Fluidisches Antriebssystem

Details

Veröffentlichungs-Nr.

EP4737311

Anmeldetag

21. Januar 2020

Veröffentlichung

6. Mai 2026

Rechtsraum

EP

IPC

B64C23/00(MICHAEL STROUKOFF et al.)(EVULET ANDREI et al.)

Abstract

An aircraft includes a fuselage and at least one primary wing having an upper surface, at least one recess in the upper surface and at least one conduit in fluid communication with the at least one recess. At least one ejector is disposed within the at least one recess and is configured to receive compressed air via the at least one conduit.

Anmelder

Firma

Jetoptera, Inc.

Land

🇺🇸 USA

Fachgebiete