Flugzeug und Verfahren zum Betrieb

Details

Veröffentlichungs-Nr.

EP4741289

Anmeldetag

5. November 2025

Veröffentlichung

13. Mai 2026

Rechtsraum

EP

IPC

B64D33/04, F02K1/00, F02K1/06

Abstract

An aircraft (10) includes an engine (20) defining a centerline axis (24), the engine (20) comprising a fan (22) and a turbomachine (54) rotatably driving the fan (22), the turbomachine (54) including an exhaust section (36) comprising an outlet nozzle (38), the outlet nozzle (38) including a fixed portion (40) and a movable portion (42), wherein the movable portion (42) is movable from a first position to a second position, wherein when the movable portion (42) is in the first position, the movable portion (42) is aligned with the centerline axis (24), and wherein when the movable portion (42) is in the second position, the movable portion (42) is canted downward in the vertical direction and outward in the lateral direction relative to the centerline axis (24), and wherein the movable portion (42) includes an end (44) engaging the fixed portion (40), wherein when the movable portion (42) is in the first position, the end (44) defines a nonzero cant angle with the centerline axis (24).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA