Active Health Monitoring of Thick Composite Structures by Embedded and Surface-Mounted Piezo Diagnostic Layer
An effective approach for an embedded piezo diagnostic layer into thick composite material is presented. The effectiveness of the approach is assessed in comparison to the surface-mounted layer. The proposed manufacturing alleviates difficulties associated with trimming edges of composites when embe...
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| Published in | Sensors (Basel, Switzerland) Vol. 20; no. 12; p. 3410 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
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17.06.2020
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| Abstract | An effective approach for an embedded piezo diagnostic layer into thick composite material is presented. The effectiveness of the approach is assessed in comparison to the surface-mounted layer. The proposed manufacturing alleviates difficulties associated with trimming edges of composites when embedding wires. The Electro-Mechanical Impedance technique is used to access the integrity of the piezoelectric sensors bonding process. Comparisons of ultrasonic guided waves are made between embedded and surface-mounted diagnostic layers and their penetration through and across the thickness of the composites. Temperature influences with the range from −40 °C up to 80 °C on embedded and surface-mounted guided waves are investigated. An investigation is carried out into the relationship between amplitude and time-of-flight with temperature at different excitation frequencies. The temperature has significant but different effects on amplitude and phase-shift of guided waves for the embedded layer compared to the surface-mounted layer. A Laser Doppler Vibrometer is used to identify the blue tack and impact damage. Both embedded and surface-mounted layers are shown to be an effective means of generating detectable wave scatter from damage. |
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| AbstractList | An effective approach for an embedded piezo diagnostic layer into thick composite material is presented. The effectiveness of the approach is assessed in comparison to the surface-mounted layer. The proposed manufacturing alleviates difficulties associated with trimming edges of composites when embedding wires. The Electro-Mechanical Impedance technique is used to access the integrity of the piezoelectric sensors bonding process. Comparisons of ultrasonic guided waves are made between embedded and surface-mounted diagnostic layers and their penetration through and across the thickness of the composites. Temperature influences with the range from −40 °C up to 80 °C on embedded and surface-mounted guided waves are investigated. An investigation is carried out into the relationship between amplitude and time-of-flight with temperature at different excitation frequencies. The temperature has significant but different effects on amplitude and phase-shift of guided waves for the embedded layer compared to the surface-mounted layer. A Laser Doppler Vibrometer is used to identify the blue tack and impact damage. Both embedded and surface-mounted layers are shown to be an effective means of generating detectable wave scatter from damage. |
| Author | Bekas, Dimitrios Feng, Tianyi Aliabadi, M. H. Ferri |
| AuthorAffiliation | Structural Durability and Health Monitoring, Imperial College London, South Kensington, London SW7 2AZ, UK; bekasdim@gmail.com (D.B.); m.h.aliabadi@imperial.ac.uk (M.H.F.A.) |
| AuthorAffiliation_xml | – name: Structural Durability and Health Monitoring, Imperial College London, South Kensington, London SW7 2AZ, UK; bekasdim@gmail.com (D.B.); m.h.aliabadi@imperial.ac.uk (M.H.F.A.) |
| Author_xml | – sequence: 1 givenname: Tianyi orcidid: 0000-0003-4024-5937 surname: Feng fullname: Feng, Tianyi – sequence: 2 givenname: Dimitrios orcidid: 0000-0002-0922-2975 surname: Bekas fullname: Bekas, Dimitrios – sequence: 3 givenname: M. H. Ferri surname: Aliabadi fullname: Aliabadi, M. H. Ferri |
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| CitedBy_id | crossref_primary_10_1016_j_matdes_2021_110321 crossref_primary_10_1016_j_prostr_2023_12_077 crossref_primary_10_1016_j_compositesb_2021_108673 crossref_primary_10_1016_j_ndteint_2023_102988 crossref_primary_10_3390_app12104916 crossref_primary_10_3390_s21030679 crossref_primary_10_1080_15376494_2023_2271746 crossref_primary_10_3390_ma16083057 crossref_primary_10_3390_ma14206148 crossref_primary_10_3390_machines10121185 crossref_primary_10_3390_mi15020274 crossref_primary_10_3390_s21206926 crossref_primary_10_3390_ma15196752 crossref_primary_10_1080_15376494_2024_2342028 crossref_primary_10_3390_s22207799 crossref_primary_10_3390_jcs8060201 crossref_primary_10_3390_s21155131 crossref_primary_10_1088_1361_665X_ac7d23 crossref_primary_10_3390_app131810474 crossref_primary_10_3390_s21041283 |
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| SubjectTerms | Aeronautics Aircraft Amplitudes Carbon Circuits Composite materials Composite structures Diagnostic systems Epoxy adhesives Impact damage laser doppler vibrometer Manufacturing Mechanical impedance Methods Sensors structural health monitoring temperature influences thick composites Vibration meters |
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| Title | Active Health Monitoring of Thick Composite Structures by Embedded and Surface-Mounted Piezo Diagnostic Layer |
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