Systems and methods for monitoring composite structure

Patent metadata

Field	Value
Publication number	US-12050146-B2
Application number	US-202318375414-A
Country	US
Kind code	B2
Filing date	Sep 29, 2023
Priority date	Apr 6, 2021
Publication date	Jul 30, 2024
Grant date	Jul 30, 2024

Abstract

Disclosed is a sensor for monitoring a composite structure. The sensor includes multiple sensing elements of different sizes, each configured for different respective monitoring tasks. Also disclosed are methods of fabricating the sensor, designing and manufacturing the sensor, and attaching the sensor to the composite structure.

First claim

The invention claimed is:

1. A monitoring system comprising:
a plurality of broadband piezoelectric sensors connected to a composite cylinder having a laminate structure, the broadband piezoelectric sensors being sensitive to an out-of-plane displacement of the laminate structure of the composite cylinder, and being configured to detect deformation data associated with the composite cylinder;
a controller communicatively coupled to the plurality of broadband piezoelectric sensors and configured to:
receive, from the plurality of broadband piezoelectric sensors, the detected deformation data associated with the composite cylinder when the composite cylinder is impacted by an object,
determine an estimated impact location on the composite cylinder based on arrival times from each broadband piezoelectric sensor of the detected deformation data,
determine a direct wave energy from the object based on the detected deformation data when the composite cylinder is impacted by the object, the direct wave energy being determined based on a direct arrival time of a slowest moving wave component of interest from the estimated impact location and a voltage detected at each of the plurality of broadband piezoelectric sensors,
normalize the direct wave energy for propagation effect based on propagation distance to determine an impact energy corresponding to the impact of the object to the composite cylinder at the impact location, the normalization reducing false triggers by mitigating reflections and wrapping waves, and
communicate a notification when the impact energy exceeds a threshold.

2. The system of claim 1 , wherein the controller is configured to communicate the notification to at least one of an ECU of a vehicle for activating a light indicating inspection of the composite cylinder or a non-transitory memory for updating a stored state of the composite cylinder.

3. The system of claim 1 , wherein the plurality of broadband piezoelectric sensors each have channels formed by dicing a piezoelectric material in a plurality of directions, the plurality of broadband piezoelectric sensors configured to conform to a shape of the composite cylinder,
wherein the channels of the piezoelectric material are filled with resin configured to transition to a malleable state when a temperature of the resin is above a threshold temperature, and
wherein the piezoelectric material is located between a positive electrode and a ground electrode.

4. The system of claim 3 , wherein each of the plurality of broadband piezoelectric sensors further includes a first polyimide film located above the positive electrode and a second polyimide film located below the ground electrode.

5. The system of claim 1 , wherein the plurality of broadband piezoelectric sensors are further configured to communicate deformation data detected by the plurality of broadband piezoelectric sensors to a filling controller as the composite cylinder is filled with a fluid, causing a safety action to be immediately performed when the filling controller detects damage to the composite cylinder based on the deformation data.

6. The system of claim 5 , wherein the filling controller detects the damage to the composite cylinder as the composite cylinder is filled with the fluid based on a modal acoustic emission inspection.

7. The system of claim 5 , wherein the safety action includes at least one of shutting a valve to prevent filling of the composite cylinder, providing a notification on a speaker or a display screen, or adjusting the valve to direct the fluid to a surge tank.

8. The system of claim 5 , wherein the filling controller detects the damage to the composite cylinder as the composite cylinder is filled with the fluid when one or more indicators exceed a respective predetermined threshold.

9. The system of claim 8 , wherein the one or more indicators include at least one of a fiber tow fracture indicator corresponding to detected fiber tow fracture events being quantified and compared to a fiber tow fracture threshold, an instability indicator corresponding to instability within a local volume of material above an instability threshold, a delamination event indicator corresponding to delamination of one or more layers of the composite cylinder above a delamination threshold, a damage mechanism indicator corresponding to damage mechanisms accumulated in the local volume of material above a damage mechanism threshold, or a fretting emission indicator corresponding to fretting emission above a fretting emission threshold based on a laminate composition of the composite cylinder.

10. A method comprising:
detecting, by a plurality of broadband piezoelectric sensors connected to a composite cylinder having a laminate structure, deformation data associated with the composite cylinder, the broadband piezoelectric sensors being sensitive to an out-of-plane displacement of the laminate structure of the composite cylinder;
determining, by a controller communicatively coupled to the plurality of broadband piezoelectric sensors, an estimated impact location on the composite cylinder based on arrival times from each broadband piezoelectric sensor of detected deformation data when the composite cylinder is impacted by an object;
determining, by the controller, a direct wave energy from the object based on the detected deformation data when the composite cylinder is impacted by the object, the direct wave energy being determined based on a direct arrival time of a slowest moving wave component of interest from the estimated impact location and a voltage detected at each of the plurality of broadband piezoelectric sensors;
normalizing, by the controller, the direct wave energy for propagation effect based on propagation distance to determine an impact energy corresponding to the impact of the object to the composite cylinder at the impact location, the normalization reducing false triggers by mitigating reflections and wrapping waves;
communicating, by the controller, a notification when the impact energy exceeds a threshold; and
communicating, by the plurality of broadband piezoelectric sensors to a filling controller, deformation data detected by the plurality of broadband piezoelectric sensors as the composite cylinder is filled with a fluid, causing a safety action to be performed when the filling controller detects damage to the composite cylinder based on the deformation data.

11. The method of claim 10 , wherein the detecting the damage to the composite cylinder as the composite cylinder is filled with the fluid comprises performing, by the filling controller, a modal acoustic emission inspection using the plurality of broadband piezoelectric sensors.

12. The method of claim 10 , wherein the communicating, by the controller, the notification when the impact energy exceeds the threshold comprises communicating the notification to at least one of an ECU of a vehicle for activating a light indicating inspection of the composite cylinder or a non-transitory memory for updating a stored state of the composite cylinder.

13. The method of claim 10 , wherein the safety action includes at least one of shutting a valve to prevent further filling of the composite cylinder, providing a notification on a speaker or a display screen, or adjusting the valve to direct the fluid to a surge tank.

14. The method of claim 10 , wherein the detecting the damage to the composite cylinder as the composite cylinder is filled with the fluid comprises determining whether one or more indicators exceed a respective predetermined threshold.

15. The method of claim 14 , wherein the one or more indicators

Assignees

• Hexagon Technology As

Inventors

• Burks Brian
• Prather Zack
• Eihusen John
• Johnson Joel R
• Perkins Tyler

Classifications

• H10N30/302

  Sensors · CPC title

• H10N30/088

  by cutting or dicing · CPC title

• H10N30/06

  Forming electrodes or interconnections, e.g. leads or terminals · CPC title

• G01N29/14

  using acoustic emission techniques {(echo of particles G01N29/046; measuring mechanical vibrations or acoustic waves in solids in general G01H1/00)} · CPC title

• G01N29/045

  by imparting shocks to the workpiece and detecting the vibrations or the acoustic waves caused by the shocks (measuring resonant frequency G01H13/00; measuring strength properties by application of mechanical stress G01N3/00) · CPC title