Abstract
Design and manufacturing of a curved stiffened panel has been carried out within WP135 in SARISTU Integration Scenario IS13. The aim of this fuselage panel is the integration and validation of electrical structure network (ESN) technologies developed within Application Scenario AS10. The assembled panel includes premanufactured braided frames with cocured metallic strips aimed at improving electrical performance, impact detectability and damage tolerance. The panel will be subjected to electrical testing to verify the ESN solution, with additional frames used for impact testing and evaluation.
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Abbreviations
- AS10:
-
Application Scenario 10
- BMH:
-
Braided mousehole
- CFRP:
-
Carbon fibre-reinforced plastics
- CVD:
-
Cold vapour deposition
- CTE:
-
Coefficient of thermal expansion
- ECF:
-
Expanded copper foil
- ESN:
-
Electrical structure network
- IS13:
-
Integration scenario 13
- LSP:
-
Lightening strike protection
- NDI:
-
Non-destructive inspection
- PVD:
-
Physical vapour deposition
Acknowledgments
The research leading to these results has received funding from the European Union’s Seventh Framework Programme for research, technological development and demonstration under Grant Agreement No 284562.
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© 2016 Springer International Publishing Switzerland
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Altkvist, C., Wahlbäck, J., Tauchner, J., Breu, C. (2016). Design and Manufacturing of WP135 Side Panel for Validation of Electrical Structure Network (ESN) Technologies. In: Wölcken, P., Papadopoulos, M. (eds) Smart Intelligent Aircraft Structures (SARISTU). Springer, Cham. https://doi.org/10.1007/978-3-319-22413-8_56
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DOI: https://doi.org/10.1007/978-3-319-22413-8_56
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Publisher Name: Springer, Cham
Print ISBN: 978-3-319-22412-1
Online ISBN: 978-3-319-22413-8
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