13967 results about "Servo" patented technology

The invention discloses a three-degree-of-freedom flexible manipulator control device and method. The device comprises flexible manipulator body parts, a servo motor driving part and a control part. The three-degree-of-freedom distribution is characterized in that two rotating flexible manipulators connected in series are respectively driven by a connected motor and speed reducer and are connected on a moving sliding block driven by a screw; a screw substrate and a fixed base are connected; three alternating servo motors are all provided with photoelectric encoders for detecting a rotation angle. A plurality of piezoelectric ceramic sheets are stuck to the part near a fixing end, on each flexible manipulator to respectively serve as a photoelectric sheet sensor and a photoelectric driver; and acceleration sensors are respectively installed at the parts near a free end, on each flexible manipulator. The photoelectric sheet sensor or the acceleration sensor can respectively detect the vibration of flexible beams. The detected signal is fed back, and three motors are respectively controlled by a motion control card to move after a control algorithm is operated. A control part is used for processing the detected flexible beam rotation and a vibration signal and carries out corresponding processing.

An in-situ testing equipment for testing micromechanical properties of a material in a multi-load and multi-physical field coupled condition is disclosed. The equipment comprises a frame supporting module, a tension / compression-low cycle fatigue module, a torsioning module (21), a three-point bending module (6), an impressing module (33), a thermal field and magnetic field application module (34), an in-situ observation module (32) and a clamp body module (22). The frame supporting module provides a structural support for the whole testing equipment, the tension / compression-low cycle fatigue module is arranged at upper and lower ends of the testing equipment, the torsioning module (21) is directly arranged at a front end of the tension / compression-low cycle fatigue module, the three-point bending module (6), the impressing module (33) and the thermal field and magnetic field application module (34) are disposed on a support post at one side of the whole testing equipment through a common replacing component, and the in-situ observation module is disposed on another support post at the other side of the testing equipment. The clamp body module is connected to a front segment of the torsioning module, so as to clamp a test piece. An overall structure of the testing equipment is configured in a vertically symmetrical arrangement achieved by using four support posts. Two identical servo hydraulic cylinders (10) and two torsioning modules (21) are located at the upper and the lower ends of the testing equipment respectively and are used to perform a symmetrical tension / compression test and a symmetrical torsion test on the test piece (23) positioned centrally. The testing equipment is capable of realizing applications of five different types of loads including tension / compression, low cycle fatigue, torsion, bending and impressing, performing an intensive study on micromechanical properties of the material in the multi-load and multi-physical field coupled condition by using built-in electric, thermal and magnetic application modules and the in-situ observation module, and acquiring relations between deformation behavior, mechanism of damage, performance weakening of the material, applied loads and material properties.

A vacuum chamber (22) of a pneumatically operated servo unit (30) of a motor vehicle is subjected to vacuum by an electric suction pump (28). In order to monitor the vacuum chamber (22) and the electric suction pump (28), the invention proposes that a starting pressure in the vacuum chamber (22) be determined. In addition, after a certain time interval, an ending pressure in the vacuum chamber (22) is determined. Furthermore, the difference between the ending pressure and the starting pressure is calculated and compared to a limit value. If this difference falls below the limit value, a signal is generated, in particular a warning and / or alarm signal.

The embodiment of the invention discloses an industrial robot visual servo system and a servo method and device. The industrial robot visual servo system comprises a six-axis robot, a weld joint tacker, a calibration object, a wireless handheld demonstrator, a USB wireless receiver, an infrared laser positioning base station, a robot control cabinet, a welding machine power supply control cabinet,an upper computer control cabinet and an automatic wire feeding system. Rapid demonstration without programming is achieved, non-uniform workpiece incoming is avoided, and real-time tracking of welding thermal deformation is achieved; the working process of a traditional welding automatic system is improved, and an operator does not need to use the demonstrator to carry out complex demonstrationprogramming; as the recognition technology based on deep learning is adopted for weld joint tracking, the universality of welding automation is greatly improved; and in addition, welding path planning, demonstration, system calibration and welding real-time tracking are completely integrated in the same upper computer interface, and therefore the process operation and management can be conveniently carried out by the operator.

The invention discloses a servo motor control system of an all-electric injection molding machine, comprising an injection molding machine computer controller, a servo motor controller and a PLC controller; the computer controller is connected with the servo motor controller through a CAN bus, the servo motor controller is connected with a servo motor, and the computer controller is connected with PLC controller; the servo motor controller can be a mould opening / closing servo motor controller, a plastic injection servo motor controller, a plasticizing pressure holding servo motor controller and an ejection servo motor controller; and the servo motor can be a mould opening / closing servo motor, a plastic injection servo motor, a plasticizing pressure holding servo motor and an ejection servo motor. The invention also discloses a control method for the control system; and technological procedures capable of being performed simultaneously are synchronously controlled through performing mould opening / closing control, plasticizing control, plastic injection control, pressure holding control, ejection control, mobile control of an injection platform and mould adjustment control on the motor of the electric injection molding machine, thereby saving one third of the production time.

The invention discloses a five-axis linkage loading test device for a machine tool. The device consists of a following loading mechanism mechanical part and a measurement and control system. The following loading mechanism mechanical part applies a load to a spindle through an interface of the spindle of the machine tool. The measurement and control system is used for realizing servo motor control, mechanism motion control, load calculation and signal processing functions of the following loading mechanism mechanical part. The five-axis linkage loading test method for the machine tool comprises the five major steps of: 1, measuring load data; 2, establishing a load spectrum; 3, organizing tool path data; 4, performing hardware solidification of the data; and 5, calibrating and correcting a database. The device and the method are universal and widely applicable to various types of tests in the reliability of the machine tool, and have practical significance and reference value for the research and development of high-performance load simulators in China.

An artificial force feel generating device for generation of an artificial feeling of force on an inceptor of a vehicle control system, the inceptor being adapted for controlling a servo-assisted control unit of the vehicle control system via a mechanical linkage, wherein at least one first force generating device and at least one second force generating device are mechanically connected to the inceptor, the first force generating device being provided for generating a nominal force acting in operation on the inceptor and the second force generating device being provided for generating a tactile cue force acting in operation on the inceptor, the first and second force generating devices being arranged in parallel. The invention relates further to an aircraft comprising such an artificial force feel generating device.