An aircraft structural component includes a flange having a non-planar side and a web having a first end extending from the non-planar side of the flange and a second end distal from the first end and from the non-planar side of the flange wherein the web has a non-planar shape that deviates from a plane normal to the non-planar side of the flange and extending in a longitudinal direction of the aircraft structural component, so that a deviation of the non-planar shape of the web from the plane increases with distance along the web in a direction from one of the first and second ends to the other of the first and second ends, and so that the deviation extends over at least 10 cm of a length of the aircraft structural component.
AIRCRAFT STRUCTURAL COMPONENT AND A METHOD OF FABRICATING AN AIRCRAFT STRUCTURAL COMPONENT
2024-05-23
Patent
Electronic Resource
English
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