Flow Body With A Load Introduction Element Integrated Therein, Method For Manufacturing A Flow Body, And Aircraft With Such A Flow Body

摘要

A flow body for an aircraft with a leading edge and a trailing edge includes a first spar, a second spar, and an external skin that spans from the leading edge to the trailing edge and on both sides rests on the spars. At least one of the first spar and the second spar includes a web and two spaced-apart flanges that enclose the web, on which flanges the skin that spans the respective spar is arranged. At least one of the first spar and the second spar includes at least one load introduction fin that forms an integral component with the web and extends outwards by way of one of the flanges and the skin that rests on the spars.

主权项

1. A flow body for an aircraft, the flow body with a leading edge and a trailing edge, comprising:
a first spar; a second spar; and an external skin spanning from the leading edge to the trailing edge and on both sides resting on the spars; wherein at least one of the first spar and the second spar comprises a web and first and second spaced-apart flanges enclosing the web, on which flanges the skin spanning the respective spar is arranged, and wherein at least one of the first spar and the second spar comprises at least one load introduction fin forming an integral component with the web and extending outwards by way of one of the flanges and the skin.