Multikopter mit Flügeln zum Vertikalen Starten und Landen

Details

Veröffentlichungs-Nr.

EP4818035

Anmeldetag

1. April 2025

Veröffentlichung

7. Oktober 2026

Rechtsraum

EP

Abstract

Winged vertical take-off and landing multi-copter comprising a first frame (10), defining a first longitudinal, transversal and sagittal directions (X1, Y1, Z1), supporting multiple first propellers (11), rotatable around the first sagittal direction (Z1); a second frame (20), defining a second longitudinal, transversal and sagittal directions (X2, Y2, Z2), supporting at least one fixed wing (22) and multiple second propellers (21), rotatable around the second sagittal direction (Z2); the first and second frames (10, 20) are connected through a rotative joint free to rotate about an axis parallel to the first and second transversal directions (Y1, Y2); the at least one electric source (30) and the control unit (40) are connected to the first and second propellers (11, 21) and are configured to independently control the pitch angle of the first and second frames through the differential control of the thrust produced by the first and second propellers (11, 21).

Anmelder

Firma

Fuvex Civil, SL

Land

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