Gravity gradiometer system with spherical air bearing based platform
US-2016363689-A1 · Dec 15, 2016 · US
US10060475B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10060475-B2 |
| Application number | US-201414582648-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 24, 2014 |
| Priority date | Dec 24, 2014 |
| Publication date | Aug 28, 2018 |
| Grant date | Aug 28, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
An example method includes: for a component supported by an air bearing, detecting a speed of movement of the component relative to a predefined location, the air bearing generating an air flow to elevate the component relative to a ground plane; and controlling the air bearing based, at least in part, on the speed detected.
Opening claim text (preview).
What is claimed is: 1. A method comprising: for a component supported by an air bearing, detecting a speed of movement of the component relative to a predefined location, the air bearing generating an air flow to elevate the component relative to a ground plane; determining that the speed of movement of the component is greater than a threshold; determining that the component is within a geographic area associated with the predefined location; and controlling the air bearing based, at least in part, on the speed detected, wherein controlling the air bearing comprises reducing an air flow of the air bearing so as to reduce the speed of movement of the component. 2. The method of claim 1 , further comprising restricting a rate at which the air flow is reduced. 3. A method comprising: for a component supported by an air bearing, detecting a speed of movement of the component relative to a predefined location, the air bearing generating an air flow to elevate the component relative to a ground plane; determining that the speed of movement of the component is less than a threshold; determining that the component is within a geographic area associated with the predefined location; and controlling the air bearing based, at least in part, on the speed detected, wherein controlling the air bearing comprises maintaining an air flow of the air bearing so as to maintain the speed of movement of the component. 4. A method comprising: for a component supported by an air bearing, detecting a speed of movement of the component relative to a predefined location, the air bearing generating an air flow to elevate the component relative to a ground plane; determining that the speed of movement of the component is greater than a threshold; and determining that the component is within a geographic area associated with the predefined location; and controlling the air bearing based, at least in part, on the speed detected, wherein controlling the air bearing comprises maintaining an air flow of the air bearing so as to maintain the speed of movement of the component. 5. A method comprising: for a component supported by an air bearing, detecting a speed of movement of the component relative to a predefined location, the air bearing generating an air flow to elevate the component relative to a ground plane; detecting a position of the component relative to the predefined location; and controlling the air bearing based the speed detected and on the position; wherein the position is detected relative to a mat having position markers. 6. The method of claim 5 , wherein the position markers comprise concentric shapes having pitches that decrease at increasing distances from a center. 7. The method of claim 5 , wherein the position markers are detected optically. 8. The method of claim 5 , wherein the position is detected using radio frequency detection, where a transmitter is at the component and a receiver is at the predefined location, or where the receiver is at the component and the transmitter is at the predefined location. 9. The method of claim 5 , wherein the position is detected using ultrasound. 10. The method of claim 5 , wherein the position is detected using a tether and a potentiometer, or tethers and potentiometers, the tether or tethers being connected to the component and being configured to move with the component; and wherein a length of the tether corresponds to resistance measured by the potentiometer, the position being based on the length of the tether, or wherein lengths of the tethers correspond to resistances measured by the potentiometers, the position being based on the lengths of the tethers. 11. The method of claim 5 , wherein the position is detected using a global positioning system. 12. The method of claim 1 , 3 , 4 , or 5 , wherein the component comprises a manipulator for holding a test head. 13. The method of claim 1 , 3 , 4 , or 5 , wherein the component comprises a combined test head and manipulator. 14. The method of claim 1 , 3 , or 4 , wherein determining that the component is within the geographic area is performed using radio frequency detection, where a transmitter is at the component and a receiver is at a predefined location, or where the receiver is at the component and the transmitter is at the predefined location. 15. The method of claim 1 , 3 , or 4 , wherein determining that the component is within the geographic area is performed using ultrasound. 16. The method of claim 1 , 3 , or 4 , wherein determining that the component is within the geographic area is performed using a tether and a potentiometer, or tethers and potentiometers, the tether or tethers being connected to the component and being configured to move with the component; and wherein a length of the tether corresponds to resistance measured by the potentiometer, the position being based on the length of the tether, or wherein lengths of the tethers correspond to resistances measured by the potentiometers, the position being based on the lengths of the tethers. 17. The method of claim 1 , 3 , or 4 , wherein determining that the component is within the geographic area is performed using a global positioning system. 18. A system comprising: a component; an air bearing to support the component, the air bearing being configured to generate an air flow to elevate the component relative to a ground plane; a detector to detect a speed of movement of the component on the air bearing; and a controller to output signals for controlling the air bearing based, at least in part, on the speed detected; wherein the controller is configured to perform operations comprising: determining that the speed of movement of the component is greater than a threshold; and determining that the component is within a geographic area; wherein controlling the air bearing comprises reducing an air flow of the air bearing so as to reduce the speed of movement of the component. 19. The system of claim 18 , wherein controlling the air bearing comprises restricting a rate at which the air flow is reduced. 20. A system comprising: a component; an air bearing to support the component, the air bearing being configured to generate an air flow to elevate the component relative to a ground plane; a detector to detect a speed of movement of the component on the air bearing; and a controller to output signals for controlling the air bearing based, at least in part, on the speed detected; wherein the controller is configured to perform operations comprising: determining that the speed of movement of the component is less than a threshold; and determining that the component is within a geographic area; wherein controlling the air bearing comprises modulating air flow of the air bearing so as to reduce the speed of movement of the component by allowing a braking surface to contact a supporting surface of the air bearing. 21. A system comprising: a component; an air bearing to support the component, the air bearing being configured to generate an air flow to elevate the component relative to a ground plane; a detector to detect a speed of movement of the component on the air bearing; and a controller to output signals for controlling the air bearing based, at least in part, on the speed detected; wherein the controller is configured to perform operations comprising: determining that the speed of movement of the component is greater than a threshold; and determining that the component is withi
the gas being supplied under pressure, e.g. aerostatic bearings · CPC title
using optical means, i.e. using infrared, visible, or ultraviolet light (G01P3/80 takes precedence {; by reflection of waves G01S17/58}) · CPC title
delivered by photo-electric detectors · CPC title
Devices characterised by the use of mechanical means · CPC title
using electric or magnetic means (G01P3/80 takes precedence; measuring short time intervals G04F8/00, G04F10/00) · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.