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493 results about "Pulse circuits" patented technology

Neck protecting instrument

The invention belongs to the technical field of massaging equipment, and particularly relates to a neck protecting instrument. The neck protecting instrument comprises an elastic housing, electrode piece massaging heads and handles, wherein the elastic housing comprises an elastic surface shell, a silica gel bottom shell and a microprocessor circuit; the silica gel bottom shell is clamped to the back surface of the elastic surface shell; the microprocessor circuit is located between the elastic surface shell and the silica gel bottom shell; the microprocessor circuit comprises a master controlchip and a pulse circuit; the master control chip is connected with the pulse circuit; mounting protrusion platforms are arranged at the back surface of the silica gel bottom shell; each electrode piece massaging head comprises a fixed block, a bracket and an electrode piece; each fixed block is located on one side of the front surface of the corresponding mounting protrusion platform; one end ofeach bracket penetrates through the corresponding mounting protrusion platform to be connected with the corresponding fixed block; the other end of each bracket is connected with the corresponding electrode piece; the electrode pieces are connected with the pulse circuit; the elastic housing is connected with the handles through connecting pieces; and the electrode piece massaging heads are integrally connected with the silica gel bottom shell through the mounting protrusion platforms, so that the electrode piece massaging heads can adjust position, the electrode pieces are attached to a neck, and the massaging comfort degree is improved.
Owner:东莞市固豪塑胶五金制品有限公司

Digital signal processor (DSP) embedded controller for electric dust-removing three-phase high-voltage direct-current power supply

The invention relates to a digital signal processor (DSP) embedded controller for an electric dust-removing three-phase high-voltage direct-current power supply, comprising a hardware system and a software system. The DSP embedded controller is characterized in that the hardware system comprises a control core unit of a DSP, a synchronizing signal circuit, a trigger pulse circuit, a digital quantity output circuit, a digital quantity input circuit, an analog quantity collecting circuit, a communication connector, a man-machine display, an operative keyboard, a power supply module and an photoelectric isolator; and the software system is started to normally run by electric resetting or keyboard resetting on the system, and then a software interrupting module, a hardware interrupting moduleand a task module in the control software are managed and controlled by a DSP/basic input/output system (BIOS) operating system after the software system is initialized. The invention solves the problems existing in the three-phase thyristor voltage-regulating high-voltage direct-current power supply for electric dust removal and increases the reliability of the system, and can improve the effectof electric dust removal after integrally optimizing an electric dust removing system, thereby achieving the requirement of environmental protection.
Owner:ZHEJIANG DOWAY ADVANCED TECH CO LTD

On-orbit service relative navigation experiment platform and work method

The invention discloses an on-orbit service relative navigation experiment platform and a work method. The on-orbit service relative navigation experiment platform comprises a three-axis electric turntable, a three-dimensional electric transversely-moving platform, a simulation control computer, a fault spacecraft equivalent device, a binocular stereo vision system and a navigation computer system. In the process of an experiment, the simulation control computer is utilized to generate an experiment scene, the three-axis electric turntable is controlled to simulate relative posture motion, and the three-dimensional electric transversely-moving platform is controlled to stimulate relative position motion; a pulse circuit triggers the binocular stereo vision system to collect images of the fault spacecraft equivalent device in a cycled mode, and a navigation computer processes the binocular images, conducts navigation and target parameter identification calculation through a relative navigation algorithm module to be verified, uploads the navigation and parameter identification result to the simulation control computer and conducts comparison and evaluation with the truth value set in the stimulation scene. The experiment platform is low in cost, high in simulation fidelity and capable of meeting the requirement of a relative navigation algorithm in quick validation of spacecraft on-orbit service.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Protection device of power supply line disconnection fault

The invention provides a protection device of a power supply line disconnection fault, comprising a voltage-stabilizing circuit, a three-phase voltage sampling circuit, a three-phase voltage comparison circuit, a signal superimposed circuit and a split-phase pulse output circuit, wherein the output end of the three-phase voltage sampling circuit is connected with the three-phase voltage comparisoncircuit; and the output end of the three-phase voltage comparison circuit is connected with the split-phase pulse output circuit through the signal superimposed circuit. The protection device of thepower supply line disconnection fault is characterized in that a three-phase voltage-stabilizing circuit is used as the voltage-stabilizing circuit and is additionally provided with a grounding current control circuit, a blanking pulse circuit and a protection circuit, wherein the input end of the grounding current control circuit is connected with the split-phase pulse output circuit, and the output end of the same sequentially generates three-phase grounding current on the ground; and the blanking pulse circuit and the protection circuit are both connected with the grounding current controlcircuit. The invention utilizes the residual current of the front end of the grounding current control circuit to detect the tripping operation protection of the protection device after the power supply line disconnection fault is detected, and enables a system to have very simple structure and reliable property and provide protection for faults, i.e. zero line disconnection, phase line disconnection, extra-high voltage, extra-low voltage, and the like.
Owner:山东中瑞电气有限公司

Method for calibrating satellite system clock based on bus mode

ActiveCN102096372ASolve the problem that a large number of hardware resources are required to configure multiple hardware pulse circuit interfacesSolve the problem of configuring multiple hardware pulse circuit interfacesSetting time indicationRadio-controlled time-piecesReal-time clockTime difference
The invention discloses a method for calibrating a satellite system clock based on a bus mode. In the method,, a low-accuracy clock user is mutually connected with a high-accuracy clock source through a serial data bus, and the clock is calibrated by the following steps of: 1) generating a local system clock parameter TL and transmitting the parameter to the high-accuracy clock source by the low-accuracy clock user; 2) receiving the clock parameter TL and simultaneously generating a real-time clock parameter TH of the clock source by the high-accuracy clock source, subtracting the two parameters to acquire time difference data Delta Tlast, and correcting fixed time delay to acquire time difference data Delta Tlast; 3) acquiring the time difference data Delta Tlast and adding the time difference data Delta Tlast to a system clock of the low-accuracy clock user by the low-accuracy clock user; and 4) repeating the steps 1), 2) and 3) according to certain period intervals. The method has the advantages of reducing a hardware pulse circuit and simplifying an interface between single satellites.
Owner:SHANGHAI SATELLITE ENG INST
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