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935results about "Mechanical oscillations control" patented technology

Unbalance identification and vibration suppression control system for magnetic suspension rotating machinery

An unbalance identification and vibration suppression control system for a magnetic suspension rotating machinery comprises an unbalance identification module, an unbalanced force compensation module, a magnetic bearing power amplifier, an electromagnet rotor and a displacement sensor. Based on stable control of a magnetic suspension rotor, the unbalance of a magnetic bearing is identified in an online manner by a novel wave trap based on coordinate transformation, on one hand, the identification amount is used for compensating common-frequency current stiffness force, on the other hand, proper common-frequency current stiffness force is generated according to the identification amount to compensate common-frequency displacement stiffness force, and the influence of the low-pass characteristic of the power amplifier on compensation precision of the common-frequency displacement stiffness force is eliminated by leading a simplified inverse model of the magnetic bearing power amplifier into a feed-forward channel. When the magnetic suspension rotor rotates at a high speed, common-frequency bearing force is greatly reduced, and unbalanced vibration of the magnetic suspension rotor is remarkably suppressed. The unbalance identification and vibration suppression control system is simple, convenient, easy and particularly suitable for an actual high-speed magnetic suspension rotor system.
Owner:BEIHANG UNIV

Helicopter multi-frequency vibration active control method

InactiveCN105843270AReduce order requirementsAvoiding Frequency Modulation ProblemsMechanical oscillations controlEngineeringActuator
The invention discloses a method for actively controlling multi-frequency vibration of a helicopter, including system identification, collecting the control voltage of the actuator and the acceleration response at the controlled point, using the recursive least squares algorithm for system identification, and finally obtaining the discrete state space of the secondary channel Equation; feedback controller design, using the secondary channel discrete state space equation obtained in step 1 to carry out discrete predictive sliding mode feedback controller design; reference signal and error signal acquisition, according to the helicopter rotor characteristics and speed characteristics, extract the rotor excitation frequency, synthesize reference signal, and collect the vibration response error signal at the controlled point; the feedforward-feedback hybrid control algorithm iterates, and uses the reference signal and error signal obtained in step 3 to iterate the feedforward controller and the feedback controller to obtain the feedforward-feedback Feedback the mixed control voltage signal; output the control quantity; use the mixed control voltage obtained in step 4 as the input signal at the next moment, drive the actuator to produce the required response, and return to step 3.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Flexible contilever plate vibration control set and control method based on acceleration sensor

The invention discloses a flexible cantilever plate vibration control device on the basis of accelerometers and a control method. The device is symmetrically affixed with a plurality of piezoelectric ceramic sheets on the front and back surfaces of a fixed end of the flexible plate, the polarities of the two surfaces of a plurality of piezoelectric ceramic sheets are reverse, then a plurality of piezoelectric ceramic sheets are connected in parallel to compose a bending mode piezoelectric driver; the two surfaces of the longitudinal middle part of a free end of the flexible plate are anti-symmetrically affixed with a plurality of piezoelectric ceramic sheets, the polarities of the two surfaces of the piezoelectric ceramic sheets are same, then the piezoelectric ceramic sheets are connected in parallel to compose a torsional mode driver, an accelerometer A and an accelerometer B are respectively arranged at the two side angle positions of the free end of the flexible plate; the device has small weight and less wiring, which only needs the two accelerometers to be used as the sensors of the flexible cantilever plate. The method utilizes the optimized configuration of the two accelerometers and the piezoelectric driver to realize the decoupling on the detection and the driving control of the bending mode and the torsional mode of the flexible cantilever plate, thus realizing the purpose of active inhibition of multi-bending and multi-torsinal mode vibration of the flexible plate.
Owner:SOUTH CHINA UNIV OF TECH
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