A rotor wing aircraft with a propulsion apparatus is disclosed. The aircraft has a rotating mast configured to rotate the rotor wing and the propulsion apparatus includes a pole mechanically connectable to the rotating mast of the aircraft. An electric turbine is placed at one of the ends of the pole, powered by a battery, and configured to rotate the pole around an axis of the rotating mast in such a way that the rotation of the pole can be used to rotate the rotor wing. The pole is made of carbon fiber.
An aircraft (100) with a rotary wing (40) is equipped with a propulsion system (10). The aircraft (100) includes a rotating mast (50) that rotates the rotor wing (40). The propulsion system (10) includes a pole (20) mechanically connected to the rotating mast (50) of the aircraft (100), where at least one end of the pole (20) is equipped with a motor (30) configured to rotate the pole (20) around the axis of the rotating mast (50) in such a way that the rotation of the pole (20) can be used to rotate the rotating wing (40). At each end of the pole (20) is placed a motor group (30), where each motor group (30) includes a pair of counter-rotating propellers (32,32), said pair of counter-rotating propellers (32,32′) being arranged in such a way as to generate a rotational torque to rotate the pole (20).
B64D 27/24 - Aircraft characterised by the type or position of power plants using steam or spring force
B64D 35/06 - Transmitting power from power plants to propellers or rotorsArrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors the propellers or rotors being counter-rotating
3.
ROTARY WING AIRCRAFT WITH IMPROVED PROPULSION SYSTEM
An aircraft (100) with a rotary wing (40) is equipped with a propulsion system (10). The aircraft (100) includes a rotating mast (50) that rotates the rotor wing (40). The propulsion system (10) includes a pole (20) mechanically connected to the rotating mast (50) of the aircraft (100), where at least one end of the pole (20) is equipped with a motor (30) configured to rotate the pole (20) around the axis of the rotating mast (50) in such a way that the rotation of the pole (20) can be used to rotate the rotating wing (40). At each end of the pole (20) is placed a motor group (30), where each motor group (30) includes a pair of counter-rotating propellers (32,32'), said pair of counter-rotating propellers (32,32') being arranged in such a way as to generate a rotational torque to rotate the pole (20).
A rotor wing aircraft provided with a propulsion apparatus is disclosed. The aircraft has a rotating mast configured to rotate said rotor wing and the apparatus includes a pole mechanically connectable to the rotating mast of the aircraft. At one of the ends of the pole there is placed an electric turbine, powered by a battery, and configured to rotate the pole around an axis of the rotating mast in such a way that the rotation of the pole can be used to rotate the rotor wing. Preferably the pole is made of carbon fiber.
An aircraft traffic control method comprises the following steps: - receiving data concerning the position of the aircrafts; - creating a real-time map of aircraft traffic based on the position data; - checking on the basis of the map the possibility of a collision between aircrafts, and - in the event that such check is positive, sending an anti- collision alert to theaircrafts, said method being implemented by means of an RTS server (Real Time Server) (120) configured to communicate with navigational devices (130) onboard of the aircrafts and provided with an application (150) configured to communicate data concerning the position of the aircrafts to RTS server (120).
A rotor wing aircraft (100) provided with a propulsion apparatus (10), wherein said aircraft (100) comprises a rotating mast (50) configured to rotate said rotor wing (40), said apparatus comprising a pole (20) mechanically connectable to the rotating mast (50) of the aircraft, wherein at one of the ends of said pole (20) there is placed an electric turbine (30), powered by a battery, and configured to rotate the pole (20) around an axis of the rotating mast (50) in such a way that the rotation of the pole (20) can be used to rotate the rotor wing (40). Preferably the pole (20) is made of carbon fiber.
B64C 27/14 - Direct drive between power plant and rotor hub
B64C 27/16 - Drive of rotors by means, e.g. propellers, mounted on rotor blades
B64C 27/82 - RotorcraftRotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting-rotor torque or changing direction of rotorcraft
B64C 27/18 - Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
7.
Method of estimating an attitude of a control device for controlling operating machines
A method of estimating an attitude of a control device for controlling operating machines, where the control device has a plurality of pushbuttons for controlling the movement of an operating machine along respective directions, the method having the following steps: —preliminary estimating the attitude of the control device using data from an accelerometer and a magnetometer onboard of the control device; —updating of the preliminary estimate of the attitude of the control device using data from a gyroscope onboard of the control device.
G05B 19/402 - Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by control arrangements for positioning, e.g. centring a tool relative to a hole in the workpiece, additional detection means to correct position
B66C 13/40 - Applications of devices for transmitting control pulsesApplications of remote control devices
G01C 21/08 - NavigationNavigational instruments not provided for in groups by terrestrial means involving use of the magnetic field of the earth
G05B 19/409 - Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by using manual data input [MDI] or by using control panel, e.g. controlling functions with the panelNumerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by control panel details or by setting parameters
G01C 21/16 - NavigationNavigational instruments not provided for in groups by using measurement of speed or acceleration executed aboard the object being navigatedDead reckoning by integrating acceleration or speed, i.e. inertial navigation
8.
METHOD OF ESTIMATING AN ATTITUDE OF A CONTROL DEVICE FOR CONTROLLING OPERATING MACHINES
A method of estimating an attitude of a control device for controlling operating machines, where the control device comprises a plurality of pushbuttons for controlling the movement of an operating machine along respective directions, the method comprising the following steps: - preliminary estimating the attitude of the control device using data from an accelerometer and a magnetometer onboard of the control device; - updating of the preliminary estimate of the attitude of the control device using data from a gyroscope onboard of the control device.
G05B 19/409 - Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by using manual data input [MDI] or by using control panel, e.g. controlling functions with the panelNumerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by control panel details or by setting parameters
B66C 13/40 - Applications of devices for transmitting control pulsesApplications of remote control devices
G01C 21/08 - NavigationNavigational instruments not provided for in groups by terrestrial means involving use of the magnetic field of the earth
G01C 21/18 - Stabilised platforms, e.g. by gyroscope
9.
Device and a process for controlling a swinging of a load suspended from a lifting apparatus
A device for controlling a swinging of a load suspended from a motorized slidable element is described. The controlling device includes a control unit and an inertial platform. The control unit is provided with means to measure and control the speed of the motorized slidable element and is able to process the values representative of the inclination angle of the cable with respect to the vertical to calculate and to impart control actions in order to dynamically control the speed of the motorized slidable element as a function of a desired inclination angle of the cable with respect to the vertical.
B66C 13/06 - Auxiliary devices for controlling movements of suspended loads, or for preventing cable slack for minimising or preventing longitudinal or transverse swinging of loads
B66C 13/30 - Circuits for braking, traversing, or slewing motors
B66C 17/00 - Overhead travelling cranes comprising one or more substantially-horizontal girders the ends of which are directly supported by wheels or rollers running on tracks carried by spaced supports
10.
A DEVICE AND A PROCESS FOR CONTROLLING A SWINGING OF A LOAD SUSPENDED FROM A LIFTING APPARATUS
An embodiment of the present invention discloses a device for controlling a swinging of a load suspended from a motorized slidable element which can move along a substantially horizontal axis, the controlling device comprising a control unit and an inertial platform, the inertial platform being able to detect representative values of an inclination angle of a cable that supports the load with respect to the vertical and being provided with means for communicating the values to the control unit, wherein the control unit is provided with means to measure and control the speed of the motorized slidable element and is able to process the values representative of the inclination angle of the cable with respect to the vertical so as to calculate and to impart control actions in order to dynamically the speed of the motorized slidable element as a function of a desired inclination angle of the cable with respect to the vertical.
B66C 13/06 - Auxiliary devices for controlling movements of suspended loads, or for preventing cable slack for minimising or preventing longitudinal or transverse swinging of loads
11.
A DEVICE AND A PROCESS FOR CONTROLLING A SWINGING OF A LOAD SUSPENDED FROM A LIFTING APPARATUS
An embodiment of the present invention discloses a device for controlling a swinging of a load suspended from a motorized slidable element which can move along a substantially horizontal axis, the controlling device comprising a control unit and an inertial platform, the inertial platform being able to detect representative values of an inclination angle of a cable that supports the load with respect to the vertical and being provided with means for communicating the values to the control unit, wherein the control unit is provided with means to measure and control the speed of the motorized slidable element and is able to process the values representative of the inclination angle of the cable with respect to the vertical so as to calculate and to impart control actions in order to dynamically the speed of the motorized slidable element as a function of a desired inclination angle of the cable with respect to the vertical.
B66C 13/06 - Auxiliary devices for controlling movements of suspended loads, or for preventing cable slack for minimising or preventing longitudinal or transverse swinging of loads
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