Signal monitoring system for monitoring strain applied to a composite component

Boeing Aircraft Co. (2015) Signal monitoring system for monitoring strain applied to a composite component. .

Official URL: https://www.uspto.gov

Abstract

A system for estimating a strain of a component and method of estimating strain is provided. The system includes a signal generator configured to transmit a signal toward the component. A sensor is coupled to the component and configured to receive the signal and to generate a reflected signal, The system includes a Fibre Bragg grating filter coupled to the sensor and configured to filter the reflected signal and to generate filtered signal. A detector is coupled to the filter and configured to convert filtered signal to a time domain signal. The system includes an artificial neural network coupled to the detector and configured to process the time domain signal to facilitate estimating the strain of the component.


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Item Type: Patent
Item Status: Live Archive
Faculty / Department / School: Current - Faculty of Health, Engineering and Sciences - School of Mechanical and Electrical Engineering
Date Deposited: 16 May 2017 05:11
Last Modified: 03 Oct 2017 01:33
Uncontrolled Keywords: strain measurement, neural network, FBG sensors, Structural Health Monitoring
Fields of Research : 09 Engineering > 0906 Electrical and Electronic Engineering > 090606 Photonics and Electro-Optical Engineering (excl. Communications)
09 Engineering > 0901 Aerospace Engineering > 090199 Aerospace Engineering not elsewhere classified
09 Engineering > 0901 Aerospace Engineering > 090103 Aerospace Structures
09 Engineering > 0913 Mechanical Engineering > 091308 Solid Mechanics
Socio-Economic Objective: B Economic Development > 88 Transport > 8803 Aerospace Transport > 880303 Air Safety
URI: http://eprints.usq.edu.au/id/eprint/31173

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