Hinterer Endabschnitt für ein Flugzeug

Details

Veröffentlichungs-Nr.

EP3904202

Aktenzeichen

EP20382351

Anmeldetag

29. April 2020

Veröffentlichung

7. Juni 2023

Erteilung

7. Juni 2023

Rechtsraum

EP

IPC

B64C1/06B64C1/00B64C9/38B64C21/06B64D27/14

Abstract

The invention refers to a rear end section (1) for an aircraft, having a fuselage (4), a v-tail (2), and a thruster assembly (3) comprising: at least one propulsion device (5) installed to ingest and consume air forming a fuselage boundary layer, a control surface (6) attached at the rearmost section of the rear end, and a casing (7) covering at least part of the propulsion device (5) such that an air inlet (8) and an air outlet (9) are defined between the casing (7) and the propulsion device (5), the air inlet (8) being designed for the passage of the fuselage boundary layer towards the propulsion device (5), and the air outlet (9) being designed for directing the airflow exhausted from the propulsion device (5) into the control surface (6), to divert said airflow and provide vectoring thrust for the aircraft.

Anmelder

Firma

Airbus Operations, S.L.

Land

🇪🇸 Spanien

Fachgebiete