F16F15/00

BIOMIMETIC SELF-ADAPTABLE SYSTEMS
20230407556 · 2023-12-21 ·

Self-adaptive systems, uses of the systems, and methods for adapting one or more properties of a material are disclosed.

Method for stabilizing transversal oscillations of a rotor

A method for stabilizing transversal oscillations of a rotor including the steps of acquiring a first signal representing a value of transversal oscillations of a rotor; estimating a value of a thermal gradient from the first signal; computing a value of an actuation parameter from the value of thermal gradient; emitting an actuation signal representing the value of the actuation parameter.

METHOD FOR OPERATING A DRIVETRAIN OF A MOTOR VEHICLE AND DRIVETRAIN FOR A MOTOR VEHICLE
20210062889 · 2021-03-04 · ·

A method for operating a drivetrain of a motor vehicle having at least one centrifugal pendulum, in which the centrifugal pendulum comprises at least one primary part rotatable about an axis of rotation, at least one secondary part movable relative to the primary part, and at least one damping medium by which relative movements are hydraulically dampened between the primary part and the secondary part, wherein at least one temperature of the damping medium is calculated by an electronic calculating device of the drivetrain with the aid of a mathematical model.

ACTIVE VIBRATION CONTROL OF FLOOR AND SEAT FRAME VIBRATION
20210047043 · 2021-02-18 ·

An active vibration control system (AVCS) and method for reducing motion and/or vibration of a seat frame within an aircraft includes vibration sensors, a controller, and force generators. In some embodiments, the vibration sensors and/or the force generators are attached to the seat frames. In other embodiments, the vibration sensors and/or the force generators are attached to aircraft structures, proximate to the seat frame. By monitoring the motion and/or vibration of the seat frame, the controller calculates a cancelling force to be generated by the force generators to reduce the vibration experienced by the seat frame and its occupant. Such seat frame vibration control can be implemented as a separate AVCS in an aircraft, or can be integrated in an existing AVCS that is also configured to provide vibration control in other parts thereof.

Device for compensating free inertia forces of a reciprocating piston internal combustion engine

Systems and methods for reducing inertial forces of a reciprocating piston internal combustion engine are described. The systems and methods may provide for counterweights in a form of pistons in cylinders that are moved via electromagnets. The counterweights may be moved at a frequency that corresponds to engine speed via an alternating current.

System for controlling the vibration of a platform
10951088 · 2021-03-16 · ·

A control system (1) controls the vibration of a platform (2), the platform is formed by a fixed lower support (2a), an upper support (2b) and a plurality of intermediate bodies (2c). The control system (1) includes at least one vibration generator (3) inside the platform (2) between intermediate bodies (2c) and comprising a stator body (4) and at least one vibrating body (5), made of material that is magnetic and concentric with respect to the stator body (4) and in a position that is radially external around the stator body (4), configured to vibrate the upper support (2b) with respect to the lower support (2a). The control system (1) also includes an electric circuit comprising a coil wound around the stator body (4) and designed to receive an audio and/or video signal to generate a magnetic field by the coil and designed to vibrate the at least one vibrating body (5) of the at least one vibration generator (3) as a function of the audio and/or video signal.

METHOD FOR SUPPRESSING VIBRATION OF GIMBAL, AND GIMBAL
20210041772 · 2021-02-11 ·

A method for suppressing a vibration of a gimbal includes obtaining state information of the gimbal, determining a vibration frequency of the gimbal according to the state information, and performing an operation of suppressing the vibration of the gimbal according to the vibration frequency of the gimbal.

Piezoelectric Self-Powered Combination Beam Vibration Damper And Control Method Thereof

The present disclosure discloses a piezoelectric self-powered combination beam vibration damper and a control method thereof. An upper guiding component is installed inside an upper rigid frame, a lower guiding component is installed inside a lower rigid component, a guide rod is nested inside the upper guiding component and the lower guiding component, an upper elastic component is sleeved outside the upper idler wheel mechanism, a lower elastic component is sleeved outside the lower idler wheel mechanism, one end of each piezoelectric cantilever beam is fixed between the upper rigid frame and the lower rigid frame, the other end of each piezoelectric cantilever beam is arranged between the upper idler wheel mechanism and the lower idler wheel mechanism, at least one piezoelectric cantilever beam is connected with the input end of a circuit system, and other piezoelectric cantilever beams are connected with the output end of the circuit system.

Electromagnetic-Piezoelectric Composite Vibration Control Device Based on Synchronized Switch Damping Technology

The present invention discloses an electromagnetic-piezoelectric composite vibration control device based on a synchronized switch damping technology, and relates to the technical field of vibration abatement. An upper rigid frame is arranged at the upper part of a lower rigid frame, an upper guiding component is installed inside the upper rigid frame, a lower guiding component is installed inside a lower rigid component, a guide rod is nested inside the upper guiding component and the lower guiding component, a load platform is fixed to the upper end of the guide rod, an upper idler wheel mechanism and a lower idler wheel mechanism are fixedly sleeved on the guide rod and are positioned between the upper guiding component and the lower guiding component respectively, an electromagnetic mechanism is fixedly sleeved outside the guide rod, an elastic component is sleeved outside the lower idler wheel mechanism, one end of each piezoelectric cantilever beam is fixed between the upper rigid frame and the lower rigid frame, the other end of each piezoelectric cantilever beam is arranged between the upper idler wheel mechanism and the lower idler wheel mechanism, and the piezoelectric cantilever beams and the electromagnetic mechanism are connected with a circuit system respectively. The device is simple in structure and reliable in performance, a voltage source does not need to be provided externally, and the device is of an adaptive characteristic.

SELF-POWERED VIBRATION DAMPER BASED ON PIEZOELECTRICITY AND CONTROL METHOD THEREOF

Disclosed is a self-powered vibration damper based on piezoelectricity and a control method. The damper comprises a loading platform, an energy collecting mechanism, a curved leaf spring, a vibration control mechanism and a substrate all connected in sequence, the circuit system comprises a rectifier circuit, a DC-DC voltage conversion circuit, an energy storage circuit, a control circuit and a charging battery, a first piezoelectric stack is connected with the input end of the rectifier circuit, the output end of the rectifier circuit is connected with the input end of the DC-DC voltage conversion circuit, the output end of the DC-DC voltage conversion circuit is connected with the input ends of the energy storage circuit and the charging battery, the output end of the energy storage circuit is connected with the input end of the control circuit, the output end of the control circuit is connected with the second piezoelectric stack.