sensitive to the gravity gradient and centrifugal force errors, whereby the angular accelerometer is configured to produce a signal indicative only of a rotation of the sensor to be counteracted by the stabilizing mechanism.

2. The gravity gradiometer of claim 1 wherein the sensor bars are positioned in sensor housings carried on the mounting and coupled to the sensor housings by respective sensor flexure webs for rotation about the one axis.

3. The gravity gradiometer of claim 1 wherein the accelerometer mass is positioned in an accelerometer housing carried on the mounting an coupled to the accelerometer housing by an accelerometer flexure web.

4. The gravity gradiometer of claim 3 wherein the accelerometer mass is formed by a cut through the accelerometer housing except for where the accelerometer mass connects to the accelerometer housing by the accelerometer flexure web.

5. The gravity gradiometer of claim 1 wherein the accelerometer mass is of chevron shape.

6. The gravity gradiometer of claim 1 wherein the angular accelerometer is one of a plurality of such accelerometers for providing signals indicative of rotations of the sensor about more than one of said three orthogonal axes.