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59results about How to "Simple theory" patented technology

Method for improving optical element additional surface shape caused by force of gravity, and clamping system thereof

The invention relates to a method for improving an optical element additional surface shape caused by force of gravity, and a clamping system thereof. The method utilizes the lever principle, and aims at a heavy-calibre ultrathin transmission-type optical element under the condition of effective clear aperture. Through the clamping system provided by the invention, finite-element analysis software is adopted to carry out modeling simulation and determine lengths, widths and positions of a support strip and a pressure strip as well as force applied onto the pressure strip in the clamping system when the optical element is placed to be balanced at different work gestures and has the minimum additional surface shape change. Through changing the force applied onto the pressure strip, the optical element in the clamping system can have the balanced state at different work gestures, so as to achieve the purpose of improving the optical element additional surface shape caused by force of gravity. The clamping system for realizing the method includes a base, the support strip, a baffle plate, the pressure strip, the optical element, as well as an external wrench and a heavy-calibre interferometer. The method and the clamping system provided by the invention can improve the additional surface shape of the heavy-calibre ultrathin transmission-type optical element caused by force of gravity.
Owner:LASER FUSION RES CENT CHINA ACAD OF ENG PHYSICS +1

Method of designing dam-reservoir water coupled dynamic model test on vibration table

ActiveCN104977151ASolve the leakSolve the problem of water wave rebound effectHydrodynamic testingDynamic modelsEngineering
The invention relates to a method of designing a dam-reservoir water coupled dynamic model test on a vibration table, which belongs to the field of hydraulic structure engineering and model test study. A geometrical size of each part of a two-dimensional model dam section and a layout scheme for each related monitoring device are firstly designed; main physical and mechanical parameters of the model material are determined; the dam model is cast, and each test instrument is buried in advance according to the well-designed layout scheme; a water tank which simulates the reservoir is lifted to the upstream side of the model dam; a reservoir tail energy dissipation device is placed at one end, far away from the model dam, inside the water tank; and after the model dam and the water tank which simulates the reservoir are assembled and the test instruments are assembled and connected, a model dam seismic dynamic simulation test is begun. According to the method of the invention, the theory is simple and easy to understand, the construction process is simple, and hydrodynamic pressure borne by the upstream dam and influences on a dam dynamic response by the upstream reservoir water in the case of an earthquake can be accurately measured in a lab.
Owner:KUNMING UNIV OF SCI & TECH

Multi-stage visual precise landing method and device for unmanned aerial vehicle

ActiveCN114415736APrecision landingRealize identification and positioning without blind spotsPosition/course control in three dimensionsBlind zoneUncrewed vehicle
The invention discloses a multi-stage visual precise landing method for an unmanned aerial vehicle, which comprises the following steps of: S1, acquiring internal parameters of an airborne overlook camera and actual landing height requirements of the unmanned aerial vehicle, and constructing a ground visual landing mark of a multi-scale multi-cooperation label; s2, carrying out detection calculation, landing target identification and angular point detection on the ground visual landing mark; s3, calculating a three-dimensional relative position of a landing target position in an airborne overlook camera coordinate system by using a camera attitude estimation algorithm; and S4, according to the three-dimensional relative position and the real-time three-dimensional position information of the unmanned aerial vehicle, the position of a landing target under a vehicle body coordinate system is solved, and landing is completed by adopting a mode of reducing the landing speed stage by stage. According to the method, the unmanned aerial vehicle can be identified and positioned without blind areas in the whole process at different landing heights by detecting different multi-scale multi-cooperation labels on the ground, so that safe, accurate and smooth landing is completed.
Owner:ZHEJIANG LAB

Fast and high-precision conversion method for Earth fixed connection system-inertial system based on relative rotation

The invention relates to a fast and high-precision conversion method for an Earth fixed connection system-an inertial system based on relative rotation. The method comprises steps of 1, preparation; 2, initial parameter calculation; 3, outputting an ephemeris interpolation table; 4, reading the ephemeris interpolation table; 5, initializing a correlation matrix at the time t; and 6, solving a coordinate transformation matrix corresponding to the time t. A fast coordinate transformation calculation method for a fixed connection system-an inertial system based on relative rotation is brought forward through the steps above, and the method is used for calling relevant subroutines of SOFA only when the ephemeris interpolation table is generated in advance; after the ephemeris interpolation table is generated, only looking up the interval containing the corresponding to-be-solved time in the table, reading relevant parameters, performing linear interpolation and finally substituting valuesinto a corresponding matrix and completing three multiplication operations are required. The method consumes only a small amount of calculation, does not require too much astronomical theoretical background, is inexpensive and easy to implement, has important significance in guidance and navigation of aerospace, and can be used to quickly transform coordinates of the fixed connection system into coordinates of the inertial system. Compared with a traditional SOFA-based program method, the method greatly reduces complexity and can achieve the same function at small computational cost while guaranteeing certain precision.
Owner:孙秀聪 +1

Shallow sea wind electricity facility force absorption pile

The invention provides a shallow sea wind electricity facility force absorption pile, and belongs to the field of ocean equipment. The pipe comprises an outer cylinder, grouting pipes, an inner cylinder, a vacuum pump, a one-way valve, an upper arc-shaped body, a lower arc-shaped body and plugs. The grouting pipes are installed between the outer cylinder and the inner cylinder. The outer cylinder, the inner cylinder and the grouting pipes are fixed to be a whole through linear laser welding, and stress on welding portions is eliminated through Hawking. The upper arc-shaped body and the lower arc-shaped body are welded in the inner cylinder, wherein the upper arc-shaped body is provided with the vacuum pump, the lower arc-shaped body is provided with the one-way valve, and the lower ends of the grouting pipes are provided with the plugs. The eight grouting pipes are uniformly distributed between the outer cylinder and the inner cylinder. The plugs are cone-shaped and are made of magnetic steel. Welding line stress elimination can be achieved on the upper arc-shaped body and the lower arc-shaped body which are welded in the inner cylinder through Hawking. The outer cylinder and the inner cylinder are both big-end-up and are cones with force absorption characteristics. The pile is simple in structure, convenient to insert, large in bearing capacity and little in pile pulling resistance, construction difficulty is the same as that of a cylindrical leg pile, all principles and theories which are used are simple and mature, and reliability of the device is high.
Owner:ZHOUSHAN JUYANG TECH DEV

Reservoir area anti-seepage geomembrane seepage overhauling device and overhauling method thereof

The invention discloses a reservoir area anti-seepage geomembrane seepage overhauling device and an overhauling method thereof, and belongs to the field of hydraulic structure engineering applicationstudy. According to the reservoir area anti-seepage geomembrane seepage overhauling device and the overhauling method thereof, concrete anti-seepage walls are adopted to divide the bottom (the lower portion of an anti-seepage geomembrane) of the whole reservoir area into a plurality of small-area independent areas, a drainage blind ditch is arranged below the anti-seepage geomembrane of each areaand connected with a drainage pipe, and the drainage pipes are connected to flow monitoring equipment arranged outside the reservoir area; and after water storage of a reservoir, the water flow changes of the drainage pipes corresponding to the different independent areas in the reservoir can be observed to accurately judge the area where the anti-seepage geomembrane seeps, and accordingly the accurate geomembrane positioning and overhauling function can be achieved. By means of the reservoir area anti-seepage geomembrane seepage overhauling device and the overhauling method thereof, the waterseepage area after water accumulation can be accurately found, water is drained to the water seepage elevation position for repairing, accordingly, the anti-seepage geomembrane can be repaired, wastecaused by excessive water drainage can be avoided, the water seepage position can be accurately found without mistakes, and the water resource, capital and manpower are saved.
Owner:红河哈尼族彝族自治州水利水电工程地质勘察咨询规划研究院

Ball-end mill cutter five-axis machining instantaneous cutting thickness solution method

The invention discloses a ball-end mill cutter five-axis machining instantaneous cutting thickness solution method. The method comprises the following steps: (1) a three-dimensional ball-end mill cutter model is established according to ball-end mill cutter parameters, and a three-dimensional workpiece model is established according to workpiece parameters; the mill parameters are set with the ball-end mill cutter model acting as the tool body and the workpiece model acting as the object, and the real three-dimensional machined surface model is obtained by Boolean subtraction; (2) the auxiliary entity is established based on the instantaneous cutting thickness theory; (3) the instantaneous cutting thickness entity after Boolean intersection operation of the auxiliary entity and the machined surface model under the same mill parameters is solved; (4) and the instantaneous cutting thickness of the ball-end mill cutter is calculated by using datum plane discretization according to the cutting thickness entity model. The intersection entity three-dimensional model of the auxiliary entity and the machined surface is established through the Boolean operation method and the instantaneouscutting thickness is obtained so that the theory is simple, the solution efficiency is high and the engineering application value is high.
Owner:KUNSHAN SOKAY AUTOMATION TECH CO LTD

A UAV multi-stage visual precision landing method and device

ActiveCN114415736BPrecision landingRealize identification and positioning without blind spotsPosition/course control in three dimensionsView cameraBlind zone
The invention discloses a multi-stage visual precision landing method for an unmanned aerial vehicle, comprising the following steps: Step S1: Obtaining the internal parameters of the airborne bird's-eye view camera and the actual landing height requirement of the unmanned aerial vehicle, and constructing a ground visual landing of multi-scale and multi-cooperative tags Step S2: Perform detection and calculation on the ground visual landing mark, landing target recognition and corner detection; Step S3: Use the camera attitude estimation algorithm to calculate the three-dimensional relative position of the landing target position in the airborne overhead camera coordinate system; Step S4: According to the three-dimensional relative position combined with the real-time three-dimensional position information of the UAV, the landing target position in the body coordinate system is calculated, and the landing is completed by reducing the landing speed step by step. The invention enables the UAV to detect different multi-scale and multi-cooperative labels on the ground at different landing heights, so as to realize the identification and positioning without blind spots in the whole process, so as to complete a safe, accurate and smooth landing.
Owner:ZHEJIANG LAB

Constant-volume combustion technology adopting rotating valve to control opening and closing of combustion chamber and power system applying constant-volume combustion technology

The invention relates to the technical field of combustion, in particular to a constant-volume combustion technology adopting a rotating valve to control opening and closing of a combustion chamber and a power system applying the constant-volume combustion technology. A device used for the constant-volume combustion technology comprises a base, a rotating shaft and the combustion chamber; a stepped through hole is formed in the base and matched with the rotating shaft in mounting; a gas inlet and a gas outlet are axially formed in the middle section of the top of the base and matched with a gas inlet and a gas outlet of the combustion chamber in mounting in a penetrated manner; a gas inlet passage and a gas outlet passage are axially formed in the rotating shaft; a gas inlet passage outlet groove is formed in the front section of the rotating shaft and communicated with the gas outlet passage and cooperates with the gas outlet in the top of the base to control opening and closing of the combustion chamber; a flow rectifying blade is arranged inside the combustion chamber. The constant-volume combustion technology has the advantages that the device can cooperate with the fixed base and the combustion chamber through the rotatable rotating shaft to control opening and closing of the combustion chamber so as to achieve constant-volume combustion, and the device is simple in structure and reliable in working.
Owner:北京首赫防务科技有限公司

Kernel-function-based dimension reduction method of audio feature signal

The invention, which belongs to the technical field of audio signal processing, relates to a kernel-function-based dimension reduction method of an audio feature signal. Dimension reduction processingis carried out on a feature parameter of an audio signal; the required dimension reduction effect is realized while the audio feature information amount is not abandoned; and then last dimension reduction data are displayed visually and comparative analysis is carried out on the last dimension reduction data and results obtained by other audio feature parameter dimension reduction methods. According to the invention, for dimension reduction of the audio feature parameter, dimension reduction processing is mainly carried out on a linear prediction coefficient, a linear prediction cepstral coefficient and a Mel frequency cepstral coefficient in an audio coefficient domain and the data results after dimension reduction are displayed visually. The audio feature dimension reduction processingcan be applied to broadcast signal monitoring and quick identification processing of audio signals. The algorithm is simple and the nonlinear kernel function is used for expressing a mapping relationship between Gaussian observation space and hidden space, thereby overcoming defects of usage range limitation and poor dimension reduction effect of the linear mapping method.
Owner:KUNMING UNIV OF SCI & TECH

EMD-based transient state and steady state response calculation method under action of non-steady signal

The invention provides an EMD-based transient state and steady state response calculation method under the action of a non-steady signal. The method includes the steps that 1, the non-steady signal is decomposed into multiple IMF components with the EMD; 2, fitting simple harmonic processing is carried out on all semiwaves in each IMF component, wherein firstly, linear interpolation is carried out on the current IMF component, all the semiwaves in the current IMF component obtained after interpolation are fitted into simple harmonic waves in sequence, and every time each semiwave is fitted, the semiwave acts in the system and then the transient state response and steady state response of the semiwave are calculated; secondly, the obtained transient state responses and steady state responses of all the semiwaves in the current IMF component are stored in an array; thirdly, the next IMF component is processed, and the first step is executed again till the transient state responses and steady state responses of the semiwaves in all the IMF components are calculated and stored in arrays in sequence; 3, the arrays corresponding to the IMF components are superposed. According to the method, the calculation time is short, and the result is reliable.
Owner:FUJIAN UNIV OF TECH
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