Protective edge members for composite flexures

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/32 (2006.01) B64C 27/33 (2006.01)

Patent

CA 2320606

The protective edge member (51, 53) for use on a composite flexure, such as a helicopter main rotor yoke (11), having an exposed edge surface (24), comprises an innermost composite ply (57) attached to the exposed edge surface (24), an outermost composite ply (59) attached to the innermost composite ply (57); and at least one interior composite ply (55) disposed between the innermost composite ply (57) and the outermost composite ply (59).

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