Health monitoring of aircraft landing gear mechanical structures

1. A method, comprising:

calibrating a sensor for measuring a condition of a stop joint formed by a first stop pad and a second stop pad of a levered landing gear against a nominal condition of at least one of the first stop pad and the second stop pad, wherein the first stop pad is included in a first shock strut of the levered landing gear, and the second stop pad is included in a truck lever of the levered landing gear that is connected to the first shock strut and a second shock strut disposed concentrically along a longitudinal axis of the first shock strut to extend along a shared extension axis;

monitoring, by the sensor, a current condition of the at least one of the first stop pad and the second stop pad from the nominal condition;

determining whether a non-conformance from the nominal condition of the at least one of the first stop pad and the second stop pad has been detected by the sensor for the current condition; and

in response to determining that the non-conformance has been detected, generating an alert.

2. The method of claim 1 , further comprising, in response to determining that the non-conformance has been detected:

capturing an image via a camera focused on the at least one of the first stop pad and the second stop pad;

storing the image for retrieval to corroborate the determination that the non-conformance has been detected; and

displaying the image to a user in response to the user acknowledging the alert.

3. The method of claim 1 , wherein the condition includes at least one of:

a thickness of the second stop pad measured by the sensor via ultrasound;

a gap distance between the first stop pad and the second stop pad measured by the sensor via an eddy current;

a gap distance between the first stop pad and the second stop pad measured by the sensor via range finding;

a visual indication of debris in the stop joint measured by the sensor via image recognition;

a visual indication of corrosion in the stop joint measured by the sensor via image recognition; and

a visual indication of surface marring in the stop joint measured by the sensor via image recognition.

4. The method of claim 1 , wherein the sensor is an eddy current sensor mounted in a fixed position within the first stop pad.

5. The method of claim 1 , wherein the sensor is an ultrasound sensor held in contact with a second mounting surface of one of the first stop pad and the second stop pad via an actuator member.

6. A method, comprising:

calibrating a sensor for measuring a condition of a stop joint formed by a first stop pad and a second stop pad of a levered landing gear against a nominal condition of at least one of the first stop pad and the second stop pad;

monitoring, by the sensor, a current condition of the at least one of the first stop pad and the second stop pad from the nominal condition;

determining whether a non-conformance from the nominal condition of the at least one of the first stop pad and the second stop pad has been detected by the sensor for the current condition; and

in response to determining that the non-conformance has been detected:

generating an alert;

capturing an image via a camera focused on the at least one of the first stop pad and the second stop pad;

storing the image for retrieval to corroborate the determination that the non-conformance has been detected; and

displaying the image to a user in response to the user acknowledging the alert.

7. The method of claim 6 , wherein the condition includes at least one of:

a thickness of the second stop pad measured by the sensor via ultrasound;

a gap distance between the first stop pad and the second stop pad measured by the sensor via an eddy current;

a gap distance between the first stop pad and the second stop pad measured by the sensor via range finding;

a visual indication of debris in the stop joint measured by the sensor via image recognition;

a visual indication of corrosion in the stop joint measured by the sensor via image recognition; and

a visual indication of surface marring in the stop joint measured by the sensor via image recognition.

8. The method of claim 6 , wherein the sensor is an eddy current sensor mounted in a fixed position within the first stop pad.

9. The method of claim 6 , wherein the sensor is an ultrasound sensor held in contact with a second mounting surface of one of the first stop pad and the second stop pad via an actuator member.

10. The method of claim 6 , wherein the first stop pad is included in a first shock strut of the levered landing gear, and the second stop pad is included in a truck lever of the levered landing gear that is connected to the first shock strut and a second shock strut disposed concentrically along a longitudinal axis of the first shock strut to extend along a shared extension axis.

11. A method comprising:

monitoring, by a sensor, a condition of at least one of a first stop pad and a second stop pad in a levered landing gear, wherein the first stop pad is included in a first shock strut of the levered landing gear, and the second stop pad is included in a truck lever of the levered landing gear that is connected to the first shock strut and a second shock strut disposed concentrically along a longitudinal axis of the first shock strut to extend along a shared extension axis; and

in response to determining that the sensor has detected a non-conformance in least one of the first stop pad and the second stop pad, generating an alert.

12. The method of claim 11 , further comprising, in response to determining that the non-conformance has been detected:

capturing an image via a camera focused on the at least one of the first stop pad and the second stop pad;

storing the image for retrieval to corroborate the determination that the non-conformance has been detected; and

displaying the image to a user in response to the user acknowledging the alert.

13. The method of claim 11 , wherein the sensor is an eddy current sensor mounted in a fixed position within the first stop pad to measure a thickness of the first stop pad or a combined thickness of the first stop pad and second stop pad.

14. The method of claim 11 , wherein the sensor is an ultrasound sensor held in contact with a second mounting surface of one of the first stop pad and the second stop pad via an actuator member.

15. The method of claim 11 , wherein the sensor is an eddy current sensor and the condition measures a gap distance between the first stop pad and the second stop pad.

16. The method of claim 11 , wherein the sensor is a range finder and the condition measures a gap distance between the first stop pad and the second stop pad.

17. The method of claim 11 , wherein the sensor is a camera and the condition measures, via image recognition, a visual indication of debris in a stop joint between the first stop pad and the second stop pad.

18. The method of claim 11 , wherein the sensor is a camera and the condition measures, via image recognition, a visual indication of corrosion in a stop joint between the first stop pad and the second stop pad.

19. The method of claim 11 , wherein the sensor is a camera and the condition measures, via image recognition, a visual indication of surface marring in a stop joint between the first stop pad and the second stop pad.

20. The method of claim 11 , further comprising:

calibrating the sensor, before monitoring the condition of the at least one of the first stop pad and the second stop pad in the levered landing gear, wherein the sensor is calibrated for measuring the condition against a nominal condition of at least one of the first stop pad and the second stop pad.