Fuselage component for an aircraft, method for producing a fuselage component, and aircraft
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United States of America Patent
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Jan 24, 2023
Grant Date -
Jun 25, 2020
app pub date -
Dec 19, 2019
filing date -
Dec 20, 2018
priority date (Note) -
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status (Latency Note)
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Abstract
A fuselage component for an aircraft, including a shell part composed of a fiber composite material and a stiffening structure which is connected to an inner surface of the shell part and has shaped parts composed of a fiber composite material, wherein the shaped parts each have a flat base section which extends along the inner surface of the shell part, and a step-shaped profile edge which extends in an encircling manner around the base section. The shaped parts are arranged in the form of parquetry with overlapping profile edges. As a result, the overlapping profile edges form stiffening profiles intersecting at an intersection. Furthermore, an aircraft which has at least one such fuselage component and a method for producing a fuselage component are described.
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