METHOD FOR PRODUCING A FUSELAGE STRUCTURAL COMPONENT FOR A TRIANGLE REGION, AND INTEGRAL FUSELAGE STRUCTURAL COMPONENT
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United States of America Patent
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Issued Date -
Aug 29, 2024
app pub date -
Feb 12, 2024
filing date -
Feb 27, 2023
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Abstract
A method for producing a fuselage structural component for a triangle region of an aircraft by: providing an integral board of a former material, wherein the board has an opening; and deforming at least one internal edge of the board that forms the opening to an internal flange; and deforming at least one external edge of the board to an external flange. Adjacent to the opening, the integral and deformed board forms in each case a former portion, a floor beam and a vertical support. Also a fuselage structural component and an aircraft with the fuselage structural component.
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