Load assembly and unmanned aerial vehicle
US-11155344-B2 · Oct 26, 2021 · US
US9611024B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9611024-B2 |
| Application number | US-201113197713-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 3, 2011 |
| Priority date | Aug 3, 2011 |
| Publication date | Apr 4, 2017 |
| Grant date | Apr 4, 2017 |
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Systems and methods for measuring a volume of a ballonet are provided. In some aspects, the system may include a plurality of sensors configured to transmit a plurality of signals toward an interior surface of the ballonet and to receive the plurality of signals reflected off of the interior surface of the ballonet, a distance calculating module configured to calculate a plurality of distances from the plurality of sensors to the interior surface of the ballonet using the received plurality of signals, and a mapping module configured to create a three-dimensional surface using the calculated plurality of distances. The system may further include a measurement module configured to calculate the volume of the ballonet using the three-dimensional surface.
Opening claim text (preview).
What is claimed is: 1. A system for measuring a volume of a ballonet, the system comprising: a plurality of reflectors arranged in a grid pattern along a non-rigid interior surface of the ballonet and configured to reflect a plurality of signals directed at the plurality of reflectors; a plurality of sensors mounted on a rigid interior surface of the ballonet and configured to transmit the plurality of signals toward the non-rigid interior surface of the ballonet and to receive the plurality of signals reflected off of the plurality of reflectors while the ballonet is not fully pressurized and comprises a folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet; and one or more processors configured to: calculate, while the ballonet is not fully pressurized and comprises the folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet, a plurality of distances from the plurality of sensors to the plurality of reflectors using the received-plurality of signals; create a three-dimensional surface using the calculated plurality of distances; and calculate the volume of the ballonet using the three-dimensional surface. 2. The system of claim 1 , wherein the plurality of sensors comprise laser based sensors. 3. The system of claim 1 , wherein the plurality of sensors comprise radio frequency based sensors. 4. The system of claim 1 , wherein the plurality of sensors comprise sonic based sensors. 5. The system of claim 1 , wherein the one or more processors are further configured to: detect the folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet based on comparing data received for the portion by a first sensor of the plurality of sensors with data received for the portion by a second sensor of the plurality of sensors; and exclude erroneous distances corresponding to the folded, wrinkled or creased portion from the calculated plurality of distances. 6. The system of claim 1 , wherein the one or more processors are further configured to calculate the volume of the ballonet in real time. 7. The system of claim 1 , wherein the one or more processors are further configured to calculate the volume of the ballonet in a time increment of one second or more. 8. The system of claim 1 , wherein the one or more processors are further configured to calculate the volume of the ballonet within 1% of a total volume of the ballonet. 9. The system of claim 1 , wherein the one or more processors are further configured to determine the orientation of the ballonet relative to a plane using the three-dimensional surface and orientation data from gyro instrumentation. 10. The system of claim 9 , wherein the one or more processors are further configured to calculate the center of gravity of the ballonet using the three-dimensional surface and the determined orientation of the ballonet. 11. The system of claim 1 , wherein the one or more processors are further configured to calculate a leakage rate of the ballonet by predicting the volume of the ballonet and determining a difference between the predicted volume of the ballonet and the calculated volume of the ballonet. 12. The system of claim 1 , wherein the one or more processors are further configured to perform statistical checks to determine the reliability of the calculated volume of the ballonet. 13. A method for measuring a volume of a ballonet, the method comprising: transmitting, by a plurality of sensors mounted on a rigid interior surface of the ballonet, a plurality of signals toward a plurality of reflectors arranged in a grid pattern along a non-rigid interior surface of the ballonet; receiving the plurality of signals reflected off of the plurality of reflectors while the ballonet is not fully pressurized and comprises a folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet; calculating, while the ballonet is not fully pressurized and comprises the folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet, a plurality of distances from the plurality of sensors to the plurality of reflectors using the received plurality of signals; creating a three-dimensional surface using the calculated plurality of distances; and calculating the volume of the ballonet using the three-dimensional surface. 14. The method of claim 13 , wherein the plurality of signals comprise light beams. 15. The method of claim 13 , wherein the plurality of signals comprise radio waves. 16. The method of claim 13 , wherein the plurality of signals comprise sound waves. 17. The method of claim 13 , further comprising, after calculating a plurality of distances: detecting the folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet based on comparing data received for the portion by a first sensor of the plurality of sensors with data received for the portion by a second sensor of the plurality of sensors; and excluding erroneous distances corresponding to the folded, wrinkled or creased portion from the calculated plurality of distances. 18. The method of claim 13 , wherein the calculating the volume of the ballonet comprises calculating the volume of the ballonet in real time. 19. The method of claim 13 , wherein the calculating the volume of the ballonet comprises calculating the volume of the ballonet in time increments of one second or more. 20. The method of claim 13 , further comprising determining the orientation of the ballonet relative to a plane using the three-dimensional surface and orientation data from gyro instrumentation. 21. The method of claim 20 , further comprising calculating the center of gravity of the ballonet using the three-dimensional surface and the determined orientation of the ballonet. 22. The method of claim 13 , further comprising calculating a leakage rate of the ballonet by predicting the volume of the ballonet and determining a difference between the predicted volume of the ballonet and the calculated volume of the ballonet. 23. The method of claim 13 , further comprising performing statistical checks to determine the reliability of the calculated volume of the ballonet. 24. A non-transitory machine-readable storage medium encoded with instructions executable by a processing system to perform a method for measuring a volume of a ballonet, the instructions comprising code for: transmitting, by a plurality of sensors mounted on a rigid interior surface of the ballonet, a plurality of signals toward a plurality of reflectors arranged in a grid pattern along a non-rigid interior surface of the ballonet; receiving the plurality of signals reflected off of the plurality of reflectors while the ballonet is not fully pressurized and comprises a folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet; calculating, while the ballonet is not fully pressurized and comprises the folded, wrinkled or creased portion of the non-rigid interior surface of the ballonet, a plurality of distances from the plurality of sensors to the plurality of reflectors using the received plurality of signals; creating a three-dimensional surface using the calculated plurality of distances; and calculating the volume of the ballonet using the three-dimensional surface. 25. The non-transitory machine-readable storage medium of claim 24 , further comprising code for: detecting the folded, wri
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