Paralleles Hybrides Elektrisches Vertikalstart- und -Landeflugzeug

Details

Veröffentlichungs-Nr.

EP4759708

Anmeldetag

20. November 2025

Veröffentlichung

17. Juni 2026

Rechtsraum

EP

Abstract

A vertical takeoff and landing aircraft, includes a main rotor system, a gearbox mechanically connected to the main rotor system, a first gas turbine engine mechanically connected to the gearbox, a first electrical motor-generator mechanically connected to the first gas turbine engine and mechanically connected to the gearbox, a second electrical motor-generator mechanically connected to the gearbox, a third electrical motor electrically connected to the second electrical motor-generator and mechanically connected to an anti-torque device, the third electrical motor configured to provide mechanical power to the anti-torque device, and a plurality of power-controller interface units. The plurality of power-controller interface units are configured to, during a first phase of flight, control the first gas turbine engine and the first electrical motor-generator to provide mechanical power to the gearbox, and control the second electrical motor-generator to provide electrical power to the third electrical motor.

Anmelder

Firma

Lockheed Martin Corporation

Land

🇺🇸 USA