Phased Array Ultrasonic Inspection of Composite Fuselage Panel

The composite fuselage panel is a crucial component in large civil aircraft, necessitating higher detection rates and efficiency. Phased array ultrasonic testing can enhance the efficiency and defect detection rate; however, it is essential to consider the structural characteristics of the fuselage...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of physics. Conference series 2024-09, Vol.2822 (1), p.12108
Hauptverfasser: Zhiying, Li, Feifei, Liu, Yusen, Yang, Songping, Liu
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue 1
container_start_page 12108
container_title Journal of physics. Conference series
container_volume 2822
creator Zhiying, Li
Feifei, Liu
Yusen, Yang
Songping, Liu
description The composite fuselage panel is a crucial component in large civil aircraft, necessitating higher detection rates and efficiency. Phased array ultrasonic testing can enhance the efficiency and defect detection rate; however, it is essential to consider the structural characteristics of the fuselage to ensure reliable identification of design defects. Based on the material properties, structural features, and defect detection requirements of composite fuselage panels, a test block reflecting their characteristics was designed and fabricated with various prefabricated defects. Ultrasonic phased array method was employed for a series of testing parameter optimization experiments and defect detectability analysis. The detected flaws were quantitatively analyzed and compared with those obtained using conventional ultrasonic automatic scanning techniques to validate the effectiveness of the developed ultrasonic phased array method. The feasibility of utilizing phased array ultrasonics for nondestructive evaluation of wide-body airliner composite fuselage panels is confirmed.
doi_str_mv 10.1088/1742-6596/2822/1/012108
format Article
fullrecord <record><control><sourceid>proquest_iop_j</sourceid><recordid>TN_cdi_proquest_journals_3121582797</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3121582797</sourcerecordid><originalsourceid>FETCH-LOGICAL-c1207-c1dc495da86cc7bd7f0720f5b8bfe6500570d85f980b3dbe3ad5b17b087105503</originalsourceid><addsrcrecordid>eNqFkE1PwzAMhiMEEmPwG4jEedRJlya9IE0TG5MmsQM7R_kqdOqaknSH_XtSFY0jPtiW7Pe1_CD0SOCZgBAZ4XM6K1hZZFRQmpEMCE2DKzS5TK4vvRC36C7GA0Cegk_Qy-5LRWfxIgR1xvumDyr6tjZ408bOmb72LfYVXvpj52PdO7w6RdeoT4d3qnXNPbqpVBPdw2-dov3q9WP5Ntu-rzfLxXZmCAWesjXzklklCmO4trwCTqFiWujKFQyAcbCCVaUAnVvtcmWZJlyD4AQYg3yKnkbfLvjvk4u9PPhTaNNJmad3maC85GmLj1sm-BiDq2QX6qMKZ0lADrDkgEEOSOQASxI5wkrKfFTWvvuz_k_1A6-Fapg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>3121582797</pqid></control><display><type>article</type><title>Phased Array Ultrasonic Inspection of Composite Fuselage Panel</title><source>Open Access: IOP Publishing Free Content</source><source>Full-Text Journals in Chemistry (Open access)</source><source>IOPscience journals</source><source>Alma/SFX Local Collection</source><source>EZB Electronic Journals Library</source><creator>Zhiying, Li ; Feifei, Liu ; Yusen, Yang ; Songping, Liu</creator><creatorcontrib>Zhiying, Li ; Feifei, Liu ; Yusen, Yang ; Songping, Liu</creatorcontrib><description>The composite fuselage panel is a crucial component in large civil aircraft, necessitating higher detection rates and efficiency. Phased array ultrasonic testing can enhance the efficiency and defect detection rate; however, it is essential to consider the structural characteristics of the fuselage to ensure reliable identification of design defects. Based on the material properties, structural features, and defect detection requirements of composite fuselage panels, a test block reflecting their characteristics was designed and fabricated with various prefabricated defects. Ultrasonic phased array method was employed for a series of testing parameter optimization experiments and defect detectability analysis. The detected flaws were quantitatively analyzed and compared with those obtained using conventional ultrasonic automatic scanning techniques to validate the effectiveness of the developed ultrasonic phased array method. The feasibility of utilizing phased array ultrasonics for nondestructive evaluation of wide-body airliner composite fuselage panels is confirmed.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/2822/1/012108</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aircraft detection ; Airframes ; Design defects ; Flaw detection ; Fuselages ; Material properties ; Nondestructive testing ; Panels ; Parameter identification ; Phased arrays ; Prefabricated buildings ; Ultrasonic testing ; Wide-body aircraft</subject><ispartof>Journal of physics. Conference series, 2024-09, Vol.2822 (1), p.12108</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>Published under licence by IOP Publishing Ltd. This work is published under https://creativecommons.org/licenses/by/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c1207-c1dc495da86cc7bd7f0720f5b8bfe6500570d85f980b3dbe3ad5b17b087105503</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://iopscience.iop.org/article/10.1088/1742-6596/2822/1/012108/pdf$$EPDF$$P50$$Giop$$Hfree_for_read</linktopdf><link.rule.ids>314,780,784,27924,27925,38868,38890,53840,53867</link.rule.ids></links><search><creatorcontrib>Zhiying, Li</creatorcontrib><creatorcontrib>Feifei, Liu</creatorcontrib><creatorcontrib>Yusen, Yang</creatorcontrib><creatorcontrib>Songping, Liu</creatorcontrib><title>Phased Array Ultrasonic Inspection of Composite Fuselage Panel</title><title>Journal of physics. Conference series</title><addtitle>J. Phys.: Conf. Ser</addtitle><description>The composite fuselage panel is a crucial component in large civil aircraft, necessitating higher detection rates and efficiency. Phased array ultrasonic testing can enhance the efficiency and defect detection rate; however, it is essential to consider the structural characteristics of the fuselage to ensure reliable identification of design defects. Based on the material properties, structural features, and defect detection requirements of composite fuselage panels, a test block reflecting their characteristics was designed and fabricated with various prefabricated defects. Ultrasonic phased array method was employed for a series of testing parameter optimization experiments and defect detectability analysis. The detected flaws were quantitatively analyzed and compared with those obtained using conventional ultrasonic automatic scanning techniques to validate the effectiveness of the developed ultrasonic phased array method. The feasibility of utilizing phased array ultrasonics for nondestructive evaluation of wide-body airliner composite fuselage panels is confirmed.</description><subject>Aircraft detection</subject><subject>Airframes</subject><subject>Design defects</subject><subject>Flaw detection</subject><subject>Fuselages</subject><subject>Material properties</subject><subject>Nondestructive testing</subject><subject>Panels</subject><subject>Parameter identification</subject><subject>Phased arrays</subject><subject>Prefabricated buildings</subject><subject>Ultrasonic testing</subject><subject>Wide-body aircraft</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNqFkE1PwzAMhiMEEmPwG4jEedRJlya9IE0TG5MmsQM7R_kqdOqaknSH_XtSFY0jPtiW7Pe1_CD0SOCZgBAZ4XM6K1hZZFRQmpEMCE2DKzS5TK4vvRC36C7GA0Cegk_Qy-5LRWfxIgR1xvumDyr6tjZ408bOmb72LfYVXvpj52PdO7w6RdeoT4d3qnXNPbqpVBPdw2-dov3q9WP5Ntu-rzfLxXZmCAWesjXzklklCmO4trwCTqFiWujKFQyAcbCCVaUAnVvtcmWZJlyD4AQYg3yKnkbfLvjvk4u9PPhTaNNJmad3maC85GmLj1sm-BiDq2QX6qMKZ0lADrDkgEEOSOQASxI5wkrKfFTWvvuz_k_1A6-Fapg</recordid><startdate>20240901</startdate><enddate>20240901</enddate><creator>Zhiying, Li</creator><creator>Feifei, Liu</creator><creator>Yusen, Yang</creator><creator>Songping, Liu</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20240901</creationdate><title>Phased Array Ultrasonic Inspection of Composite Fuselage Panel</title><author>Zhiying, Li ; Feifei, Liu ; Yusen, Yang ; Songping, Liu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c1207-c1dc495da86cc7bd7f0720f5b8bfe6500570d85f980b3dbe3ad5b17b087105503</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Aircraft detection</topic><topic>Airframes</topic><topic>Design defects</topic><topic>Flaw detection</topic><topic>Fuselages</topic><topic>Material properties</topic><topic>Nondestructive testing</topic><topic>Panels</topic><topic>Parameter identification</topic><topic>Phased arrays</topic><topic>Prefabricated buildings</topic><topic>Ultrasonic testing</topic><topic>Wide-body aircraft</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhiying, Li</creatorcontrib><creatorcontrib>Feifei, Liu</creatorcontrib><creatorcontrib>Yusen, Yang</creatorcontrib><creatorcontrib>Songping, Liu</creatorcontrib><collection>Open Access: IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>Advanced Technologies &amp; Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection (Proquest) (PQ_SDU_P3)</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>ProQuest Advanced Technologies &amp; Aerospace Database</collection><collection>ProQuest Advanced Technologies &amp; Aerospace Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Journal of physics. Conference series</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhiying, Li</au><au>Feifei, Liu</au><au>Yusen, Yang</au><au>Songping, Liu</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Phased Array Ultrasonic Inspection of Composite Fuselage Panel</atitle><jtitle>Journal of physics. Conference series</jtitle><addtitle>J. Phys.: Conf. Ser</addtitle><date>2024-09-01</date><risdate>2024</risdate><volume>2822</volume><issue>1</issue><spage>12108</spage><pages>12108-</pages><issn>1742-6588</issn><eissn>1742-6596</eissn><abstract>The composite fuselage panel is a crucial component in large civil aircraft, necessitating higher detection rates and efficiency. Phased array ultrasonic testing can enhance the efficiency and defect detection rate; however, it is essential to consider the structural characteristics of the fuselage to ensure reliable identification of design defects. Based on the material properties, structural features, and defect detection requirements of composite fuselage panels, a test block reflecting their characteristics was designed and fabricated with various prefabricated defects. Ultrasonic phased array method was employed for a series of testing parameter optimization experiments and defect detectability analysis. The detected flaws were quantitatively analyzed and compared with those obtained using conventional ultrasonic automatic scanning techniques to validate the effectiveness of the developed ultrasonic phased array method. The feasibility of utilizing phased array ultrasonics for nondestructive evaluation of wide-body airliner composite fuselage panels is confirmed.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1742-6596/2822/1/012108</doi><tpages>10</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 1742-6588
ispartof Journal of physics. Conference series, 2024-09, Vol.2822 (1), p.12108
issn 1742-6588
1742-6596
language eng
recordid cdi_proquest_journals_3121582797
source Open Access: IOP Publishing Free Content; Full-Text Journals in Chemistry (Open access); IOPscience journals; Alma/SFX Local Collection; EZB Electronic Journals Library
subjects Aircraft detection
Airframes
Design defects
Flaw detection
Fuselages
Material properties
Nondestructive testing
Panels
Parameter identification
Phased arrays
Prefabricated buildings
Ultrasonic testing
Wide-body aircraft
title Phased Array Ultrasonic Inspection of Composite Fuselage Panel
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T18%3A34%3A19IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_iop_j&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Phased%20Array%20Ultrasonic%20Inspection%20of%20Composite%20Fuselage%20Panel&rft.jtitle=Journal%20of%20physics.%20Conference%20series&rft.au=Zhiying,%20Li&rft.date=2024-09-01&rft.volume=2822&rft.issue=1&rft.spage=12108&rft.pages=12108-&rft.issn=1742-6588&rft.eissn=1742-6596&rft_id=info:doi/10.1088/1742-6596/2822/1/012108&rft_dat=%3Cproquest_iop_j%3E3121582797%3C/proquest_iop_j%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=3121582797&rft_id=info:pmid/&rfr_iscdi=true