Aircraft panel

Aeronautics and astronautics – Aircraft structure

Reexamination Certificate

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C244S123100, C244S132000

Reexamination Certificate

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07025305

ABSTRACT:
An aircraft panel comprising a sandwich construction with an outer skin portion of high strength material, an inner portion of high strength material and an intermediate core material. The core material includes areas with low density core material and a reinforcement grid of high strength material, with longitudinal and transversal grid members.

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patent: 19715529 (1998-08-01), None

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