Damage visualization of a cylindrical CFRP lattice-skin structure based on a pulse-echo ultrasonic propagation imager
•NDE using a PE UPI was performed to visualize damage in a lattice-skin structure.•Cylindrical lattice-skin structures cause a curvature effect in the PE UPI results.•Curvature-compensating algorithm was developed to reduce the curvature effect.•Delaminations were clearly visualized by effectively r...
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Veröffentlicht in: | Measurement : journal of the International Measurement Confederation 2019-12, Vol.147, p.106837, Article 106837 |
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creator | Shin, Hye-Jin Choi, Yunshil Lee, Jung-Ryul |
description | •NDE using a PE UPI was performed to visualize damage in a lattice-skin structure.•Cylindrical lattice-skin structures cause a curvature effect in the PE UPI results.•Curvature-compensating algorithm was developed to reduce the curvature effect.•Delaminations were clearly visualized by effectively reducing the curvature effect.
Recently, composite lattice structures are attracting significant attention owing to their high specific stiffness and specific strength and are mainly used in aerospace applications. However, the composite lattice structure also exhibits damage occurrence probability during operation as well as defects in the filament winding manufacturing process. Thus a non-destructive evaluation (NDE) technique for defect and damage evaluation is essential although its complexity is not desirable, especially with respect to in-situ NDE. In this study, we propose a pulse-echo ultrasonic propagation imaging (PE UPI) system for in-situ NDE of cylindrical composite lattice-skin specimen and develop a VTWAM (Variable time window amplitude mapping)-based curvature-compensating algorithm that eliminates the curved surface effect of the PE UPI system. As a result of the actual application to a damaged lattice cylindrical specimen, the damage position, size, and shape are clearly visualized by effectively suppressing the curved surface effect in the inspection region via the VTWAM-based curvature-compensating algorithm. We demonstrate the capability of the linear scan PE UPI to inspect a curved and complex lattice-skin structure with a curved surface compensation algorithm and propose the same as a tool for in-situ health management of composite lattice structures for manufacturing to in-service stages. |
doi_str_mv | 10.1016/j.measurement.2019.07.065 |
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Recently, composite lattice structures are attracting significant attention owing to their high specific stiffness and specific strength and are mainly used in aerospace applications. However, the composite lattice structure also exhibits damage occurrence probability during operation as well as defects in the filament winding manufacturing process. Thus a non-destructive evaluation (NDE) technique for defect and damage evaluation is essential although its complexity is not desirable, especially with respect to in-situ NDE. In this study, we propose a pulse-echo ultrasonic propagation imaging (PE UPI) system for in-situ NDE of cylindrical composite lattice-skin specimen and develop a VTWAM (Variable time window amplitude mapping)-based curvature-compensating algorithm that eliminates the curved surface effect of the PE UPI system. As a result of the actual application to a damaged lattice cylindrical specimen, the damage position, size, and shape are clearly visualized by effectively suppressing the curved surface effect in the inspection region via the VTWAM-based curvature-compensating algorithm. We demonstrate the capability of the linear scan PE UPI to inspect a curved and complex lattice-skin structure with a curved surface compensation algorithm and propose the same as a tool for in-situ health management of composite lattice structures for manufacturing to in-service stages.</description><identifier>ISSN: 0263-2241</identifier><identifier>EISSN: 1873-412X</identifier><identifier>DOI: 10.1016/j.measurement.2019.07.065</identifier><language>eng</language><publisher>London: Elsevier Ltd</publisher><subject>Aerospace industry ; Algorithms ; Complexity ; Composite lattice structure ; Composite materials ; Curvature ; Curvature-compensating algorithm ; Damage assessment ; Damage visualization ; Destructive testing ; Filament winding ; In-situ non-destructive evaluation ; Inspection ; Lattice theory ; Mapping ; Nondestructive testing ; Pulse propagation ; Pulse-echo ultrasonic propagation imaging ; Skin ; Stiffness ; Structural damage ; Structural health monitoring ; Ultrasonic testing ; Windows (intervals)</subject><ispartof>Measurement : journal of the International Measurement Confederation, 2019-12, Vol.147, p.106837, Article 106837</ispartof><rights>2019 Elsevier Ltd</rights><rights>Copyright Elsevier Science Ltd. Dec 2019</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c349t-f2d7efb45779d37d52c26f86aa6da0d7917f9626029e762d10f7c8eb10c5c6bb3</citedby><cites>FETCH-LOGICAL-c349t-f2d7efb45779d37d52c26f86aa6da0d7917f9626029e762d10f7c8eb10c5c6bb3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.measurement.2019.07.065$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,778,782,3539,27911,27912,45982</link.rule.ids></links><search><creatorcontrib>Shin, Hye-Jin</creatorcontrib><creatorcontrib>Choi, Yunshil</creatorcontrib><creatorcontrib>Lee, Jung-Ryul</creatorcontrib><title>Damage visualization of a cylindrical CFRP lattice-skin structure based on a pulse-echo ultrasonic propagation imager</title><title>Measurement : journal of the International Measurement Confederation</title><description>•NDE using a PE UPI was performed to visualize damage in a lattice-skin structure.•Cylindrical lattice-skin structures cause a curvature effect in the PE UPI results.•Curvature-compensating algorithm was developed to reduce the curvature effect.•Delaminations were clearly visualized by effectively reducing the curvature effect.
Recently, composite lattice structures are attracting significant attention owing to their high specific stiffness and specific strength and are mainly used in aerospace applications. However, the composite lattice structure also exhibits damage occurrence probability during operation as well as defects in the filament winding manufacturing process. Thus a non-destructive evaluation (NDE) technique for defect and damage evaluation is essential although its complexity is not desirable, especially with respect to in-situ NDE. In this study, we propose a pulse-echo ultrasonic propagation imaging (PE UPI) system for in-situ NDE of cylindrical composite lattice-skin specimen and develop a VTWAM (Variable time window amplitude mapping)-based curvature-compensating algorithm that eliminates the curved surface effect of the PE UPI system. As a result of the actual application to a damaged lattice cylindrical specimen, the damage position, size, and shape are clearly visualized by effectively suppressing the curved surface effect in the inspection region via the VTWAM-based curvature-compensating algorithm. We demonstrate the capability of the linear scan PE UPI to inspect a curved and complex lattice-skin structure with a curved surface compensation algorithm and propose the same as a tool for in-situ health management of composite lattice structures for manufacturing to in-service stages.</description><subject>Aerospace industry</subject><subject>Algorithms</subject><subject>Complexity</subject><subject>Composite lattice structure</subject><subject>Composite materials</subject><subject>Curvature</subject><subject>Curvature-compensating algorithm</subject><subject>Damage assessment</subject><subject>Damage visualization</subject><subject>Destructive testing</subject><subject>Filament winding</subject><subject>In-situ non-destructive evaluation</subject><subject>Inspection</subject><subject>Lattice theory</subject><subject>Mapping</subject><subject>Nondestructive testing</subject><subject>Pulse propagation</subject><subject>Pulse-echo ultrasonic propagation imaging</subject><subject>Skin</subject><subject>Stiffness</subject><subject>Structural damage</subject><subject>Structural health monitoring</subject><subject>Ultrasonic testing</subject><subject>Windows (intervals)</subject><issn>0263-2241</issn><issn>1873-412X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNqNkM9LwzAUx4MoOKf_Q8Rza5K2SXuU6lQYKKLgLaTJ68zs2pqkg_nXmzEPHj083uX7470PQpeUpJRQfr1ON6D85GADfUgZoVVKREp4cYRmtBRZklP2foxmhPEsYSynp-jM-zUhhGcVn6HpVm3UCvDW-kl19lsFO_R4aLHCetfZ3jirVYfrxcsz7lQIVkPiP22PfXCTDrEYN8qDwdGl8Dh1HhLQHwOeuuCUH3qr8eiGUa0OyXbf5s7RSaui9OJ3z9Hb4u61fkiWT_eP9c0y0VlehaRlRkDb5IUQlcmEKZhmvC25UtwoYkRFRVtxxgmrQHBmKGmFLqGhRBeaN002R1eH3HjC1wQ-yPUwuT5WSpZRFqckRVRVB5V2g_cOWjm6eKfbSUrknrJcyz-U5Z6yJEJGytFbH7wQ39hacNJrC70GYx3oIM1g_5HyA6KVjow</recordid><startdate>201912</startdate><enddate>201912</enddate><creator>Shin, Hye-Jin</creator><creator>Choi, Yunshil</creator><creator>Lee, Jung-Ryul</creator><general>Elsevier Ltd</general><general>Elsevier Science Ltd</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>201912</creationdate><title>Damage visualization of a cylindrical CFRP lattice-skin structure based on a pulse-echo ultrasonic propagation imager</title><author>Shin, Hye-Jin ; Choi, Yunshil ; Lee, Jung-Ryul</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c349t-f2d7efb45779d37d52c26f86aa6da0d7917f9626029e762d10f7c8eb10c5c6bb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Aerospace industry</topic><topic>Algorithms</topic><topic>Complexity</topic><topic>Composite lattice structure</topic><topic>Composite materials</topic><topic>Curvature</topic><topic>Curvature-compensating algorithm</topic><topic>Damage assessment</topic><topic>Damage visualization</topic><topic>Destructive testing</topic><topic>Filament winding</topic><topic>In-situ non-destructive evaluation</topic><topic>Inspection</topic><topic>Lattice theory</topic><topic>Mapping</topic><topic>Nondestructive testing</topic><topic>Pulse propagation</topic><topic>Pulse-echo ultrasonic propagation imaging</topic><topic>Skin</topic><topic>Stiffness</topic><topic>Structural damage</topic><topic>Structural health monitoring</topic><topic>Ultrasonic testing</topic><topic>Windows (intervals)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Shin, Hye-Jin</creatorcontrib><creatorcontrib>Choi, Yunshil</creatorcontrib><creatorcontrib>Lee, Jung-Ryul</creatorcontrib><collection>CrossRef</collection><jtitle>Measurement : journal of the International Measurement Confederation</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Shin, Hye-Jin</au><au>Choi, Yunshil</au><au>Lee, Jung-Ryul</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Damage visualization of a cylindrical CFRP lattice-skin structure based on a pulse-echo ultrasonic propagation imager</atitle><jtitle>Measurement : journal of the International Measurement Confederation</jtitle><date>2019-12</date><risdate>2019</risdate><volume>147</volume><spage>106837</spage><pages>106837-</pages><artnum>106837</artnum><issn>0263-2241</issn><eissn>1873-412X</eissn><abstract>•NDE using a PE UPI was performed to visualize damage in a lattice-skin structure.•Cylindrical lattice-skin structures cause a curvature effect in the PE UPI results.•Curvature-compensating algorithm was developed to reduce the curvature effect.•Delaminations were clearly visualized by effectively reducing the curvature effect.
Recently, composite lattice structures are attracting significant attention owing to their high specific stiffness and specific strength and are mainly used in aerospace applications. However, the composite lattice structure also exhibits damage occurrence probability during operation as well as defects in the filament winding manufacturing process. Thus a non-destructive evaluation (NDE) technique for defect and damage evaluation is essential although its complexity is not desirable, especially with respect to in-situ NDE. In this study, we propose a pulse-echo ultrasonic propagation imaging (PE UPI) system for in-situ NDE of cylindrical composite lattice-skin specimen and develop a VTWAM (Variable time window amplitude mapping)-based curvature-compensating algorithm that eliminates the curved surface effect of the PE UPI system. As a result of the actual application to a damaged lattice cylindrical specimen, the damage position, size, and shape are clearly visualized by effectively suppressing the curved surface effect in the inspection region via the VTWAM-based curvature-compensating algorithm. We demonstrate the capability of the linear scan PE UPI to inspect a curved and complex lattice-skin structure with a curved surface compensation algorithm and propose the same as a tool for in-situ health management of composite lattice structures for manufacturing to in-service stages.</abstract><cop>London</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.measurement.2019.07.065</doi></addata></record> |
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subjects | Aerospace industry Algorithms Complexity Composite lattice structure Composite materials Curvature Curvature-compensating algorithm Damage assessment Damage visualization Destructive testing Filament winding In-situ non-destructive evaluation Inspection Lattice theory Mapping Nondestructive testing Pulse propagation Pulse-echo ultrasonic propagation imaging Skin Stiffness Structural damage Structural health monitoring Ultrasonic testing Windows (intervals) |
title | Damage visualization of a cylindrical CFRP lattice-skin structure based on a pulse-echo ultrasonic propagation imager |
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