UAV for continuous ultrasound testing (UT) scans with a flexible payload

Patent metadata

Field	Value
Publication number	US-12084182-B2
Application number	US-202117444515-A
Country	US
Kind code	B2
Filing date	Aug 5, 2021
Priority date	Aug 5, 2021
Publication date	Sep 10, 2024
Grant date	Sep 10, 2024

Abstract

An unmanned aerial vehicle (UAV) includes a flexible holder retaining a plurality of probes. The flexible holder is deformable to arrange the probes around a portion of a structure, allowing the probes to scan the portion of the structure. At least one of the plurality of probes is an ultrasonic test (UT) probe to scan the portion of the structure with ultrasonic waves.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) for probing a portion of a structure, comprising:
a chassis;
a plurality of propellers mounted to the chassis;
a plurality of probes that collect data;
a processor configured by code executing therein to generate a first signal and a second signal; and
a flexible holder mounted to the chassis and adapted to receive the first and second signals from the processor and to retain the plurality of probes,
wherein the flexible holder, responsive to the first signal, is configurable by the processor to be set in a first configuration in which the flexible holder is pressed against the portion of the structure,
wherein the flexible holder in the first configuration, responsive to the second signal, is configurable by the processor to deform from the first configuration into a second configuration in which the plurality of probes is arranged around the portion of the structure,
wherein the plurality of probes scan the portion of the structure, and
wherein the flexible holder in the second configuration, responsive to the first signal, is configurable by the processor to deform back from the second configuration into the first configuration.

2. The UAV of claim 1 , wherein the processor is configured by the code to enable a first flight mode in which the propellers move the UAV while the flexible holder is in the first configuration and a second flight mode in which the propellers move the UAV solely along a length of the portion of the structure while the flexible holder is in the second configuration, wherein the probes collect data when the UAV is in the second flight mode.

3. The UAV of claim 1 , wherein the flexible holder is disposed on a top portion of the chassis.

4. The UAV of claim 1 , wherein the flexible holder is disposed on a bottom portion of the chassis.

5. The UAV of claim 1 , wherein the flexible holder is disposed on a side portion of the chassis.

6. The UAV of claim 1 , wherein at least one of the plurality of probes is an ultrasonic test (UT) probe.

7. The UAV of claim 6 , wherein the at least one of the plurality of probes is a dry coupled UT probe.

8. A payload of an unmanned aerial vehicle (UAV) of the type arranged to probe a portion of a structure, comprising:
a plurality of probes that collect data;
a processor configured by code executing therein to generate a first signal and a second signal; and
a flexible holder mounted to a chassis of the UAV and adapted to receive the first and second signals from the processor and to retain the plurality of probes,
wherein the flexible holder, responsive to the first signal, is configurable by the processor to be set in a first configuration in which the flexible holder is pressed against the portion of the structure,
wherein the flexible holder in the first configuration, responsive to the second signal, is configurable by the processor to deform from the first configuration into a second configuration in which the plurality of probes is arranged around the portion of the structure,
wherein the plurality of probes scan the portion of the structure, and
wherein the flexible holder in the second configuration, responsive to the first signal, is configurable by the processor to deform back from the second configuration into the first configuration.

9. The payload of claim 8 , wherein the processor is configured by the code to enable a first flight mode in which the propellers move the UAV while the flexible holder is in the first configuration and a second flight mode in which the propellers move the UAV solely along a length of the portion of the structure while the flexible holder is in the second configuration, wherein the probes collect data when the UAV is in the second flight mode.

10. The payload of claim 8 , wherein the flexible holder is disposed on a top portion of the chassis.

11. The payload of claim 8 , wherein the flexible holder is disposed on a bottom portion of the chassis.

12. The payload of claim 8 , wherein the flexible holder is disposed on a side portion of the chassis.

13. The payload of claim 8 , wherein at least one of the plurality of probes is an ultrasonic test (UT) probe.

14. The payload of claim 13 , wherein the at least one of the plurality of probes is a dry coupled UT probe.

15. A method for probing a portion of a structure using an unmanned aerial vehicle (UAV), comprising:
providing a processor configured by code executing therein to generate a first signal and a second signal;
providing a payload with a flexible holder mounted to a chassis of the UAV;
providing a plurality of probes on the flexible holder;
advancing the UAV to a first location along the structure;
receiving the first signal at the flexible holder;
responsive to the first signal, setting the flexible holder to be in a first configuration;
pressing the flexible holder in the first configuration against the portion of the structure at the first location;
receiving the second signal at the flexible holder in the first configuration;
responsive to the second signal, deforming the flexible holder from the first configuration to a second configuration to arrange the plurality of probes around the structure;
scanning the structure at the first location using the plurality of probes;
navigating the UAV to at least a second location along the structure;
repeating the scanning step at at least the second location;
receiving the first signal at the flexible holder in the second configuration; and
responsive to the first signal, deforming the flexible holder back from the second configuration to the first configuration.

16. The method of claim 15 , wherein the navigating step is performed while the flexible holder remains in the deformed second configuration.

17. The method of claim 15 , further comprising:
disposing the payload on a top portion of the chassis.

18. The method of claim 15 , further comprising:
disposing the payload on a bottom portion of the chassis.

19. The method of claim 15 , further comprising:
disposing the payload on a side portion of the chassis.

20. The method of claim 15 , wherein the scanning further comprises:
scanning the portion of the structure using an ultrasonic test (UT) probe as at least one of the plurality of probes.

Assignees

• Saudi Arabian Oil Co
• Univ King Abdullah Sci & Tech

Inventors

• Abdellatif Fadl
• Shamma Jeff S
• Shaqaq Sultan
• Arab Abdullah
• Alkhder Abdullah A
• Patel Sahejad

Classifications

• B64U2101/00

  UAVs specially adapted for particular uses or applications · CPC title

• B64U10/13 Primary

  Flying platforms · CPC title

• G01N29/2475

  Embedded probes, i.e. probes incorporated in objects to be inspected · CPC title

• G01N29/28

  providing acoustic coupling {, e.g. water (impedance matching G10K11/02)} · CPC title

• G01N2291/106

  one or more transducer arrays · CPC title