IP Library › Granted Patent US 10,683,106
Granted Patent B2
US 10,683,106 · App. 15/927,777 · Granted Jun 16, 2020

Structural health monitoring systems

Inventor: Christopher M. Minnella (Pittsford, NY)
Assignee: SIKORSKY AIRCRAFT CORPORATION
B64F5/60B64C27/46G01K1/14G01K11/12G01N25/72
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Quick Facts
Patent No.
US 10,683,106
App. No.
15/927,777
Granted
Jun 16, 2020
Kind
B2
Abstract

In accordance with at least one aspect of this disclosure, a structure can include a body, and one or more thermal sheet sensors disposed on or within the body. The one or more thermal sheet sensors can be configured to receive heat from the body to allow sensing of thermal flux through the body to monitor and/or determine a condition of the structure.

Claims (15)

1. A structure, comprising:

a body; and

one or more thermal sheet sensors disposed on or within the body and configured to receive heat from the body to allow sensing of thermal flux through the body to monitor and/or determine a condition of the structure, wherein the structure is a helicopter rotor blade having a laminated structure.

2. The structure of claim 1 , further comprising one or more thermal sheet heaters disposed on or within the body to provide heat to the body to allow thermal transient evaluation using the one or more thermal sheet sensors.

3. The structure of claim 1 , wherein the one or more sheet sensors are disposed on the outer surface of the structure.

4. The structure of claim 1 , wherein the one or more sheet sensors include a temperature sensitive coating that changes visual color based on the temperature.

5. The structure of claim 1 , wherein the one or more thermal sheet sensors are disposed along the entire length of the structure.

6. The structure of claim 1 , wherein the one or more thermal sheet sensors are disposed in predetermined locations of the structure that are damage prone.

7. The structure of claim 1 , wherein the one or more sensors are permanently attached on or within the structure.

8. The structure of claim 1 , further comprising a wireless communication system connected to the one or more thermal sheet sensors to allow wireless data communication of the thermal sheet sensors with a computerized device.

9. The structure of claim 1 , wherein the one or more thermal sheet sensors are disposed within the laminated structure of the rotor blade.

10. The structure of claim 9 , further comprising one or more thermal sheet heaters disposed within the laminated structure of the rotor blade to provide heat to the body to allow thermal transient evaluation using the one or more thermal sheet sensors.

11. The structure of claim 1 , further comprising a computerized device disposed on or within the structure and operatively connected to the one or more thermal sheet sensors to receive signals therefrom, and to process the signals to determine structural health.

12. The structure of claim 11 , wherein the computerized device is configured to control one or more thermal sheet heaters disposed on or within the body to output a predetermined heat.

13. The structure of claim 12 , wherein the computerized device is configured to compare thermal transient data, based on the location of the thermal signals on the thermal sheet sensor, to expected thermal transient data for a predetermined heat input.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 29, 2018
From: MINNELLA, CHRISTOPHER M.
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 046732/0776 →
Continuity (1)
Related Publication 20190291897A1 · Sep 26, 2019
Cited By (1)
US 12,705,721