Airbus Helicopters Deutschland Gmbh

Marco Schneeberger

Sebastian Mores

Marius Bebesel

Stefan Probst

Uwe Kiesewetter

Martin Blacha

Christian Reichensperger

Michael Geiss

Qinyin Zhang

Markus Paschek

Johann Barnerssoi

Hartmut Jutt

Klaus Rittel

An aircraft with an airframe and at least one thrust producing unit the at least one thrust producing unit being electrically powered by an associated electrical engine that is electrically connected to an electrical energy source via an electrical energy distribution system, wherein the airframe comprises at least one load carrying section and at least one propulsion system carrying section, wherein the at least one load carrying section and the at least one propulsion system carrying section are segregated from each other, wherein the at least one load carrying section is provided for transportation of passengers and/or cargo, and wherein the at least one propulsion system carrying section is provided for carrying at least essentially the electrical energy source and the electrical energy distribution system.

Aircraft with an airframe and at least one electrically powered thrust producing unit

A multirotor aircraft with an airframe and a thrust producing units arrangement, wherein the thrust producing units arrangement comprises a predetermined number of thrust producing units for producing thrust in a predetermined direction, and wherein a flexible suspension unit is rigidly mounted to the airframe, wherein the flexible suspension unit comprises at least one bearing that mechanically couples the thrust producing units arrangement to the airframe such that the thrust producing units of the predetermined number of thrust producing units are inclinable in relation to the airframe.

Multirotor aircraft with an airframe and a thrust producing units arrangement

An aircraft with a fuselage that comprises a framework structure having at least one hollow frame that is integrally formed in one piece and comprises fiber reinforced polymers, the at least one hollow frame defining an integrated ventilation air duct that is adapted for guiding ventilation air into the aircraft.

Aircraft framework structure with integral ventilation air duct

Growing community of inventors

Rosenheim, Germany

Marco Schneeberger