Abstract
In the context of developing competitive liquid composites molding processes for primary aircraft structures, modeling the forming stage of automatically-placed initially flat stacks of dry reinforcements is of great interest. In the case of HiTape®, a dry unidirectional carbon fiber reinforcement designed to achieve performances comparable to state-of-the-art pre-impregnated materials, the presence of a thermoplastic veil on each side of the material for both processing and mechanical purposes should also be considered when modeling forming in hot conditions. As a dry unidirectional reinforcement, HiTape® is expected to exhibit a transversely isotropic behavior. Computation cost and strong characterization challenges led us to model its behavior at the forming process temperature (above the thermoplastic veil melting temperature) through a homogeneous equivalent continuous medium exhibiting four ‘classical’ deformation modes and a specific structural mode, namely out-of-plane bending. The response of both single plies and stacks of HiTape® to this latter structural mode was characterized at the forming process temperature using a modifiedPeirce flexometer. Results on single plies showed a non-linear softening moment-curvature behavior and a corresponding flexural stiffness much lower than what can be inferred from continuum mechanics. Moreover, testing stacks revealed that the veil acts as a thin load transfer layer between the plies undergoing relative in-plane displacement,i.e.inter-ply sliding. This inter-ply response was then characterized separately at the forming process temperature thanks to a specific method relying on apull-throughtest. Experiments performed at pressures and speeds representative of the forming stage revealed that a hydrodynamic lubricated friction regime predominates,i.e.a linearly increasing relationship between the friction coefficient and the modified Hersey number. From an industrial point of view, high forming pressures and low speeds are therefore recommended to promote inter-ply slip to limit the occurrence of defects such as wrinkles.
Highlights
Composite materials have been recognized as optimal solutions for lightweight structures in the industry of transportation
Such characterization works need to be conducted under conditions as close as possible from double-membrane vacuum hot forming process, at the forming process temperature and for external pressures between 0.5 and 1.5 bar
® In order to characterize the non-linear bending behavior of HiTape at ply scale and at the forming process temperature (Tproc) which is above the melting temperature of the TP veil (Tmelt), a modified flexometer based on the same principle than previous studies was designed
Summary
Composite materials have been recognized as optimal solutions for lightweight structures in the industry of transportation. The best performances are reached with long fiber semi-products pre-impregnated with non-consolidated organic resin, and processed in autoclave environments. In the context of continuous cost reduction and production rate increase, liquid composites molding (LCM) processes (Hexcel, 2015a) appear as ideal routes for manufacturing primary aircraft structures. These Out-of-Autoclave (OOA) processes consist in draping and shaping dry composite semi-products, and inject (for Resin Transfer Molding for instance) or infuse (in infusionbased processes) liquid resins in this potentially complex fibrous architecture
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