Gravity gradiometer system with spherical air bearing based platform

Patent metadata

Field	Value
Publication number	US-9891341-B2
Application number	US-201414147899-A
Country	US
Kind code	B2
Filing date	Jan 6, 2014
Priority date	Jan 6, 2014
Publication date	Feb 13, 2018
Grant date	Feb 13, 2018

Abstract

A non-contacting spherical air bearing-based stable platform for use by a gravity gradiometer instrument (GGI) is provided by attaching a spherical ball-shaped bearing to a rotational stage of the GGI and integrating a concave spherical cup in the linear stage and mounting base assembly of the GGI which is fixedly attached to a host vehicle or platform. The spherical cup supports the spherical ball-shaped bearing on a thin cushion of air provided by a source of compressed air or gas at the concave surface of the spherical cup. The spherical ball-shaped bearing is supported, providing three degrees of rotational freedom of motion without the need for slip rings, flex capsules, races, or mechanical bearings, thereby reducing or eliminating gradient disturbance signals owing to parasitic torques and jitter in the output of the accelerometers of the GGI.

First claim

What is claimed is:

1. A gravity gradient instrument (GGI) comprising:
a linear stage and mounting base assembly fixedly attached to a host vehicle or platform;
a rotational stage;
a spherical air bearing comprising an upper half comprising a spherical ball-shaped bearing of said rotational stage, and a lower half comprising a spherical cup of said linear stage, wherein said spherical ball-shaped bearing is supported by said spherical cup by a thin cushion of air such that said rotational stage rotates relative to said linear stage without contacting said linear stage and is rotationally decoupled from the linear stage; and
at least one alignment sensor configured to measure a relative position and/or alignment of said linear stage relative to said rotational stage, and send a signal based on the relative position and/or alignment of said linear stage relative to said rotational stage to a processor for aligning the relative position and/or alignment of said linear stage relative to said rotational stage.

2. The GGI of claim 1 , wherein said linear stage and mounting base assembly further comprises:
a mounting base fixedly attached to said host vehicle or platform; and
a linear stage coupled to said base by a suspension.

3. The GGI of claim 2 , wherein said suspension comprises a passive suspension.

4. The GGI of claim 3 , wherein said passive suspension includes a mechanical helical spring and a damper element.

5. The GGI of claim 3 , wherein said passive suspension includes a wire rope suspension.

6. The GGI of claim 3 , wherein said passive suspension includes an air spring having a viscoelastic damper.

7. The GGI of claim 2 , wherein said suspension comprises an active suspension.

8. The GGI of claim 7 , wherein said active suspension includes at least one mechanical actuator.

9. The GGI of claim 1 , further comprising:
a source of compressed air; and
a pneumatic line having a first end coupled to said source of compressed air, and a second end coupled to an underside of said spherical cup of said linear stage.

10. The GGI of claim 9 , wherein said pneumatic line allows compressed air to pass through a concave surface of said spherical cup from said second end of said pneumatic line, through at least one aperture in said concave surface of said spherical cup.

11. The GGI of claim 1 , wherein said rotational stage further comprises:
an instrument block including a plurality of accelerometers;
a battery power supply;
a mass storage device for storing data relating to outputs of said plurality of accelerometers;
a processor in communication with said mass storage device for processing data relating to outputs of said plurality of accelerometers; and
an enclosure for housing said instrument block, said battery power supply, said mass storage device, and said processor.

12. The GGI of claim 11 , wherein said enclosure is configured as a magnetic shield for said plurality of accelerometers, and wherein said enclosure provides a temperature controlled internal volume housing said plurality of accelerometers.

13. The GGI of claim 1 , said rotational stage further comprising at least one non-contacting spherical actuator configured to provide relative alignment between said noncontacting rotational stage and said linear stage.

14. The GGI of claim 1 further comprising an umbilical cable configured to cross an interface between said rotational stage and said linear stage, said umbilical cable configured to have minimum stiffness and a minimized routing path and effective moment arm to said rotational stage.

15. The GGI of claim 1 , wherein said alignment sensor is an optical sensor.

16. The GGI of claim 15 wherein said optical sensor is a laser coupled to said linear stage and a reflector is coupled to said rotational stage.

17. The GGI of claim 1 , wherein said alignment sensor is an electromagnetic sensor.

18. The GGI of claim 1 , wherein said linear stage comprises a brake mechanism which when activated includes a brake member associated with said linear stage that contacts a rotational skirt coupled to said rotational stage, said contact causing said rotational stage to stop rotating.

19. A gravity gradient instrument (GGI) comprising:
a linear stage and mounting base assembly fixedly attached to a host vehicle or platform;
a rotational stage;
a spherical air bearing comprising an upper half comprising a spherical ball-shaped bearing of said rotational stage, and a lower half comprising a spherical cup of said linear stage, wherein said spherical ball-shaped bearing is supported by said spherical cup by a thin cushion of air such that said rotational stage rotates relative to said linear stage without contacting said linear stage and is rotationally decoupled from the linear stage; and
wherein said rotational stage further comprises at least one non-contacting spherical actuator configured to provide relative alignment between said noncontacting rotational stage and said linear stage.

20. A gravity gradient instrument (GGI) comprising:
a linear stage and mounting base assembly fixedly attached to a host vehicle or platform;
a rotational stage;
a spherical air bearing comprising an upper half comprising a spherical ball-shaped bearing of said rotational stage, and a lower half comprising a spherical cup of said linear stage, wherein said spherical ball-shaped bearing is supported by said spherical cup by a thin cushion of air such that said rotational stage rotates relative to said linear stage without contacting said linear stage and is rotationally decoupled from the linear stage; and
wherein said linear stage further comprises a brake mechanism which when activated includes a brake member associated with said linear stage that contacts a rotational skirt coupled to said rotational stage, said contact causing said rotational stage to stop rotating.

Assignees

• Lockheed Corp

Inventors

• Meyer Thomas J

Classifications

• G01V7/16 Primary

  specially adapted for use on moving platforms, e.g. ship, aircraft · CPC title

• G01V7/08

  using balances · CPC title

• F16C32/0614

  the gas being supplied under pressure, e.g. aerostatic bearings · CPC title

• F16C32/0696

  for both radial and axial load · CPC title

• F16C2370/00

  Apparatus relating to physics, e.g. instruments · CPC title