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Cited by 136Cellular and Composite StructuresAdditive Manufacturing and 3D Printing TechnologiesAdditive Manufacturing Materials and Processes

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Development of a multifunctional panel for aerospace use through SLM additive manufacturing

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Bici, Michele, Brischetto, Salvatore, Campana, Francesca, Ferro, Carlo Giovanni, Seclì, Carlo, Varetti, Sara, Maggiore, Paolo, Mazza, Andrea·2018·Procedia CIRP
DOI 10.1016/j.procir.2017.12.202
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Abstract

Lattice materials can overcome the need of light and stiff structures in the aerospace industry. The wing leading edge is one of the most critical parts for both on-board subsystem and structure features: it must withstand to the aerodynamic loads and bird-strike, integrating also the anti-ice system functions. Nowadays, this part is made by different components bonded together such as external skin, internal passageways, and feeding tubes. In the present work, a single-piece multifunctional panel made by additive manufacturing will be developed. Optimal design and manufacturing are discussed according to technological constraints, aeronautical performances and sustainability.

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Research works printed but not linked: 7

  1. Cao, 2015, Aircraft flight characteristics in icing conditions, Progress in Aerospace Sciences, 74, 62, 10.1016/j.paerosci.2014.12.001 · DOI
  2. Xin, 2014, A spongy icing model for aircraft icing, Chinese Journal of Aeronautics, 27, 40, 10.1016/j.cja.2013.12.004 · DOI
  3. Srensen K. L., Blanke M., Johansen T. A. Diagnosis of Wing Icing Through Lift and Drag Coefficient Change Detection for Small Unmanned Aircraft. IFAC-Papers OnLine, 2015, Vol. 48, pp. 541-546. · DOI
  4. Politovich, M.K. AVIATION METEOROLOGY: Aircraft Icing. Encyclopedia of Atmospheric Sciences. 2015. · DOI
  5. Parent, 2011, Anti-icing and de-icing techniques for wind turbines: Critical review, Cold Regions Science and Technology, 65, 88, 10.1016/j.coldregions.2010.01.005 · DOI
  6. Yan, 2015, Microstructure and mechanical properties of aluminium alloy cellular lattice structures manufactured by direct metal laser sintering, Materials Science and Engineering A, 628, 238, 10.1016/j.msea.2015.01.063 · DOI
  7. Yan, 2014, Evaluation of light weight AlSi10Mg periodic cellular lattice structures fabricated via directmetal laser sintering, Journal of Materials Processing Technology, 214, 10.1016/j.jmatprotec.2013.12.004 · DOI

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Metadata

Authors
Bici, M., Brischetto, S., Campana, F., Ferro, C. G., Seclì, C., Varetti, S., Maggiore, P., & Mazza, A.
Affiliations
  • Sapienza University of Rome (IT)
  • Politecnico di Torino (IT)
Corresponding author
Ferro, Carlo Giovanni
ORCID
Venue
Procedia CIRP
Publisher
Elsevier BV
Published
2018
Volume
67
Pages
215-220
ISSN
2212-8271 (ISSN-L)
DOI
10.1016/j.procir.2017.12.202
OpenAlex
W2786153774
Cited by
136
References
0
Citations by year
2026: 9 · 2025: 20 · 2024: 29 · 2023: 20 · 2022: 21 · 2021: 17 · 2020: 13 · 2019: 3 · 2018: 4
FWCI
5.91
Type
journal article
Language
en
Open access
Licence
Locations
  • Procedia CIRP (publishedVersion, cc-by-nc-nd)
  • PORTO@Iris (submittedVersion, cc-by-nc-nd)
  • IRIS Research product catalog (Sapienza University of Rome) (submittedVersion, cc-by-nc-nd)
  • PORTO Publications Open Repository TOrino (Politecnico di Torino) (submittedVersion, cc-by-nc-nd)
Topics
  • Physical Sciences › Engineering › Mechanical Engineering › Cellular and Composite Structures
  • Physical Sciences › Engineering › Industrial and Manufacturing Engineering › Additive Manufacturing and 3D Printing Technologies
  • Physical Sciences › Engineering › Mechanical Engineering › Additive Manufacturing Materials and Processes
Keywords
lattice structures, wing leading edge, laser powder bed fusion, additive manufacturing, bird strikes, lightweight structures, aerodynamic forces, design optimization, sustainability

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CoChat. (2026). Citation check: Development of a multifunctional panel for aerospace use through SLM additive manufacturing. https://app.cochat.ai/papers/10.1016/j.procir.2017.12.202
The paper
Bici, M., Brischetto, S., Campana, F., Ferro, C. G., Seclì, C., Varetti, S., Maggiore, P., & Mazza, A. (2018). Development of a multifunctional panel for aerospace use through SLM additive manufacturing. Procedia CIRP. https://doi.org/10.1016/j.procir.2017.12.202