A balancing device for each rotating piece, the rotating piece defining an axis of rotation, the balancing device including: a fixed portion, a mobile portion defining a central axis. The balancing device constrained to the rotating piece so that the central axis substantially coincides with the rotation axis. The balancing device including at least one eccentric mass, rotatable around the central axis and not balanced with respect to the central axis. The balancing device further including apparatus for movement of the eccentric masses, including a magnetic brake and being able to rotate the eccentric masses, with respect to the rotating piece around the central axis.

Balancing system for a rotating spindle (3) of a machine tool (1); the balancing system has a rotating part comprising a balancing head (7) with at least one balancing mass (8) and at least one electric motor (9) which is adapted to regulate the position of the balancing mass; the rotating part also includes a vibration sensor (10) and a control system (11) with at least one hardware (12) and at least one software (13) executed by the hardware; the balancing system also includes a two-way contactless communication system (14) which establishes communication between the rotating control system and a fixed processing and control electronics (15) connected to a machine tool control unit (20). The software of the control system features: a management application (19) which performs all the management of the balancing head and the vibration sensor during normal operation, and a service application (18) which, when the control system is powered after a suspension of the power supply, automatically starts up and starts the management application or, if a software update is required, overwrites the existing version of the management application with a new version.

Balancing system for a rotating spindle (3) of a machine tool (1); the balancing system has a rotating part comprising a balancing head (7) with at least one balancing mass (8) and at least one electric motor (9) which is adapted to regulate the position of the balancing mass; the rotating part also includes a vibration sensor (10) and a control system (11) with at least one hardware (12) and at least one software (13) executed by the hardware; the balancing system also includes a two-way contactless communication system (14) which establishes communication between the rotating control system and a fixed processing and control electronics (15) connected to a machine tool control unit (20). The software of the control system features: a management application (19) which performs all the management of the balancing head and the vibration sensor during normal operation, and a service application (18) which, when the control system is powered after a suspension of the power supply, automatically starts up and starts the management application or, if a software update is required, overwrites the existing version of the management application with a new version.

There is provided a method and a system for propeller balancing of an aircraft. The method comprises operating a propeller in-flight, receiving propeller vibration data during operation of the propeller in-flight, computing, after at least one flight of the aircraft, an average vibration magnitude and an average vibration phase angle based on the propeller vibration data, determining a propeller balancing solution based on the average vibration magnitude and the average vibration phase angle, and generating a balancing need indication by outputting the propeller balancing solution.

There is provided a method and a system for propeller balancing of an aircraft. The method comprises operating a propeller in-flight, receiving propeller vibration data during operation of the propeller in-flight, computing, after at least one flight of the aircraft, an average vibration magnitude and an average vibration phase angle based on the propeller vibration data, determining a propeller balancing solution based on the average vibration magnitude and the average vibration phase angle, and generating a balancing need indication by outputting the propeller balancing solution.

Examples relate to a method for balancing a mirror unit for a laser deflection device comprising a mirror, a rotor for rotating the mirror around a rotation axis, and a mirror holder holding the mirror to the rotor. The mirror, the rotor, and the mirror holder are balanced using one or more balancing weights to modify a mass distribution of the mirror unit in the mirror plane and/or in a balance plane parallel to the mirror plane and containing the rotation axis. The balancing weights have a centre of mass arranged in the mirror plane and/or in the balance plane and are configured so, when deflecting a laser beam with the mirror on a laser beam position sensor and rotating the mirror unit around the rotation axis, a deviation of a position signal measured by the laser beam position sensor in a direction perpendicular to the mirror plane is reduced.

Examples relate to a method for balancing a mirror unit for a laser deflection device comprising a mirror, a rotor for rotating the mirror around a rotation axis, and a mirror holder holding the mirror to the rotor. The mirror, the rotor, and the mirror holder are balanced using one or more balancing weights to modify a mass distribution of the mirror unit in the mirror plane and/or in a balance plane parallel to the mirror plane and containing the rotation axis. The balancing weights have a centre of mass arranged in the mirror plane and/or in the balance plane and are configured so, when deflecting a laser beam with the mirror on a laser beam position sensor and rotating the mirror unit around the rotation axis, a deviation of a position signal measured by the laser beam position sensor in a direction perpendicular to the mirror plane is reduced.

A method for determining stability of a vehicle having a load suspended from the vehicle is provided. The method can include obtaining measurements from a plurality of sensors positioned on the vehicle, obtaining a measurement from a vehicle accelerometer operative to determine an inclination of the vehicle, determining a position of the load suspended from the vehicle, determining a slung load of the load suspended from the vehicle, using the determined slung load and the determined position of the load suspended from the vehicle, determining tipping moments acting on the vehicle, determining righting moments acting on the vehicle and determining a tipping stability based on the determined tipping moments and determined righting moments.

A method for determining stability of a vehicle having a load suspended from the vehicle is provided. The method can include obtaining measurements from a plurality of sensors positioned on the vehicle, obtaining a measurement from a vehicle accelerometer operative to determine an inclination of the vehicle, determining a position of the load suspended from the vehicle, determining a slung load of the load suspended from the vehicle, using the determined slung load and the determined position of the load suspended from the vehicle, determining tipping moments acting on the vehicle, determining righting moments acting on the vehicle and determining a tipping stability based on the determined tipping moments and determined righting moments.

The present application discloses a method for detecting an abnormity in an optical path or measuring and adjusting of a dynamic balance of a gantry in a CT system, comprising performing, by a gantry controlled by a controller, a test scan along an optical path of the CT system, the optical path being a path along which rays pass from a ray source to a detector. The method further comprises obtaining, by a processor, data relating to the test scan, and based on the data relating to the test scan. The method further comprises determining, by the processor, a status characteristic index of the optical path or an amount of dynamic imbalance of the gantry. The method further comprises analyzing, by the processor, a result of the status characteristic index; determining, by the processor, whether the optical path is abnormal, or determining whether a dynamic balance of the gantry satisfies a requirement based on a result of the analysis of the amount of dynamic imbalance.