Patent classifications
G05D19/00
Method for operating a hydraulic valve of a hydraulic device of a motor vehicle transmission device as well as a motor vehicle transmission device
A method for operating a hydraulic valve of a hydraulic device of a motor vehicle transmission device, wherein an actuating current of the hydraulic valve is superposed with a modulation alternating current in order to adjust a shaking vibration of the hydraulic valve by a control device, wherein a deviation between an actual pressure resulting from the actuating current and a setpoint pressure determined as a function of the actuating current is determined for the hydraulic device by means of an electronic computing device, and an amplitude and/or a frequency of the modulation alternating current is increased as compared to a starting value equalizing a hysteresis of the actual pressure relative to the setpoint pressure, as a function of a tolerance range being exceeded by the determined deviation.
Method for operating a hydraulic valve of a hydraulic device of a motor vehicle transmission device as well as a motor vehicle transmission device
A method for operating a hydraulic valve of a hydraulic device of a motor vehicle transmission device, wherein an actuating current of the hydraulic valve is superposed with a modulation alternating current in order to adjust a shaking vibration of the hydraulic valve by a control device, wherein a deviation between an actual pressure resulting from the actuating current and a setpoint pressure determined as a function of the actuating current is determined for the hydraulic device by means of an electronic computing device, and an amplitude and/or a frequency of the modulation alternating current is increased as compared to a starting value equalizing a hysteresis of the actual pressure relative to the setpoint pressure, as a function of a tolerance range being exceeded by the determined deviation.
Servo controller for measuring lubrication characteristics of a machine by experimental modal analysis
A servo controller includes: a sinusoidal wave disturbance input unit for supplying a sinusoidal wave disturbance to a speed control loop including a speed command generator, a torque command generator and a speed detector; a frequency response calculator for estimating the gain and phase from the output of the speed control loop; a resonance frequency detector for detecting resonance frequencies at which the gain becomes maximum; a resonance mode characteristics analyzer for estimating resonance characteristics from the frequency response; and, a reference modal damping ratio retainer for retaining a reference modal damping ratio as a resonance characteristic corresponding to the reference lubricating condition, and the resonance mode characteristics analyzer calculates lubrication characteristics on the basis of the reference modal damping ratio and the measured modal damping ratio at the resonance frequency corresponding to the reference modal damping ratio.
Frequency response diagnostics for characterizing servo controlled mechanisms
A server includes a processor to supply a torque command to an amplifier that controls a motor that drives a linkage; include, in the torque command, an alternating signal wave that is to test a frequency response of the motor and the linkage; receive, from the amplifier, an instantaneous torque value of the motor and an instantaneous mechanical parameter value of the linkage at each time step according to a sampling rate and over a period of time; store an aggregate of both these values; determine, for a first frequency of the alternating signal wave, a magnitude and phase shift between the aggregate of the instantaneous mechanical parameter values and the aggregate of the instantaneous torque values; and generate, using an aggregate of magnitude and phase shift data for multiple frequencies of the alternating signal wave, a fingerprint to be used in performing diagnostics of motor and linkage.
Frequency response diagnostics for characterizing servo controlled mechanisms
A server includes a processor to supply a torque command to an amplifier that controls a motor that drives a linkage; include, in the torque command, an alternating signal wave that is to test a frequency response of the motor and the linkage; receive, from the amplifier, an instantaneous torque value of the motor and an instantaneous mechanical parameter value of the linkage at each time step according to a sampling rate and over a period of time; store an aggregate of both these values; determine, for a first frequency of the alternating signal wave, a magnitude and phase shift between the aggregate of the instantaneous mechanical parameter values and the aggregate of the instantaneous torque values; and generate, using an aggregate of magnitude and phase shift data for multiple frequencies of the alternating signal wave, a fingerprint to be used in performing diagnostics of motor and linkage.
FREQUENCY RESPONSE DIAGNOSTICS FOR CHARACTERIZING SERVO CONTROLLED MECHANISMS
A server includes a processor to supply a torque command to an amplifier that controls a motor that drives a linkage; include, in the torque command, an alternating signal wave that is to test a frequency response of the motor and the linkage; receive, from the amplifier, an instantaneous torque value of the motor and an instantaneous mechanical parameter value of the linkage at each time step according to a sampling rate and over a period of time; store an aggregate of both these values; determine, for a first frequency of the alternating signal wave, a magnitude and phase shift between the aggregate of the instantaneous mechanical parameter values and the aggregate of the instantaneous torque values; and generate, using an aggregate of magnitude and phase shift data for multiple frequencies of the alternating signal wave, a fingerprint to be used in performing diagnostics of motor and linkage.
Controlling mechanical vibrations
Mechanical vibrations are generated on a frame of an aerial vehicle as a response to operation of the aerial vehicle, such as rotation of motors and/or propellers. Likewise, environmental conditions, such as wind, humidity, etc., may also cause vibrations on the frame of aerial vehicles. These vibrations may be destructive to the aerial vehicle, impact stability of the aerial vehicle, and/or result in audible sounds. Disclosed are systems and methods for measuring and/or predicting the vibrations on the frame of the aerial vehicle, generating anti-vibrations, and outputting those anti-vibrations such that the anti-vibrations modify vibrations on the frame of the aerial vehicle.
Controlling mechanical vibrations
Mechanical vibrations are generated on a frame of an aerial vehicle as a response to operation of the aerial vehicle, such as rotation of motors and/or propellers. Likewise, environmental conditions, such as wind, humidity, etc., may also cause vibrations on the frame of aerial vehicles. These vibrations may be destructive to the aerial vehicle, impact stability of the aerial vehicle, and/or result in audible sounds. Disclosed are systems and methods for measuring and/or predicting the vibrations on the frame of the aerial vehicle, generating anti-vibrations, and outputting those anti-vibrations such that the anti-vibrations modify vibrations on the frame of the aerial vehicle.
Adjusting method and adjusting system for resonance frequency of vibration isolator, vibration isolator, and designing method, designing system, and manufacturing method for vibration isolator
Provided is an adjusting method for a resonance frequency of a vibration isolator, the vibration isolator including first to n-th elastic member groups and/or an n+1-th elastic member group, the first to n-th elastic member groups and/or the n+1-th elastic member group being located on an xy plane of an xyz coordinate system, and an xy coordinate system of the xyz coordinate system being a coordinate system obtained by, when a tensor of inertia I with respect to an XYZ coordinate system having an origin in a center of gravity of a vibration sensing side structure or a vibration source side structure is represented as I, rotating an XY coordinate system by =tan.sup.1(2I.sub.XY/(I.sub.XXI.sub.YY)) around a Z axis, the adjusting method including, when rigidity K.sub.i of the first to n-th elastic member groups is represented as
rigidity K.sub.n+1 of the n+1-th elastic member group is represented as
Method of controlling a gate valve
An object of the invention is to provide a method of controlling a gate valve that operates the gate valve in a short time while suppressing vibration of the valve body. A method of controlling a gate valve provided on an opening of a chamber, wherein the gate valve includes a valve body that opens and closes so as to close the opening of a chamber, a valve seat provided on the edge of the opening to which the valve body is pressed, and a sealing material for sealing between the valve body and the valve seat. The invented method is characterized in that, in moving the valve body to the open position from the closed position where the valve body is pressed against the valve seat with the sealing material compressed, the valve body is made to stop temporarily for a predetermined time at the position immediately before the compressed sealing material is pulled apart or immediately after pulled apart in the opening movement of the valve body.