AIRCRAFT HORIZONTAL STABILIZER DESIGN

AIRCRAFT HORIZONTAL STABILIZER DESIGN

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). Moreove...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: 0'NEIL, Joshua R, LANIGAN, Brendan P
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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).