Non destructive inspection (NDI) is a widely used method for quality control and materials inspection across various industries, especially in the aerospace field where the introduction of composite materials has revolutionized inspection techniques. In addition, in-service ultrasonic inspection (UT) is also used for preventive maintenance purposes. One of the biggest challenges of such techniques is the need to use a coupling medium, which can often be a critical issue. For this reason, considerable effort has been made in the aerospace field in recent years to employ innovative techniques that do not require the use of coupling media. One of the proposed techniques is Laser Ultrasonic Non-Destructive Testing (LUNDT), which is recognized as a promising method due to its rapid scanning speed, non-contact inspection, coupling-agent independence, and ability to inspect complex shapes. Today, the primary focus is not on generating ultrasound in the material, but rather on how to receive and interpret it. In recent years, several companies have attempted to provide their own solutions in this field. In this study, the utilized solution is based on an all-optical akinetic sensor, which has demonstrated the most promising results. With this technology, we performed a series of analyses on aerospace components of interest, including those made of composite and metallic materials.

Laser Ultrasonic Non-Destructive Testing for Aerospace Applications / Del Prete, Giuseppe; Leone, Fabrizio; Dentico, Valerio; Gallo, Nicola; Maio, Leandro; Memmolo, Vittorio; Vespini, Veronica; Coppola, Sara; Stella, Ettore; Ferraro, Pietro. - (2023), pp. 525-528. ( 10th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2023 ita 2023) [10.1109/metroaerospace57412.2023.10189937].

Laser Ultrasonic Non-Destructive Testing for Aerospace Applications

Maio, Leandro;Memmolo, Vittorio;Ferraro, Pietro
2023

Abstract

Non destructive inspection (NDI) is a widely used method for quality control and materials inspection across various industries, especially in the aerospace field where the introduction of composite materials has revolutionized inspection techniques. In addition, in-service ultrasonic inspection (UT) is also used for preventive maintenance purposes. One of the biggest challenges of such techniques is the need to use a coupling medium, which can often be a critical issue. For this reason, considerable effort has been made in the aerospace field in recent years to employ innovative techniques that do not require the use of coupling media. One of the proposed techniques is Laser Ultrasonic Non-Destructive Testing (LUNDT), which is recognized as a promising method due to its rapid scanning speed, non-contact inspection, coupling-agent independence, and ability to inspect complex shapes. Today, the primary focus is not on generating ultrasound in the material, but rather on how to receive and interpret it. In recent years, several companies have attempted to provide their own solutions in this field. In this study, the utilized solution is based on an all-optical akinetic sensor, which has demonstrated the most promising results. With this technology, we performed a series of analyses on aerospace components of interest, including those made of composite and metallic materials.
2023
Laser Ultrasonic Non-Destructive Testing for Aerospace Applications / Del Prete, Giuseppe; Leone, Fabrizio; Dentico, Valerio; Gallo, Nicola; Maio, Leandro; Memmolo, Vittorio; Vespini, Veronica; Coppola, Sara; Stella, Ettore; Ferraro, Pietro. - (2023), pp. 525-528. ( 10th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2023 ita 2023) [10.1109/metroaerospace57412.2023.10189937].
File in questo prodotto:
File Dimensione Formato  
Laser_Ultrasonic_Non-Destructive_Testing_for_Aerospace_Applications.pdf

solo utenti autorizzati

Tipologia: Versione Editoriale (PDF)
Licenza: Copyright dell'editore
Dimensione 522.34 kB
Formato Adobe PDF
522.34 kB Adobe PDF   Visualizza/Apri   Richiedi una copia

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/1016663
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 4
  • ???jsp.display-item.citation.isi??? ND
social impact