#AIRBUS HELICOPTERS [FR]

MULTI-ENGINE AIRCRAFT PROVIDED WITH AT LEAST ONE AIR SUPPLY DUCT EQUIPPED WITH AN AIR DEFLECTOR

The present invention relates to an aircraft (1) comprising a first turbine engine (21) and a second turbine engine (31) supplied with air respectively by a first air supply system (401) and a second …

DRIVE·Jun 10·1 min read

B64D33/02 AIRBUS HELICOPTERS [FR]

METHOD FOR AUTOMATICALLY CONTROLLING AN AIRCRAFT IN THE PRESENCE OF A FIRE IN AN ENGINE ZONE AND AN AIRCRAFT

The present invention concerns a method for controlling an aircraft (1) comprising at least two engines (16, 17), each engine (16, 17) being arranged in its own engine compartment (21, 22), each engin…

DRIVE·Apr 15·2 min read

A62C3/08 AIRBUS HELICOPTERS [FR]

AIRCRAFT PROVIDED WITH A HEATING SYSTEM FOR A TURBINE ENGINE PLENUM

Aircraft (1) fitted with a turbine engine (10) comprising a gas generator (15), the gas generator (15) comprising a compression assembly (20) supplying air to a combustion chamber (24) as well as a tu…

DRIVE·Feb 25·1 min read

B64D33/02 AIRBUS HELICOPTERS [FR]

METHOD FOR CONTROLLING A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND COMPUTER PROGRAM

The present invention relates to a method for controlling a rotorcraft (1), said rotorcraft (1) comprising at least two combustion engines (2, 3), at least one control system (13) and a transmission s…

DRIVE·Feb 25·1 min read

B64C27/04 AIRBUS HELICOPTERS [FR]

PARTITION FOR A VEHICLE COMPRISING A DEVICE FOR ASSISTING THE EVACUATION OF PERSONS BY AN EMERGENCY EXIT FROM THE PARTITION

The present invention relates to a partition for a vehicle (10) comprising a structure (41) pierced with an opening (43) forming an emergency exit (44) closed off by a movable panel (45) as well as an…

DRIVE·Dec 24·2 min read

B60Q3/46 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·Nov 26·2 min read

B64C27/08 AIRBUS HELICOPTERS [FR]

ACTUATOR PROVIDED WITH TWO PRESSURE SENSORS AND A VIRTUAL PRESSURE SENSOR; A BRAKING SYSTEM AND AN AIRCRAFT PROVIDED WITH SUCH AN ACTUATOR, AND THE APPLIED METHOD

The present invention relates to an actuator (10) equipped with a pump (15) connected to a first hydraulic line (30) connected to a reservoir (25) and to a second hydraulic line (35). A control contro…

DRIVE·Nov 12·2 min read

B60Q9/00 AIRBUS HELICOPTERS [FR]

METHOD FOR TRAINING THE PILOTING OF A ROTORCRAFT, ASSOCIATED SYSTEM AND ROTORCRAFT

The present invention relates to a method of training for the piloting of a rotorcraft (1) comprising at least two engines (3, 4) and at least one rotor (5) participating in the lift of said rotorcraf…

DRIVE·Aug 13·1 min read

B64D31/10 AIRBUS HELICOPTERS [FR]

METHOD AND DEVICE FOR ENTERING AND EXITING AN ECONOMICAL OPERATING MODE FOR A TWIN-ENGINE AIRCRAFT

The present invention relates to a method of controlling an economical operating mode for an aircraft (1) comprising two heat engines (11), only one of said heat engines (11) being active and supplyin…

DRIVE·Jun 25·1 min read

B64C27/12 AIRBUS HELICOPTERS [FR]

METHOD AND DEVICE FOR ASSISTING THE PILOTING OF AN AIRCRAFT WITH A HEAD-UP DISPLAY

The present invention relates to a method for assisting in the piloting of an aircraft (1) comprising a head-up display (30) and an autopilot system (20) which comprises a human-machine selection inte…

DRIVE·Jun 25·2 min read

B64C13/18 AIRBUS HELICOPTERS [FR]

METHOD FOR CONTROLLING A MULTI-ENGINE ROTARY WING AIRCRAFT WITH REDUCED FUEL CONSUMPTION ON THE GROUND

The present invention relates to a method for piloting an aircraft (1) having at least two engines (10) burning fuel and a transmission chain (25) connected to a rotary wing (5), each engine (10) havi…

DRIVE·Jun 11·1 min read

B64C27/12 AIRBUS HELICOPTERS [FR]

AIRCRAFT PROVIDED WITH AN ENGINE AND A DRAIN CONDUIT WHICH IS ARRANGED AROUND AN EXHAUST DUCT OF THE ENGINE

The present invention relates to an aircraft (1) equipped with an engine compartment (5), said aircraft (1) comprising a motor (10) housed at least partially in the engine compartment (5), the motor (…

DRIVE·Jun 4·1 min read

B64C1/1453 AIRBUS HELICOPTERS [FR]

A DISPLAY SYSTEM FOR AN AIRCRAFT

The present invention relates to a display system (10) for an aircraft, comprising at least one first display unit (16); at least one second display unit (18); a control unit (20) that is configured t…

DRIVE·May 14·1 min read

G01C23/00 AIRBUS HELICOPTERS [FR]

AIRCRAFT HAVING AN EXHAUST CONDUIT COUPLED TO A STABILIZATION SYSTEM

The present invention relates to an aircraft (1) equipped with at least one exhaust duct (30) for ejecting gases from an engine (10), the exhaust duct (30) being partially housed in an internal housin…

DRIVE·Jan 15·2 min read

B64C27/04 AIRBUS HELICOPTERS [FR]

METHOD FOR AUTHORIZING THE FLIGHT OF AN AIRCRAFT HAVING A HYBRID POWER PLANT PROVIDED WITH AT LEAST ONE ELECTRIC MOTOR AND AT LEAST ONE HEAT ENGINE

The present invention concerns a method for authorizing flight of an aircraft (1) equipped with a hybrid power plant installation (10) having at least one thermal engine (15) and at least one electric…

DRIVE·Jan 15·2 min read

B60L3/0046 AIRBUS HELICOPTERS [FR]

METHOD AND AIRCRAFT HAVING AT LEAST ONE COMBUSTION ENGINE AND A DRIVE SYSTEM HAVING AT LEAST TWO ELECTRIC MACHINES

The present invention relates to an aircraft (1) provided with a power plant (10) provided with at least one combustion engine (20) mechanically connected to a drive system (30), the drive system (30)…

DRIVE·Dec 18·2 min read

B64D27/02 AIRBUS HELICOPTERS [FR]

AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND A DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT

The present invention relates to an aircraft (1) and a method for controlling such an aircraft (1) comprising two turbine engines (11, 12), an electrical machine (4), an electrical power source (5) an…

DRIVE·Nov 6·2 min read

B64C27/12 AIRBUS HELICOPTERS [FR]

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

DRIVE·Jul 10·2 min read

B64C27/08 AIRBUS HELICOPTERS [FR]

A VEHICLE CONTROL SYSTEM FOR AUTONOMOUS, REMOTELY-CONTROLLED, OR MANUAL OPERATION OF A VEHICLE

The present embodiments relate to a vehicle control system 350 for controlling a vehicle and to a method 800 of operating such a vehicle control system. The vehicle control system 350 may include an i…

DRIVE·Jan 12·1 min read

B60W10/08 AIRBUS HELICOPTERS [FR]

A device for protecting an individual sitting on a seat, a seat, and a vehicle

The present invention relates to a protection device (10) having a set (15) of inflatable protection members including a neck airbag (21), a left lower airbag (22), a left upper airbag (32), a right l…

DRIVE·Sep 16·2 min read

B60R21/18 AIRBUS HELICOPTERS [FR]

FUEL STORAGE SYSTEM WITH TANKS COUPLED BY FLEXIBLE LINES

Fuel storage system (9) comprising at least two tanks (10,20,30) and at least one removable connection device (50), each tank (10,20,30) having at least one flexible conduit (11,21,31), each removable…

DRIVE·Dec 31·1 min read

B64D37/08 AIRBUS HELICOPTERS [FR]

System for heating the passenger compartment of an aircraft provided with an annular heat exchanger around the exhaust nozzle

The present invention relates to a heating system (50) for a cabin (2) of an aircraft (1) comprising an annular heat exchanger (10) positioned around an exhaust duct (21) of a turbine engine (20) and …

DRIVE·Dec 24·2 min read

B60H1/18 AIRBUS HELICOPTERS [FR]

Anti-crash seat, and aircraft

The present invention relates to a seat (5) comprising a bucket (10) and a frame (15) fixed to a floor (2). Said seat (5) comprising at least one energy absorption system (20) provided with a pluralit…

DRIVE·Dec 17·1 min read

B60N2/54 AIRBUS HELICOPTERS [FR]

Method for approaching a platform

A method comprising a development phase for developing an approach trajectory (25) towards a theoretical position (20') of a platform (20). During a consolidation phase, the current position (20") of …

DRIVE·Dec 10·1 min read

G01C21/20 AIRBUS HELICOPTERS [FR]

Human-machine interface with designating means and armrest, and vehicle

The present invention relates to a human-machine interface (10) of a vehicle (1) equipped with a designation means (40). The interface (10) comprises a base and a support (20) extending in elevation f…

DRIVE·Dec 3·1 min read

A47C7/54 AIRBUS HELICOPTERS [FR]

Volute casing with two volumes for gas turbine

The present invention relates to a dual-volume volute (10) for a gas turbine (50) comprising a circumferential spiral-shaped conduit (11), a first opening (12) arranged tangentially to said circumfere…

DRIVE·Nov 5·1 min read

F01D9/026 AIRBUS HELICOPTERS [FR]

Anti-scratch method for a windscreen of a vehicle, and windscreen wiper implementing said method

The method involves determining if a windscreen (5) of a vehicle (1) i.e. helicopter, is dried with the aid of a water sensor (70), when a manual operation of each wiper (10) is required. A washer flu…

DRIVE·Oct 1·1 min read

B60S1/0818 AIRBUS HELICOPTERS [FR]

Seat for powered aircraft having a leg assembly comprising three points for anchoring to the floor of the aircraft

The seat has a base that is arranged for carrying a bucket seat through an energy absorbing unit. The base is arranged with an establishment frame (5) on an installation plane (P1) on the base. The es…

DRIVE·Jul 30·1 min read

B60N2/015 AIRBUS HELICOPTERS [FR]

System for monitoring the start of a rotary wing aircraft, aircraft and method implementing this system

The system (20) has a measurement device (40) measuring torque exerted on an upstream portion (11) of a drive train (10) when mounted. Another measurement device (50) measures speed of rotation of a g…

DRIVE·Jul 23·1 min read

B64D45/00 AIRBUS HELICOPTERS [FR]

Method for rotating a rotorcraft rotor, by anticipating torque requirements between two set speeds of rotation of the rotor

The method involves identifying a necessary speed (NR) of a swing drive of a main rotor (1) by a control unit (10). The necessary speed is calculated by application of a calculation rule integrating a…

DRIVE·Jul 2·1 min read

B64C27/04 AIRBUS HELICOPTERS [FR]

Device for wirelessly supplying power to devices installed inside an aircraft

The device (50) has an electric harness (5) that is provided with two electric drivers (6) that are electrically connected to an electrical supply source (8) of a vehicle i.e. aircraft. A transmitting…

DRIVE·May 21·1 min read

B60N2/0264 AIRBUS HELICOPTERS [FR]

Method and active device for dealing with noise on board a vehicle, and vehicle provided with such a device

The device has a position sensor determining a position of a head of a passenger. A treatment unit is connected to a local noise sound sensor to receive a local noise signal, and delivers a control si…

DRIVE·Apr 30·1 min read

B60N2/879 AIRBUS HELICOPTERS [FR]