SG10201606205SA - System and Method for Monitoring Structural Health of Bonded Components - Google Patents

System and Method for Monitoring Structural Health of Bonded Components

Info

Publication number
SG10201606205SA
SG10201606205SA SG10201606205SA SG10201606205SA SG10201606205SA SG 10201606205S A SG10201606205S A SG 10201606205SA SG 10201606205S A SG10201606205S A SG 10201606205SA SG 10201606205S A SG10201606205S A SG 10201606205SA SG 10201606205S A SG10201606205S A SG 10201606205SA
Authority
SG
Singapore
Prior art keywords
structural health
monitoring structural
bonded components
bonded
monitoring
Prior art date
Application number
SG10201606205SA
Inventor
Ihn Jeong-Beom
Choi Keeyoung
Original Assignee
Boeing Co
Choi Keeyoung
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co, Choi Keeyoung filed Critical Boeing Co
Publication of SG10201606205SA publication Critical patent/SG10201606205SA/en

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B21/00—Alarms responsive to a single specified undesired or abnormal condition and not otherwise provided for
    • G08B21/18—Status alarms
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0016—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of aircraft wings or blades
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0083—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by measuring variation of impedance, e.g. resistance, capacitance, induction
    • G—PHYSICS
    • G08—SIGNALLING
    • G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B5/00—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied
SG10201606205SA 2015-11-09 2016-07-27 System and Method for Monitoring Structural Health of Bonded Components SG10201606205SA (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/935,887 US10210740B2 (en) 2015-11-09 2015-11-09 System and method for monitoring structural health of bonded components

Publications (1)

Publication Number Publication Date
SG10201606205SA true SG10201606205SA (en) 2017-06-29

Family

ID=57288161

Family Applications (1)

Application Number Title Priority Date Filing Date
SG10201606205SA SG10201606205SA (en) 2015-11-09 2016-07-27 System and Method for Monitoring Structural Health of Bonded Components

Country Status (6)

Country Link
US (1) US10210740B2 (en)
EP (1) EP3165890B1 (en)
JP (1) JP6937106B2 (en)
CN (1) CN107063591A (en)
ES (1) ES2719173T3 (en)
SG (1) SG10201606205SA (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9233765B2 (en) * 2011-06-16 2016-01-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Multi-dimensional damage detection
CN109959678A (en) * 2017-12-23 2019-07-02 青岛青特众力车桥有限公司 Metal part crackle forecasts alarm method
US10995037B1 (en) 2018-12-13 2021-05-04 United States Of America As Represented By The Secretary Of The Air Force High temperature composite structure and system for detecting degradation thereof
US11053020B2 (en) 2019-08-13 2021-07-06 The Boeing Company Electrically conductive patch for indicating a compromised electrical discharge point in an aircraft
US10919643B1 (en) * 2019-08-14 2021-02-16 Goodrich Corporation Aircraft light fixture energy harvesting
US11181518B2 (en) * 2019-10-31 2021-11-23 The Boeing Company System and method for evaluating a bond
CN110823960B (en) * 2019-11-26 2022-04-01 桂林电子科技大学 Surface damage detection device
US20220268737A1 (en) * 2021-02-22 2022-08-25 Zhengzhou University of Aeronautics Ltd. Method, Equipment and Readable Medium for Evaluating Structural Strength of Fiber and Nanosized Materials Reinforced Concrete
US11718415B2 (en) * 2021-06-04 2023-08-08 Goodrich Corporation Energy autonomous aircraft evacuation slide systems and methods

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US4503710A (en) * 1983-06-08 1985-03-12 Conoco Inc. Crack detection by electrical resistance
JPS6360953U (en) * 1986-10-09 1988-04-22
JPH0564751U (en) * 1992-02-04 1993-08-27 帝人製機株式会社 Indicator plug
JP2902639B1 (en) * 1998-06-29 1999-06-07 圭策 仙波 Input key switch structure
JP2005091167A (en) * 2003-09-17 2005-04-07 Railway Technical Res Inst Crack detecting tape, and crack detection system
JPWO2005033475A1 (en) * 2003-10-01 2006-12-14 株式会社日立製作所 Tunnel fall monitoring system, tunnel fall monitoring method, and civil engineering structure damage monitoring system
US20050112768A1 (en) * 2003-11-26 2005-05-26 Thomas Evans Method of authenticating tagged polymers
US7233250B2 (en) * 2004-12-29 2007-06-19 Avery Dennison Corporation Radio frequency identification device with visual indicator
US7398698B2 (en) * 2005-11-03 2008-07-15 The Boeing Company Smart repair patch and associated method
WO2007085070A1 (en) 2006-01-26 2007-08-02 National Research Council Of Canada Surface-mounted crack detection
DE102006010901B4 (en) * 2006-03-09 2022-02-17 Robert Bosch Gmbh Fluid sensor with error detection device
WO2009124054A1 (en) * 2008-03-31 2009-10-08 Delta Technologies System, device and associated methods for monitoring a physical condition or operating performance of a structure
WO2009144488A1 (en) 2008-05-27 2009-12-03 Bae Systems Plc Damage sensors and processing arrangements therefor
DE112009004421T8 (en) 2009-02-25 2012-09-13 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. RFID scanning system without external power supply to query the structural health
GB0909778D0 (en) * 2009-06-08 2009-07-22 Conductive Inkjet Technology Ltd Display device
US8570152B2 (en) 2009-07-23 2013-10-29 The Boeing Company Method and apparatus for wireless sensing with power harvesting of a wireless signal
WO2012048237A2 (en) 2010-10-08 2012-04-12 Checkit Technologies, Llc Structural integrity system and methods
US8812251B2 (en) 2011-04-12 2014-08-19 The Boeing Company System and method for monitoring bonding integrity
CN202794092U (en) * 2012-09-14 2013-03-13 于百勇 Metro tunnel concrete crack monitoring device based on flexible conductive coating

Also Published As

Publication number Publication date
JP2017111119A (en) 2017-06-22
US20170132901A1 (en) 2017-05-11
EP3165890B1 (en) 2019-01-09
US10210740B2 (en) 2019-02-19
EP3165890A1 (en) 2017-05-10
ES2719173T3 (en) 2019-07-08
CN107063591A (en) 2017-08-18
JP6937106B2 (en) 2021-09-22

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