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150results about How to "Reduce vibration levels" patented technology

Large-torque magnetic suspension flywheel

The invention discloses a large-torque magnetic suspension flywheel, which can be used as an execution mechanism for attitude stabilization and attitude maneuver of spacecrafts such as a satellite, an earth observation platform and the like. The magnetic suspension flywheel mainly consists of a base, a sealing cover, a radial decoupling conical magnetic bearing assembly, a core shaft, a rotor assembly, a Lorentz force magnetic bearing assembly, a motor assembly, a sensor assembly and the like. The core shaft is positioned in the center of the wheel body, a stator assembly is positioned at theradial outer side of the core shaft, the rotor assembly is arranged at the radial outer side of the stator assembly, the rotor assembly consists of a wheel flange and a wheel hub, and the Lorentz force magnetic bearing assembly consists of a magnetic bearing stator part and a magnetic bearing rotor part; an adapter plate is connected with the core shaft, the stator assembly and a motor stator; and the sensor assembly consists of a sensor shell and a sensor. The components of the flywheel are arranged reasonably and compactly, the flywheel can be used for attitude stabilization of the spacecraft, and attitude maneuver of the spacecraft can be realized by using large control torque provided by gyroscopic effect of the magnetic suspension flywheel.
Owner:BEIHANG UNIV

Hard rock road-header damping design method based on multi-tuning mass damper

The invention provides a hard rock road-header damping design method based on a multi-tuning mass damper. The hard rock road-header damping design method comprises the steps of establishing a hard rock road-header whole-machine rigid-flexible coupling multi-body dynamics model; 2, calculating hob dynamic rock breaking force and shield-surrounding rock mutual acting force and simulating hard rock road-header vibration exciting force; 3, analyzing and evaluating hard rock road-header driving performance and the whole-machine vibration level; 4, installing the multi-tuning mass damper on a hard rock road-header gearbox; 5, determining the quantity, distribution mode, mass, rigidity and damping of damper bodies in the multi-tuning mass damper by minimizing a minimal whole-machine vibration level index value or a maximal whole-machine vibration level index value of a minimal driving performance index. By arranging the multi-tuning mass damper on the hard rock driving gearbox and optimizing parameters of the multi-tuning mass damper, on the basis of improving or maintaining the hard rock road-header driving performance, the whole-machine vibration can be effectively lowered, and the damage to key parts caused by strong vibration can be avoided or lowered.
Owner:SHANGHAI JIAO TONG UNIV

Mechanical frequency modulation type dynamic absorber for satellite flywheel

The invention relates to a mechanical frequency modulation type dynamic absorber for a satellite flywheel. A guide rod is vertically fixed to the center of a bottom plate. A shock absorption mass block horizontally moves in the axial direction of the guide rod through a linear bearing. Linear modules are symmetrically arranged on the two sides of the guide rod. The mechanical frequency modulation type dynamic absorber comprises a guide rail, a ball screw, a ball nut sliding block, a leaf spring assembly and a motor connection seat, wherein the guide rail is fixed to the bottom plate, the ball screw is arranged on the guide rail, the ball nut sliding block is arranged on the ball screw, the leaf spring assembly is connected between the shock absorption mass block and the ball nut sliding block. The motor connection seat is fixed to one end of the guide rail. By adoption of the symmetrical structural design, the inherent structure frequency is adjusted according to the mechanical frequency modulation principle and changes of the rotation speed of the flywheel, vibration of the flywheel is controlled and restrained to a low order, stability and reliability of the on-satellite high-accuracy sensitivity load in-orbit operation are ensured, and the mechanical frequency modulation type dynamic absorber has the advantages that the frequency tracing speed is high, the vibration absorption performance is excellent, the structure is simple, reliability is high, assembly is convenient, and the manufacturing cost is low.
Owner:SHANGHAI SATELLITE ENG INST

Centralized mounting bracket for avionics equipment

The invention provides a centralized mounting bracket for avionics equipment. Centralized and fast loading and unloading of multiple avionics equipment can be achieved. The centralized mounting bracket includes a fast loading and unloading mechanism, a damping mechanism, a ventilating and cooling pipeline, and a communication channel for communication between equipment as well as between a systemand an aircraft. The fast loading and unloading mechanism comprises fasteners and spring positioning pins which are arranged on the centralized mounting bracket, and a locking handle on the avionics equipment. The damping system consists of six dampers, the vibration magnitude of the avionics equipment can be effectively decreased, and the reliability of the system is improved. The ventilating andcooling pipeline includes an air inlet pipe, an air cavity, a ventilating pipe and a sealing ring and can provide air cooling conditions for the avionics equipment, the working temperature of internal electronic components can be effectively adjusted, and the working reliability is improved. The communication channel for communication between equipment as well as between the system and the aircraft comprises circular connectors mounted on a back shell and a left shell of the centralized mounting bracket and a rectangular connector mounted on a front cover plate, and communication connection between equipment as well as between the system and the aircraft is achieved.
Owner:LUOYANG INST OF ELECTRO OPTICAL EQUIP OF AVIC

Drive device of magnet exciting coil with online magnetic balancing head

The invention discloses a drive device of a magnet exciting coil with an online magnetic balancing head. The drive device comprises a voltage regulating circuit and a current regulating circuit, wherein the voltage regulating circuit is composed of a comparison circuit, a metal-oxide-semiconductor field effect transistor (MOSFET) drive circuit, an MOSFET and a filter circuit and can convert a voltage signal output by a controller into a power signal with a wave form similar to that of the voltage signal; and the current regulating circuit is composed of an H bridge circuit and two half-bridge drive circuits and can change a current direction of the power signal output by the voltage regulating circuit in a staggered manner by controlling the H bridge circuit to switch on or off a bridge so as to meet a requirement for an operation of a drive coil with a dynamic balancing head. By coordinating the voltage regulating circuit with the current regulating circuit, drive voltages meeting the requirement for a magnet exciting coil with an online active balancing head can be outputted. The drive circuit provided by the invention is adopted, so that the magnet exciting coil with a balancing head can be driven so as to rotate a counterweight plate in relative to a main shaft, thus further correcting imbalance of the high-speed main shaft. Therefore, a vibration level of a machine is reduced, and operation quality, efficiency and service life of the machine are improved.
Owner:XI AN JIAOTONG UNIV

Control system and method for helicopter electrically-driven tail rotor

The invention relates to a control system and method for a helicopter electrically-driven tail rotor. The control system comprises a pedal, an angular displacement sensor, a helicopter controller, a motor controller, a driver for a tail rotor driving motor, a motor driver of a tail rotor variable pitch structure, a detection unit, a gyroscope, a motor-reducer integrated structure capable of driving the tail rotor to rotate, and an electrically-driven variable pitch structure. By use of the control method, according to a pedal angle change and a helicopter tail gesture change of gyroscope detection, the revolving speed of the tail rotor driving motor is automatically controlled, and a variable pitch structure is regulated so as to realize the balance or the diversion of the helicopter. Theinvention provides the control system and method for the helicopter electrically-driven tail rotor, and replaces the internal combustion engine driving and the excessive transmission shaft of a traditional helicopter, so that the quick and stable automatic balance and diversion of the helicopter can be realized, operation difficulty is reduced, and reliability and stability are enhanced so as to be favorable for accelerating the technology of an electric helicopter to be progressed and developed.
Owner:HEFEI UNIV OF TECH
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