Umwandelbares Luftfahrzeug, das Schweben Kann

Details

Veröffentlichungs-Nr.

EP4653316

Aktenzeichen

EP24425020

Anmeldetag

24. Mai 2024

Veröffentlichung

26. November 2025

Rechtsraum

EP

IPC

B64C29/00B64C39/12B64U10/20B64U30/297

Abstract

There is described an aircraft (1, 1', 1", 1‴, 1"", 1‴ʺ, 1‴‴ 1‴‴) comprising a structure (2) comprising, in turn, a nose (4) and a tail (5); a pair of half-wings (3); a first and a second rotor (20a, 20b) respectively rotatable around a third and fourth axis (B, C); a third and a fourth rotor (21a, 21b) respectively rotatable around a fifth and sixth axis (D, E); and a fifth and a sixth rotor (22a, 22b) carried by respective half-wings (3) and respectively rotatable around a seventh and eighth axis (F, G) with respect to the structure (2); the aircraft (1, 1', 1" , 1‴, 1"", 1‴ʺ, 1‴‴ 1‴‴) is switchable between a first hovering or taking off/landing configuration wherein the seventh and eighth axis (F, G) are arranged orthogonal to the first axis (Y); and a second forward flight configuration wherein the seventh and eighth axis (F, G) are arranged parallel or inclined with respect to the first axis (Y); the aircraft ((1, 1', 1", 1‴, 1ʺʺ, 1‴ʺ, 1‴‴ 1‴‴) comprises a first support beam (30) supporting the first, third and fifth rotor (20a, 21a, 23a); and a second support beam (31) supporting the second, fourth and sixth rotor (20b, 21b, 23b) each connected to a respective half-wing (3) and to a respective aerodynamic surface (9). (Fig. 1)

Anmelder

Firma

Leonardo S.p.a.

Land

🇮🇹 Italien

Fachgebiete