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50results about How to "Increased mechanical sensitivity" patented technology

Energy capturing and energy storing integrated micro-nano battery based on multilayer structure

The invention discloses an energy capturing and energy storing integrated micro-nano battery based on a multilayer structure. The battery mainly comprises an upper energy capturing structure and a lower energy storing structure. The energy capturing structure is formed by repeatedly folding two long strip shape electrodes; one long strip shape electrode is a bottom electrode and has a copper / industrialized liquid crystal polymer / copper three layer composite structure; and the other flexible electrode is a counter electrode and has an electret / copper / industrialized liquid crystal polymer / copper / electret five layer composite structure. The work principle is electrostatic induction: charges are implanted into an electret polymer film in advance to generate a bias voltage, when external vibration causes two electrodes to move relative to each other, due to the capacitance change, charges of two electrodes are recombined, the external mechanical energy is converted into electrical energy,and at the same time, through a two dimensional planar energy storing structure formed on a flexible substrate, in-situ energy storage is realized. The battery has the characteristics of good output performance, simple structure, small volume, light weight, durability, and flexibility.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

MEMS gyro automatic modal matching control device and method based on negative stiffness effect

The invention provides an MEMS gyro automatic modal matching control device based on a negative stiffness effect, and adopts external calibrating signal input, so as to obtain a required modal matching control quantity. The external calibration signal is formed by superposition of two groups of sinusoidal signals a and b with different frequencies, the frequency of one group is higher than the center frequency of a driving mode, the frequency of the other group is lower than the center frequency of the driving mode, frequency difference between the frequencies of the two groups and the center frequency of the driving mode is equal, thus automatic modal matching is realized, and no extra reference quantity is needed. The device suppresses signal coupling and interference in a modal matching process. Two paths of calibrating signals having the same frequency difference with a driving signal are used, a reference signal of a PI controller is set to be 0, and open-loop search for a reference point is not needed. In the device, the calibrating signals are loaded on a detection mechanism in the form of force feedback, the detection mechanism is put in a feedback loop, detection of the amplitude-frequency characteristic of a mode is brought into full play, and output amplitude of the calibrating signal passing the detection mechanism is relatively large.
Owner:SOUTHEAST UNIV

Obliquity rod suspension type gravity gradient former

The present invention discloses an obliquity rod suspension type gravity gradient former. The former comprises a probe, an upper quality inspection, an upper obliquity rod, a cross bar, a lower obliquity rod, a reed, a rotary table, a capacitive displacement sensing module, an electrostatic feedback module and an analog-digital conversion circuit. The reed is in rigid connection with the middle portion of the cross bar, one end of the upper obliquity rod is in rigid connection with one end of the cross bar, one end of the lower obliquity rod is in rigid connection with the other end of the cross bar; the other end of the upper obliquity rod, is connected with the upper quality inspection; the other end of the lower obliquity rod, is connected with the upper quality inspection in the probe; and the upper obliquity rod and the lower obliquity rod are arranged in parallel, and the control end of the probe is connected with the output end of the electrostatic feedback module. The obliquity rod suspension type gravity gradient former only needs an apparatus to complete the measurement of the gravity gradient changing, the entirety of obliquity rod is a central symmetry structure and is insensitive for the ground vibration, the two sides, opposite to the polar plate, of the upper obliquity rod, the lower obliquity rod and the upper quality inspection, the two sides corresponding to the upper quality inspection, the left polar plate and the right polar plate are mutually parallel so as to improve the machinery sensitivity; and through changing of the angle of the obliquity rods and the cross bar the obliquity rod suspension type gravity gradient former can measure the diagonal tensor and the full tensor of the gravity gradient.
Owner:HUAZHONG UNIV OF SCI & TECH

Comb tooth capacitive micro-electromechanical accelerometer structure

The invention discloses a comb tooth capacitive micro-electromechanical accelerometer structure. The structure comprises comb tooth groups, a mass block, flexible beams, flexible beam support rods andcomb tooth support rods, wherein the mass block is a frame structure shaped like a Chinese character Ri; the comb tooth groups are variable-gap comb tooth groups; each comb tooth for forming the combtooth groups is a pentagonal comb tooth with a gradually varied comb tooth width at the overlapped area; the comb tooth groups are crossly distributed in the inner and outer sides of the mass block frame to form a differential capacitor; the movable comb teeth of the comb tooth groups are connected with the mass block and are suspended at two ends of the flexible beam support rods on the two outermost sides of the structure through four flexible beams at four corners of the mass block frame; and the fixed comb teeth of the comb tooth groups are connected with the comb tooth support rods. Thepentagonal comb teeth is capable of increasing the tooth pair number while keeping the tooth clearance ratio, so that benefit is brought to improve the sensitivity of the accelerometer. The crossly distributed comb tooth groups are capable of making up the capacitive differences caused by nonuniform etching process so as to improve the capacitive symmetry, and is also capable of compensating the influences, on the differential capacitor, caused by environment temperature change so as to improve the stability of a calibration factor of the accelerometer.
Owner:XIAN FLIGHT SELF CONTROL INST OF AVIC

Silicon micromachined resonant accelerometer

The invention provides a silicon micromachined resonant accelerometer. One end of each force arm of a micro-mechanical lever mechanism, which is far away from a corresponding anchoring body, is fixedon a mass block; the moving components of resonators are connected with the force arms and are driven to move by the force arms; the resonators are symmetrically arranged with respect to the middle line of the mass block; the displacement directions of the moving components of the two resonators which are symmetrical to each other after the moving components bear forces are opposite to each other;the resonators are symmetrically arranged with respect to the center line of the mass block, so that the resonant frequencies of the operating modes of the two resonators are equal; the two resonators are distributed at two ends of the mass block, so that the mutual interference of resonant structures can be greatly reduced, and the noise level of the accelerometer can be decreased; since the resonators are located at the two ends of the mass block, the asymmetric vibration of the resonant structures which is caused by the asymmetry of the machining of the mass block can be greatly reduced; and therefore, drift caused by process error, temperature change and environmental vibration can be greatly reduced, and the interference of environmental factors can be effectively suppressed from thestructure of the accelerometer, and the sensitivity of the accelerometer can be effectively improved.
Owner:JIAXING NAJIE MICROELECTRONICS TECH

f-p pressure sensor with composite dielectric film

A F-P pressure sensor with a composite dielectric film disclosed by the present invention comprises an upper ferrule with a F-P resonant cavity, a lower ferrule which is axially fixedly connected with the upper ferrule and inserted into the lower ferrule. A ferrule for the fiber, and a pressure diaphragm covering the port of the F‑P resonator. At least one layer of composite dielectric film is grown on the back side of the pressure diaphragm and the silicon wafer at the bottom of the groove of the F-P resonator, and the composite dielectric film is SiO 2 / Ta 2 o 5 Thin film, Si 3 N 4 / Ta 2 o 5 thin film or SiO 2 / Ta 2 o 5 / Si 3 N 4 A multilayer film in at least one combination form. The invention has the advantages of simple structure, convenient and quick manufacture, low cost and high thermal stability. In the present invention, a composite dielectric film is grown on the back of the pressure diaphragm and the bottom surface of the upper ferrule groove, and the F-P resonant cavity is formed by connecting the pressure diaphragm with the upper ferrule to match the reflectivity of the system. This combined composite dielectric film is not only thermally stable At the same time, it can be combined according to the design requirements to obtain the reflectivity that meets the system requirements.
Owner:CHENGDU KAITIAN ELECTRONICS

MEMS chip and electronic equipment

The invention discloses an MEMS chip and electronic equipment. The MEMS chip comprises a substrate, a vibrating diaphragm and a back polar plate which are sequentially arranged in a stacked mode. The MEMS chip further comprises a first supporting part arranged between the substrate and the vibrating diaphragm and a second supporting part arranged between the vibrating diaphragm and the back pole plate, and the projection of the first supporting part on the vibrating diaphragm and the projection of the second supporting part on the vibrating diaphragm are arranged in a staggered mode. According to the invention, the vibrating diaphragm is supported on the substrate through the first supporting part, so that the periphery of the vibrating diaphragm and the substrate are relatively fixed; and the back pole plate is supported on the vibrating diaphragm through the second supporting part, so that the back pole plate and the vibrating diaphragm are separated to form a vibration gap, thereby facilitating vibration of the vibrating diaphragm. The first supporting part and the second supporting part are arranged at the two opposite ends of the vibrating diaphragm, and the projection of the first supporting part on the vibrating diaphragm and the projection of the second supporting part on the vibrating diaphragm are staggered, so that the stress at the anchor point of the vibrating diaphragm can be reduced, the compliance of the vibrating diaphragm can be improved, and the mechanical sensitivity of the MEMS chip can be improved.
Owner:WEIFANG GOERTEK MICROELECTRONICS CO LTD

An automatic mode matching control device and method for mems gyroscope based on negative stiffness effect

The invention provides an MEMS gyro automatic modal matching control device based on a negative stiffness effect, and adopts external calibrating signal input, so as to obtain a required modal matching control quantity. The external calibration signal is formed by superposition of two groups of sinusoidal signals a and b with different frequencies, the frequency of one group is higher than the center frequency of a driving mode, the frequency of the other group is lower than the center frequency of the driving mode, frequency difference between the frequencies of the two groups and the center frequency of the driving mode is equal, thus automatic modal matching is realized, and no extra reference quantity is needed. The device suppresses signal coupling and interference in a modal matching process. Two paths of calibrating signals having the same frequency difference with a driving signal are used, a reference signal of a PI controller is set to be 0, and open-loop search for a reference point is not needed. In the device, the calibrating signals are loaded on a detection mechanism in the form of force feedback, the detection mechanism is put in a feedback loop, detection of the amplitude-frequency characteristic of a mode is brought into full play, and output amplitude of the calibrating signal passing the detection mechanism is relatively large.
Owner:SOUTHEAST UNIV

Tangentially driven double-differential butterfly-wing silicon micro-gyroscope and its application method

The invention discloses a tangential driving double-difference butterfly-wing silicon microgyroscope and an application method thereof. The silicon microgyroscope is of a silicon-glass double-layer structure which is constituted by a silicon sensitive structure and a glass electrode plate, the silicon sensitive structure comprises an external framework, an internal coupling spring structure and two silicon sensitive subsidiary structures, each silicon sensitive subsidiary structure comprises four inertial mass blocks which are connected to a supporting beam through a cantilever beam, driving comb teeth are arranged on the inertial mass blocks, a driving electrode, a detecting electrode and an electrode welding disc are arranged on the glass electrode plate, and detecting capacitors of thetwo silicon sensitive subsidiary structures constitute a double-difference slab detecting capacitor. The application method comprises the step of additionally applying static electrostatic stiffness to a unilateral silicon sensitive structure to change a modal control method of the system modal frequency. By means of the tangential driving double-difference butterfly-wing silicon microgyroscope and the application method thereof, the limit of normal displacement on driving amplitude and capacitive gaps can be effectively removed, the driving Q value can be effectively increased, the working state of the gyroscope is improved, thus the sensitivity of the gyroscope is improved, the bandwidth of the gyroscope is increased, and the stability of the gyroscope is improved.
Owner:NAT UNIV OF DEFENSE TECH
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