An aircraft (1) is described comprising a pilot cockpit (10); a windshield (11) delimiting the cockpit (10); a windscreen wiper (14, 15) comprising a plurality of nozzles (16, 17); a first tank (20) filled with a cleaning fluid and fluidically connected wi...

A transmission assembly (3; 3'; 3"; 3ʹʹʹ; 3ʺʺ; 3‴ʺʹ; 3‴‴; 3‴‴′ʹ; 3‴‴ʺ) for an aircraft (1; 1'; 1"; 1ʹʹʹ. 1ʺʺ; 1‴ʺ; 1‴‴; 1‴‴′; 1‴‴ʺ), comprising a member to be lubricated (18; 40; 1800; 1801; 1400; 1401) for t...

A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described, the control unit (46, 46') is programmed to receive at input at least a first signal associated with real or simula...

Aircraft (1) capable of hovering comprising a fuselage (2), at least one rotor (3a, 3b, 4) that is rotatable with respect to the fuselage (2), electrical drive means adapted to rotate the rotor (3a, 3b, 4) and electrically powered by a battery (9), and a c...

A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described; the control unit (46, 46') is programmed to: - receive in input a plurality of data associated with equipment (15) ...

There is described a method for estimating rotor torques (TQ, TQ) of an aircraft (1) capable of hovering; the aircraft (1) comprises a first and a second rotor (31, 32), which are operatively connected to one another and rotatable under the action of respe...