Additive manufactured strain gauge on component surfaces for predictive failure monitoring

Patent metadata

Field	Value
Publication number	US-11719586-B2
Application number	US-202217656532-A
Country	US
Kind code	B2
Filing date	Mar 25, 2022
Priority date	Sep 17, 2018
Publication date	Aug 8, 2023
Grant date	Aug 8, 2023

Abstract

An additively manufactured strain gauge resides on the surface of a component to monitor component fatigue. The strain gauge is additively manufactured, and applied to the curvature of the component surface through either a flexible substrate or through direct printing.

First claim

The invention claimed is:

1. A method of making a strain gauge on a component comprising:
additively manufacturing a dielectric layer directedly onto a first surface of the component, wherein the dielectric layer comprises a non-conductive ink, the dielectric layer is between 0.0005 inches and 0.010 inches thick, and the dielectric layer is printed onto the first surface;
additively manufacturing the strain gauge onto the dielectric layer by printing the strain gauge directly onto the dielectric layer; and
electrically connecting the strain gauge to an external controller, wherein the external controller is configured to read and analyze data produced by the strain gauge and the external controller further comprises a predictive program for predicting when the component will fail based on data produced by the strain gauge;
wherein the component is a portion of a heated floor panel assembly that comprises:
a first stack of structural layers;
a core layer;
a heater layer;
a second stack of structural layers; and
a skin layer,
wherein the dielectric layer is additively manufactured directedly onto a surface of the second stack of structural layers and the strain gauge is additively manufactured directly onto the dielectric layer such that the dielectric layer and strain gauge are positioned between the second stack of structural layers and the skin layer.

2. The method of claim 1 , wherein additively manufacturing the strain gauge comprises printing the strain gauge during manufacture of the component.

3. The method of claim 1 , wherein electrically connecting the strain gauge comprises attaching one or more leads between the strain gauge and the external controller.

4. The method of claim 1 , further comprising encapsulating the strain gauge.

5. The method of claim 1 , wherein additively manufacturing the strain gauge comprises screen printing, ink-jet printing, or aerosol printing the strain gauge.

6. The method of claim 1 , wherein additively manufacturing the strain gauge comprises printing with a carbon loaded or silver loaded ink.

7. A heated floor panel assembly comprising:
a first stack of structural layers;
a core layer;
a heater layer;
a second stack of structural layers; and
a skin layer;
wherein a dielectric layer is additively manufactured directedly on a surface of the second stack of structural layers and a strain gauge is additively manufactured directly on the dielectric layer such that the dielectric layer and strain gauge are positioned between the second stack of structural layers and the skin layer;
wherein the dielectric layer comprises a non-conductive ink and the dielectric layer is between 0.0005 inches and 0.010 inches thick; and
the strain gauge comprises:
an additively manufactured portion comprising:
a conductive ink defining a sensing portion and one or more terminals; and
an encapsulating material; and

one or more flex leads connected to the one or more terminals; and
a controller electrically connected to the additively manufactured portion through the one or more flex leads.

8. The heated floor panel assembly of claim 7 , wherein the controller is configured to read and analyze data produced by the strain gauge and the controller further comprises a predictive program for predicting when the heated floor panel assembly will fail based on data from the strain gauge.

9. A rotor blade assembly comprising:
inner plies,
a heater layer,
an outer erosion shield, and
a nonconductive outer ply,
wherein a dielectric layer additively manufactured directedly on a surface of the outer erosion shield and a strain gauge is additively manufactured directly on the dielectric layer such that the dielectric layer and strain gauge are positioned between the outer erosion shield and the nonconductive outer ply;
wherein the dielectric layer comprising a non-conductive ink, wherein the dielectric layer is between 0.0005 inches and 0.010 inches thick; and
the strain gauge comprises:
an additively manufactured portion comprising:
a conductive ink defining a sensing portion and one or more terminals; and
an encapsulating material; and

one or more flex leads connected to the one or more terminals; and
a controller electrically connected to the additively manufactured portion through the one or more flex leads.

10. The rotor blade assembly of claim 9 , wherein the controller is configured to read and analyze data produced by the strain gauge and the controller further comprises a predictive program for predicting when the rotor blade assembly will fail based on data from the strain gauge.

11. A method of making a strain gauge on a component comprising:
additively manufacturing a dielectric layer directedly onto a first surface of the component, wherein the dielectric layer comprises a non-conductive ink, the dielectric layer is between 0.0005 inches and 0.010 inches thick, and the dielectric layer is printed onto the first surface;
additively manufacturing the strain gauge onto the dielectric layer by printing the strain gauge directly onto the dielectric layer; and
electrically connecting the strain gauge to an external controller, wherein the external controller is configured to read and analyze data produced by the strain gauge and the external controller further comprises a predictive program for predicting when the component will fail based on data produced by the strain gauge;
wherein the component is a portion of a rotor blade that comprises:
inner plies;
a heater layer;
an outer erosion shield; and
a nonconductive outer ply,
wherein the dielectric layer is additively manufactured directedly onto a surface of the outer erosion shield and the strain gauge is additively manufactured directly onto the dielectric layer such that the dielectric layer and strain gauge are positioned between the outer erosion shield and the nonconductive outer ply.

12. The method of claim 11 , wherein additively manufacturing the strain gauge comprises printing the strain gauge during manufacture of the component.

13. The method of claim 11 , wherein electrically connecting the strain gauge comprises attaching one or more leads between the strain gauge and the external controller.

14. The method of claim 11 , further comprising encapsulating the strain gauge.

15. The method of claim 11 , wherein additively manufacturing the strain gauge comprises screen printing, ink-jet printing, or aerosol printing the strain gauge.

16. The method of claim 11 , wherein additively manufacturing the strain gauge comprises printing with a carbon loaded or silver loaded ink.

Assignees

• Goodrich Corp

Inventors

• Mullen James A

Classifications

• G01L1/2287 Primary

  constructional details of the strain gauges (adjustable resistors H01C10/00) · CPC title

• C09D11/52

  Electrically conductive inks · CPC title

• G01L1/22

  using resistance strain gauges · CPC title

• G01L1/2206

  Special supports with preselected places to mount the resistance strain gauges; Mounting of supports · CPC title

• H01B1/22

  the conductive material comprising metals or alloys · CPC title