Propellerbaugruppe für ein Flugzeug

Details

Veröffentlichungs-Nr.

EP3434589

Aktenzeichen

EP18185725

Anmeldetag

26. Juli 2018

Veröffentlichung

4. November 2020

Erteilung

4. November 2020

Rechtsraum

EP

IPC

B64C27/57B64C27/43B64C27/59// B64C29/00B64C39/02

Abstract

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).

Anmelder

Firma

Airbus Defence and Space GmbH

Land

🇩🇪 Deutschland

Fachgebiete