STRUCTURAL ELEMENT OF AN AIRCRAFT

摘要

The invention concerns a rear frame of an air intake of a nacelle of an aircraft, characterized in that it is partly made of fiber-reinforced geopolymer resin-based composite material and comprises at least one part (56) that surrounds an opening provided for the passage of a de-icing system made of fiber-reinforced geopolymer-resin based composite material and at least one other part (58) made of metal.