A HELICOPTER TAIL FOLDING SYSTEM

A HELICOPTER TAIL FOLDING SYSTEM

A tail located on a helicopter has a front area located on the tail, a rear area connected to the front area in a foldable manner around the axis, and a first shaft at the front area and a second shaft at the rear area allows power transfer to the tail rotor throughout the flight movement of the hel...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: YILMAZ, Furkan
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A tail located on a helicopter has a front area located on the tail, a rear area connected to the front area in a foldable manner around the axis, and a first shaft at the front area and a second shaft at the rear area allows power transfer to the tail rotor throughout the flight movement of the helicopter. A first coupling and a second coupling are located on the first shaft in a gear form. A first hub on the first shaft surrounds the first coupling and is form-compatible with the first coupling to allow the first coupling to perform at least partially a spherical rotational movement, and a second hub form-compatible with the second coupling located on the second shaft opposite the second coupling.