A ducted fan for an aircraft includes a rotor-side fan and a stator-side duct that surrounds the rotor-side fan. The stator-side duct includes an inner wall facing the rotor-side fan and an outer wall averted from the fan. The inner wall and outer wall each includes at least one layer composed of fiber-reinforced plastic. At least two honeycomb cores are arranged between the inner wall and the outer wall, the at least two honeycomb cores abutting against one another in an axial direction of the ducted fan. The honeycombs of the at least two honeycomb cores extend at least substantially in a radial direction of the ducted fan. A first of the at least two honeycomb cores is, at least in a region of an abutting surface that adjoins another of the at least two honeycomb cores, enwound or encased by at least one layer composed of fiber-reinforced plastic.
DUCTED FAN OF AN AIRCRAFT, AIRCRAFT, AND COMPONENT THEREOF
2022-04-14
Patent
Electronic Resource
English
DUCTED FAN OF AN AIRCRAFT, AIRCRAFT, AND COMPONENT THEREOF
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