G01M1/30

OPERATING APPARATUS FOR A VEHICLE COMPONENT AND METHOD FOR PRODUCING FEEDBACK

An operating apparatus for a vehicle component comprises an operating panel (12) as well as an electric motor (34) mechanically coupled thereto with an unbalance mass. A detector (20) can capture the contact of the operating panel (12) by a user. A sensor (46) is provided in order to set exactly the number of revolutions of the electric motor in response to the contact of the operating panel by a user. The number of revolutions of the rotor is determined via this sensor.

OPERATING APPARATUS FOR A VEHICLE COMPONENT AND METHOD FOR PRODUCING FEEDBACK

An operating apparatus for a vehicle component comprises an operating panel (12) as well as an electric motor (34) mechanically coupled thereto with an unbalance mass. A detector (20) can capture the contact of the operating panel (12) by a user. A sensor (46) is provided in order to set exactly the number of revolutions of the electric motor in response to the contact of the operating panel by a user. The number of revolutions of the rotor is determined via this sensor.

Method of balancing a gas turbine engine rotor

A gas turbine engine rotor including a disc adapted to be mounted for rotation about an axis, the disc including an annular balancing flange integrally connected thereto, the balancing flange having a first radial dimension around a first arc angle and a second radial dimension greater than the first radial dimension around a second arc angle, the second arc angle corresponding to 360 minus the first arc angle, the second arc angle being less than 180 degrees, the balancing flange around the second arc angle defining a protuberance, the protuberance being defined through machining of the balancing flange, the protuberance compensating for an unbalance of the rotor.

Method of balancing a gas turbine engine rotor

A gas turbine engine rotor including a disc adapted to be mounted for rotation about an axis, the disc including an annular balancing flange integrally connected thereto, the balancing flange having a first radial dimension around a first arc angle and a second radial dimension greater than the first radial dimension around a second arc angle, the second arc angle corresponding to 360 minus the first arc angle, the second arc angle being less than 180 degrees, the balancing flange around the second arc angle defining a protuberance, the protuberance being defined through machining of the balancing flange, the protuberance compensating for an unbalance of the rotor.

LARGE HIGH-SPEED ROTARY DEVICE GAP STACKING ASSEMBLY APPARATUS AND ASSEMBLY METHOD BASED ON DIGITAL TWIN
20240102877 · 2024-03-28 ·

Provided is a large high-speed rotary equipment gap stacking assembly apparatus and assembly method based on digital twin, and relates to the technical field of engine assembly measurement. The disclosure solves the problem of unbalanced rotation of the rotary parts caused by large assembly error during multi-stage rotary parts are stacked in a gap way. The disclosure includes the assembly apparatus entity and the assembly method; the assembly apparatus entity is configured to establish data communication with the upper computer through data acquisition apparatus, and upper computer is configured to establish a virtual assembly model; the virtual assembly model and optimal coaxiality of the multi-stage rotary parts in gap stacking can be obtained according to the assembly method, and the assembly process can be controlled by using the virtual assembly model and the optimal coaxiality. The disclosure is suitable for controlling the assembly process of the rotary parts.

LARGE HIGH-SPEED ROTARY DEVICE GAP STACKING ASSEMBLY APPARATUS AND ASSEMBLY METHOD BASED ON DIGITAL TWIN
20240102877 · 2024-03-28 ·

Provided is a large high-speed rotary equipment gap stacking assembly apparatus and assembly method based on digital twin, and relates to the technical field of engine assembly measurement. The disclosure solves the problem of unbalanced rotation of the rotary parts caused by large assembly error during multi-stage rotary parts are stacked in a gap way. The disclosure includes the assembly apparatus entity and the assembly method; the assembly apparatus entity is configured to establish data communication with the upper computer through data acquisition apparatus, and upper computer is configured to establish a virtual assembly model; the virtual assembly model and optimal coaxiality of the multi-stage rotary parts in gap stacking can be obtained according to the assembly method, and the assembly process can be controlled by using the virtual assembly model and the optimal coaxiality. The disclosure is suitable for controlling the assembly process of the rotary parts.

OBSERVATION DEVICE AND OBSERVATION METHOD
20240060844 · 2024-02-22 ·

An observation device observes a balance state of a main spindle of a machine tool including the main spindle and a moving body to which the main spindle is rotatably fixed and which moves in a direction orthogonal to the axial direction of the main spindle. The observation device includes a first acquisition unit for acquiring rotation angles of the main spindle during rotation; a second acquisition unit for acquiring movement information indicating a movement state of the moving body when the main spindle is rotating; and an output generation unit for displaying, on a display unit, each of the rotation angles of the main spindle and the movement information in association with each other.

Method and system for repairing turbine airfoils

The present disclosure is directed to a method and system for repairing a blade for a turbomachine that has been damaged due to foreign object impact. Machine learning algorithms are used to determine an amount of material to be removed from one or more damage locations and determine an amount of material addition to the damaged portion(s) and/or at other locations on the blade to keep the natural frequencies of the repaired blade within design limits during operation.

Method and system for repairing turbine airfoils

The present disclosure is directed to a method and system for repairing a blade for a turbomachine that has been damaged due to foreign object impact. Machine learning algorithms are used to determine an amount of material to be removed from one or more damage locations and determine an amount of material addition to the damaged portion(s) and/or at other locations on the blade to keep the natural frequencies of the repaired blade within design limits during operation.

Bearing and eccentricity correction method
10443683 · 2019-10-15 · ·

A bearing that rotatably supports a rotating shaft includes an inner wheel that supports the rotating shaft in a manner to be coaxial with the rotating shaft; an outer wheel provided radially outside the inner wheel; and a plurality of rolling bodies that are provided in a ring-shaped gap between the inner wheel and the outer wheel. The inner wheel is provided with a correcting section that corrects eccentric rotation of the rotating shaft.