AIRCRAFT ENGINE WITH AN IMPACT PANEL

An impact panel 100 for a fan casing 40 having a support layer 120 that includes a set of partitioned cavities 110 with open faces 112 and comprising a polymer matrix composite 114 having a nanostructure 116.

» Number: EP3205846A1 (A1)

» Publication Date: 16/08/2017

» Applicant: GEN ELECTRIC?[US]

» Inventor: GEMEINHARDT GREGORY CARL?[US]; SCHULTE MICHAEL DOMINIC?[US]

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This project has received funding from the European Union's Horizon 2020 research and innovation programme under grant agreement Nº 768737