Longform — Long-form writing on the AT Protocol

A ROTARY WING AIRCRAFT WITH AT LEAST TWO ROTORS AND A PROPULSION UNIT

The present invention relates to a rotary wing aircraft 100 that extends along a roll axis R between a nose region 101 and an aft region 102, comprising: at least one first single-blade rotor 120 and …

DRIVE·Nov 26·2 min read

B64C27/08 AIRBUS HELICOPTERS [FR]

A ROTARY WING AIRCRAFT WITH AT LEAST TWO ROTORS AND A PROPULSION UNIT

The present invention relates to a rotary wing aircraft 100 that extends along a roll axis R between a nose region 101 and an aft region 102, comprising: at least one first single-blade rotor 120 and …

DRIVE·Jul 10·2 min read

B64C27/08 AIRBUS HELICOPTERS [FR]

MOTOR CONTROL SYSTEM, METHOD OF OPERATING A MOTOR CONTROL SYSTEM AND AIRCRAFT

We propose a motor control system (1), preferably for an aircraft, most preferably for a passenger and/or load carrying multi-rotor aircraft, comprising: a plurality of motors (3), preferably electric…

DRIVE·Jul 10·2 min read

B64C27/08 VOLOCOPTER GMBH [DE]

AERIAL VEHICLE

The invention is directed to an aerial vehicle with a hybrid drive unit (10) and with a rotor unit (1, 1') wherein the hybrid drive unit (10) comprises at least a combustion engine (11), a generator (…

DRIVE·Jun 7·2 min read

B64C27/08 SWISSDRONES OPERATING AG [CH]

MULTICOPTER

Provided is a multicopter providing a high level of freedom in compact design, and consuming a relatively small amount of energy. The multicopter () includes a machine body (), an N number of first li…

DRIVE·Apr 8·1 min read

B64C27/08 HONDA MOTOR CO., LTD.

#B64C27/08

A ROTARY WING AIRCRAFT WITH AT LEAST TWO ROTORS AND A PROPULSION UNIT

A ROTARY WING AIRCRAFT WITH AT LEAST TWO ROTORS AND A PROPULSION UNIT

MOTOR CONTROL SYSTEM, METHOD OF OPERATING A MOTOR CONTROL SYSTEM AND AIRCRAFT

AERIAL VEHICLE

MULTICOPTER