Intrinsic gravity gradiometer and gravity gradiometry

Patent metadata

Field	Value
Publication number	US-11002878-B2
Application number	US-201716342926-A
Country	US
Kind code	B2
Filing date	Oct 23, 2017
Priority date	Oct 21, 2016
Publication date	May 11, 2021
Grant date	May 11, 2021

Abstract

A sensing element (10) for an intrinsic gravity gradiometer (IGG) for use in sensing variation in a gravity field at a location. The sensing element (10) is flexible, elongate and has unfixed opposed ends (12, 14) when part of the gravity gradiometer. The sensing element can be a metallic ribbon, and can be mounted by a number e.g. 3 or 5, pivot points or axes 30-40 at each of the opposed sides along the sensing element, with the opposed ends of the sensing element free to move. The pivot points or axes can include pins, preferably cylindrical pins (48) or the sensing element may be etched within the side wall and remain joined to the remainder of the side wall by connections. The sensing element (10) can form part of one or more resonant cavities or wave guide (44, 52-66), such as a side or dividing wall (46) or part thereof. A dual phase bridge (61,612) arrangement can be provided. Electrical current (I) can be injected into the sensing element. Feed forward motion compensation (MC or FFMC) can be applied as part of the determination of the current. Applying electrical current into the opposed longitudinal sides (20, 22), such as right and left sides, of the sensing element, such as a ribbon, can be used for several types of compensation. Displacement of the sensing element can be detected by a resonant cavity, electromagnetic sensor or optical sensor.

First claim

The invention claimed is:

1. An apparatus for measuring direct gravity gradients, the apparatus including: a flexible, elongate sensing element connected to a support at connection points disposed along opposed side edges of the sensing element, the sensing element having opposed free ends, wherein the connection points are provided at a mid-point of the sensing element and intermediate the mid-point and each respective said free end of the sensing element, and the apparatus including at least one displacement sensor configured to detect deflection of the free ends of the sensing element due to a gravitational field acting on the sensing element.

2. The apparatus of claim 1 , further including read-out means provided at or adjacent to edges of the opposed free ends of the sensing element for recording measurements of one or more mechanical displacements of the sensing element.

3. The apparatus of claim 1 , wherein the sensing element is of or incorporates an electrically conductive material, and wherein magnets are provided adjacent to the sensing element between the mid-point connection and the respective connection intermediate the mid-point and the respective free end, and a force is generated on the portion of the sensing element adjacent to the magnets by a current fed through the sensing element, thereby providing a feedback force application means to apply a feedback force at displacement nodes located in between the mid-point connection point and the connection points intermediate the mid-point and the free ends.

4. The apparatus of claim 1 , wherein the sensing element includes a flat strip or ribbon of material.

5. The apparatus of claim 1 , wherein the sensing element is mounted to or integral to the support.

6. The apparatus of claim 1 , wherein the connections points include pins or flexure members.

7. The apparatus of claim 1 , further including wherein the sensing element is of or incorporates an electrically conductive material, and wherein magnets are provided adjacent to the sensing element between the mid-point connection and the respective connection intermediate the mid-point and the respective free end, and a force is generated on the portion of the sensing element adjacent to the magnets by a current fed through the sensing element, thereby providing a modulation means and/or a de-modulation means to respectively modulate and/or demodulate signals resulting from one or more detected direct gravity gradients.

8. The apparatus of claim 1 , wherein the sensing element forms at least part of a side wall of a resonant cavity or wave guide or at least partly fills an opening through a side wall of the resonant cavity or wave guide.

9. The apparatus of claim 1 , wherein the sensing element forms at least part of a partition between two adjacent or conjoined resonant cavities or wave guides.

10. The apparatus of claim 1 , wherein the displacement sensor includes an optical displacement sensor.

11. The apparatus of claim 1 , including an input receiving signals from at least one ancillary device, wherein the sensing element is of or incorporates an electrically conductive material, and wherein magnets are provided adjacent to the sensing element between the mid-point connection and the respective connection intermediate the mid-point and the respective free end, and a force is generated on the portion of the sensing element adjacent to the magnets by a current fed through the sensing element, thereby providing a means to utilize the received signals to generate a feed-forward compensation signal to cancel out certain motion characteristics of the sensing element.

12. The apparatus of claim 11 , wherein the at least one ancillary device includes at least one gyroscope or at least one accelerometer, or a combination of two or more thereof.

13. A method of detecting a gravity gradient including measuring displacement of at least one free end of the sensing element of the apparatus of claim 1 .

14. The method of claim 13 , further including detecting a gravity gradient without spatially repositioning the apparatus.

15. The method of claim 13 , further including detecting a gravity gradient with a single reading from each of at least one displacement sensor(s) at a particular moment in time.

16. The method of claim 13 , wherein displacement of the free ends of the sensing element is used for mechanical displacement measurements while nodes intermediate the free ends of the sensing element are used for applying feedback forces.

17. A method of calibrating, optimising or compensating for gravitational effects on a sensing element of the apparatus of claim 1 includes introducing electrical current into the sensing element to force the sensing element to straighten from a deflected orientation caused by a gravity field.

18. The method of claim 17 , including applying the current separate to or in addition to feed-forward compensation for motion effects of the sensing element.

19. The method of claim 17 , including positioning one or both ends of the sensing element relative to a respective microwave cavity interface spaced at an optimal operating point for maximum sensitivity by controlling the applied current.

Assignees

• Univ Western Australia
• Veryaskin Alexey Vladimirovich

Inventors

• Veryaskin Alexey Vladimirovich
• Bourhill Jeremy Francis
• Ivanov Eugene Nikolay
• Tobar Michael Edmund

Classifications

• G01V7/04 Primary

  Electric, photoelectric, or magnetic indicating or recording means · CPC title

• G01V7/005 Primary

  using a resonating body or device, e.g. string (G01V7/08 - G01V7/12 take precedence; measuring resonant frequency of mechanical vibrations G01H13/00; measuring frequency per se G01R23/00) · CPC title