IP Library Granted Patent US 10,861,147
Granted Patent B2
US 10,861,147 · App. 15/542,358 · Granted Dec 8, 2020

Structural health monitoring employing physics models

Inventor: Hongcheng Wang (Farmington, CT)
Assignee: Sikorsky Aircraft Corporation
G06T7/0008B64F5/60G01B11/24G01M5/0033G01N21/88G01N21/8851G06F30/23G06N7/005G06T7/0004B64D2045/0085G01N2021/8887G06T2207/10016G06T2207/10028G06T2207/20076G06T2207/20221G06T2207/30164
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Quick Facts
Patent No.
US 10,861,147
App. No.
15/542,358
Granted
Dec 8, 2020
Kind
B2
Abstract

A method for detecting structural defects includes generating a first probabilistic map of a critical location of a structural component based on a physics model of the critical location, capturing data of the critical location, generating a second probabilistic map based on an analysis of the captured data of the critical location, aligning the first probabilistic map and the second probabilistic map, combining the aligned first and second probabilistic maps, and determining if the structural component includes a structural defect based on the combined probabilistic maps.

Claims (33)

1. A method for detecting structural defects comprising:

acquiring a physics model of a structural component, the physics model based on geometric properties of the structural component and expected forces on the structural component during operation of the structural component;

generating a first probabilistic map of a critical location of a structural component based on the physics model;

capturing image data of the critical location;

generating a second probabilistic map based on an analysis of the captured image data of the critical location;

aligning the first probabilistic map and the second probabilistic map;

combining the aligned first and second probabilistic maps; and

determining if the structural component includes a structural defect based on the combined probabilistic maps.

2. The method of claim 1 , wherein the physics model is a Finite Element Analysis model.

3. The method of claim 1 , wherein the captured data comprises at least one of a 2D image, a plurality of 2D images, a video, and a 3D point cloud.

4. The method of claim 1 , wherein the step of aligning is based on a transformation obtained by model transformation between at least one of (i) the captured data and a geometric model of the critical location, (ii) the captured data and the physics model, and (iii) the first and second probabilistic maps.

5. The method of claim 1 , wherein the two probabilistic maps are combined based on a Bayesian method.

6. The method of claim 1 , further comprising rejecting false detections of structural defect based on the combined probabilistic maps.

7. The method of claim 1 , further comprising the step of providing an alarm if a structural defect is determined to exist.

8. The method of claim 1 , wherein the structural component is a component of an aircraft.

9. The method of claim 1 , wherein the determining step comprises analyzing values of the combined probabilistic maps.

10. The method of claim 1 , further comprising identifying the critical location based on the physics model.

11. A system for detecting a structural defect defining:

an image processing computer including a processor and memory, the memory having at least one physics model of a structural component stored therein, the physics model based on geometric properties of the structural component and expected forces on the structural component during operation of the structural component;

a camera configured to capture data of the critical location;

wherein the memory includes instructions stored thereon that, when executed by the processor, cause the system to:

generate a first probabilistic map of the critical location based on the physics model;

generate a second probabilistic map based on data captured by the camera;

align the first probabilistic map and the second probabilistic map;

combine the aligned first and second probabilistic maps; and

determine if the structural component includes a structural defect based on the combined probabilistic maps.

12. The system of claim 11 , wherein the physical model is a Finite Element Analysis model.

13. The system of claim 11 , wherein the camera is configured to capture at least one of a 2D image, a plurality of 2D images, a video, and a 3D point cloud.

14. The system of claim 11 , wherein the step of aligning is based on a transformation obtained by model transformation between at least one of (i) the captured data and a geometric model of the critical location, (ii) the captured data and the physics model, and (iii) the first and second probabilistic maps.

15. The system of claim 11 , wherein the two probabilistic maps are combined based on a Bayesian method.

16. The system of claim 11 , wherein the structural component is a component of an aircraft.

17. The system of claim 11 , further comprising an alarm configured to alert when a structural defect is determined to exist.

18. The system of claim 11 , wherein the processor is configured to identify the critical location based on the physics model.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 7, 2017
From: WANG, HONGCHENG
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 042935/0135 →
Continuity (2)
Provisional Application 62102634 · Jan 13, 2015
Related Publication 20180276810A1 · Sep 27, 2018
Cited By (3)
US 12,411,485 US 12,524,872 US 12,705,721