In one embodiment, a horizontal stabilizer (200) comprises an airfoil structure (210) configured to be mounted to an aircraft (100) at a horizontal orientation. The airfoil structure (210) comprises a leading edge (202), a trailing edge (204), a top surface (212), and a bottom surface (213). Moreover, the airfoil structure (210) is cambered (211), wherein a camber (211) of the airfoil structure (210) forms a concave slope on the top surface (212) and a convex slope on the bottom surface (213).
AIRCRAFT HORIZONTAL STABILIZER DESIGN
KONSTRUKTION HORIZONTALER FLUGZEUGSTABILISATOREN
CONCEPTION DE STABILISATEUR HORIZONTAL D'AÉRONEF
2019-06-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2024
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