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US 2025/0136293 A1Published application
Aircraft control surface
AssigneeRohr, Inc.
InventorJennifer Davis
Life of this patent
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Abstract
A monolithic control surface includes an upper shell portion, a lower shell portion, a stringer connected to the upper shell portion and the lower shell portion, a trailing edge end, and a solid trailing edge region connected to the upper shell portion, the lower shell portion and the stringer.
Claims5
A monolithic control surface, comprising:
- an upper shell portion;
- a lower shell portion;
- a stringer connected to the upper shell portion and the lower shell portion;
- a trailing edge end;
- and
- a solid trailing edge region connected to the upper shell portion, the lower shell portion and the stringer.
3 more elements
Dependencies are inferred from the claim text.