A composite structural component

G - Physics – 10 – K

Patent

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G10K 11/16 (2006.01) B29C 70/08 (2006.01) B29C 70/22 (2006.01) B29D 24/00 (2006.01) B32B 3/12 (2006.01) B32B 37/16 (2006.01) B64D 29/00 (2006.01) E04C 2/36 (2006.01) F02C 7/24 (2006.01) G10K 11/172 (2006.01)

Patent

CA 2064755

Fatigue, the phenomenon of structural or system failure, caused by repeated excitations from high frequency noise or vi- bration levels, can occur without warning in inlet cowls, fans ducts and thrust reverser translating cowls of aero engines. In mod- ern day nacelle and fan duct design, the use of composite structures predominates and a composite structural component is pro- vided which does not suffer or does not suffer to the same extent from such potential fatigue problems. The structural component has a front face for exposure to fatigue generating energy and includes a composite frontal region which includes the front face and which comprises a matrix (38) and a high fatigue-strength metal or metal alloy mesh (39) embodied within the matrix (38) or partially embodied within it at the front face. The matrix (38) is in sheet form and comprises or includes a synthetic resin.

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