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Multilayer ceramic composite and method of production

An aircraft part has a multilayer ceramic composite that includes an inner skin, a ceramic insulation core, and an outer skin. The inner skin includes a plurality of layers of fiberglass impregnated with a thermoset resin. The ceramic insulation core is sufficiently flame resistant to prevent penetration of a flame with a temperature of about 2000 degrees F. for at least 15 minutes when the aircraft part is directly exposed to the flame. The outer skin includes a plurality of layers of fiberglass impregnated with a thermoset resin. The multilayer ceramic composite is manufactured using a novel method that provides superior performance at a reduced cost.


» Number: US10195819B1 (B1)

» Publication Date: 19//2/05/0

» Applicant: DONNELLY FRED D?[US]

» Inventor: DONNELLY FRED D?[US]

» More Information

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This project has received funding from the European Union Seventh Framework Programme (FP7/2007-2013) under grant agreement n [310187].