Abstract
The design of composite structures currently employed in commercial aircraft is closely related to their metallic counterparts. Significant changes to the conventional design philosophy are required to provide competitive solutions for next-generation aircraft. Due to the inherently large design freedom associated with composite material, this can be achieved through a rigorous integral and multifunction design approach. Three highly promising concepts are introduced in this chapter:
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1.
Disbond-arrest features for adhesively bonded composite joints, which present an enabling technology for integral design solutions.
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2.
Selective stitching, to enhance the damage tolerance of integral composite structure.
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3.
Composite sandwich structures that provide the greatest design freedom to integrate structural as well as nonstructural functionalities.
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Notes
- 1.
Where “U” stands for unstitched, “T” for tufting, “BS” for blind stitching, and “L”, “M,” and “H” for low, medium, and high stitching densities, respectively. The stitching thread materials used are represented by the letters “A” (aramid) and “C” (carbon).
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Sachse, R., Fernandez, D., Klett, Y., Middendorf, P. (2020). Integral, Disruptive, and Multifunctional Aircraft Structures. In: Pantelakis, S., Tserpes, K. (eds) Revolutionizing Aircraft Materials and Processes. Springer, Cham. https://doi.org/10.1007/978-3-030-35346-9_7
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