PROPELLER ARRANGEMENT FOR AN AIRCRAFT

PROPELLER ARRANGEMENT FOR AN AIRCRAFT

A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) a...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Bichler, Bartholomaeus, Judas, Michael
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A propeller arrangement (100) for an aircraft, and an aircraft having a propeller arrangement of said type, are specified. The propeller arrangement (100) has a first propeller blade (110) and a second propeller blade (120), and a propeller mount (130) on which both the first propeller blade (110) and the second propeller blade (120) are mounted. The propeller arrangement (100) furthermore has a drive shaft (140) with a holding unit (160), and a first connecting unit (150). The first propeller blade (110) is rotatable about a first axis of rotation (112) and the second propeller blade (120) is rotatable about a second axis of rotation (122). The propeller mount (130) is pivotable about a pivot axis (132). The first connecting unit (150) is coupled to the first propeller blade (110) and to the holding unit (160), such that, in the event of a pivoting of the propeller mount (130) about the pivot axis (132), the first propeller blade (110) is set in rotational motion about the first axis of rotation (112).