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75 results about "Density field" patented technology

Field Density. Field density or density of field is expressed in lines of force per unit area of cross-section perpendicular to the lines of force.

Method for calibrating and measuring supersonic flow field density field

ActiveCN102706529ALarge measuring rangeIncreased spatio-temporal resolutionAerodynamic testingNanoparticleImage resolution
The invention provides a method for calibrating a supersonic flow field density field. According to the method, a supersonic flow field density-nanoparticle-based planar laser scattering (NPLS) image gray curve is calibrated by adopting a comprehensive oblique shock wave and expansion wave calibration method based on an NPLS technology. The method comprises the following steps of: 1, uniformly scattering trace particles in supersonic incoming flow, and shooting a particle image according to the instruction of a computer by a charge coupled device (CCD); 2, continuously adjusting obliqueness of an attack angle alpha in a supersonic wind tunnel, and acquiring a group of (rhoi, Ii) (i=1, 2, L, n-1) data by changing the oblique attack angle alpha; 3, placing expansion wave generators in the supersonic wind tunnel, and acquiring the other group of (rhoi, Ii) (i=n, n+1, L, N) data by placing the expansion wave generators with different deflection angles; and 4, performing polynomial fitting on the two groups of data to obtain the supersonic flow field density-NPLS image gray relation curve, namely rho=alapha0+alpha1I+alpha2I2+alpha3I3+K. The method aims to solve the technical problems of low spatial resolution and low signal-noise ratio and high error on measurement of a low-density area.
Owner:NAT UNIV OF DEFENSE TECH

Method for measuring solid particle three-dimensional concentration field and velocity field in gas/solid two-phase stream

The invention discloses a kind of method of measurement the solid particle three-dimensional density field in the gas and solid two phase flow, velocity field and equipment. The particle flux transmitting tube is laid at the front of high rate stereoscopic vision system which is consisted by the double look-out angle lens stereoscope and the high rate camera and the jet stream particle is refracted through the double look-out angle lens stereoscope mirror face and the single high rate camera target area can achieve the particle flux graphic with two different angles at the same time and after the graphic is input the computer a program module which is consisted by the pattern recognition algorithm procedure and three-inversion projection algorithm procedure treats the particle diagram and then get the transient three-dimensional density field. The program module treats series microsecond class time sequence changeable particle graphic and gets the particle three-dimensional movement trace and the velocity field. It is stabilize by using the single camera system and overcomes the problem of multiple camera system's constructer is complex and the synchronism is bad.
Owner:ZHEJIANG UNIV

Full field measuring system and method of reynolds stress of compressible turbulent flow

The invention provides a full field measuring system and method of reynolds stress of a compressible turbulent flow. The method comprises the steps that: nano trace particles are put into an experimental section of a wind tunnel by a nano particle generator; a second control signal is sent out by a synchronous controller according to a first control signal of a computer; after the second control signal is received by a charge coupled device (CCD) camera, a flow field in the experimental section of the wind tunnel is exposed, and meanwhile, laser beams are successively emitted by a double-cavity laser within the time of exposure of the CCD camera; two nano particle images relevant to the time are obtained by the CCD camera; and the velocity field and the density field of the flow field are simultaneously obtained by the computer according to the two nano particle images relevant to the time, and then the reynolds stress of the compressible turbulent flow is obtained. Through the full field measuring system and method, the technical problem that the velocity field and the density field cannot be simultaneously obtained can be solved, and then the aims that the velocity field and the density field of the compressible turbulent flow are simultaneously measured and the reynolds stress of the compressible turbulent flow is obtained according to the velocity field and the density field which are simultaneously measured are achieved.
Owner:NAT UNIV OF DEFENSE TECH

Quick volume data skeleton extraction method based on rendering

The invention relates to a quick volume data skeleton extraction method based on rendering. The quick volume data skeleton extraction method comprises the following steps: under upper, lower, front, rear, left and right viewpoints, using a RayCasting direct volume rendering algorithm to render three-dimensional volume data, so as to obtain six two-dimensional images; extracting the contours and partial key feature lines of all the two-dimensional images obtained through direct volume rendering; projecting the obtained contours and partial key feature lines of the two-dimensional images back to a three-dimensional space, so as to obtain a three-dimensional standby curve; sampling the space, calculating curve density of space sampling points and constructing a curve density field; after the curve density field is obtained, obtaining the gradients of the sampling points through a three-dimensional Sobel operator; according to the gradient values of the sampling points, calculating the curve directions of the sampling points through a least-square method; assigning the curve direction to the voxels of the corresponding three-dimensional volume data; according to the directions of the voxels, constructing a bounding box and calculating the average value of the voxels of the bounding box to obtain characterization nodes; connecting the characterization nodes and smoothing the connecting curve, so as to obtain a three-dimensional volume data skeleton.
Owner:BEIHANG UNIV

Equivalent method for cross-scale thermal analysis of fiber toughening composite material based on multiple criteria such as cross entropy and the like

ActiveCN105550390AFully Characterize HeterogeneityFully characterize the dispersion of physical propertiesSpecial data processing applicationsDispersityToughening
The invention discloses an equivalent method for cross-scale thermal analysis of a fiber toughening composite material based on multiple criteria such as a cross entropy and the like. The method comprises the following steps: establishing a random representative unit and enabling CMC fiber reinforcement phases to be randomly distributed by utilizing a Monte-Carlo method in the unit; establishing SRVEs for multiple times and performing finite element simulation on the SRVEs to obtain statistic data of thermal physical quantities such as an equivalent heat conduction coefficient of the composite material, a material temperature gradient field and a thermal flux density field; and adjusting the size of a PRVE, determining the critical size of the PRVE after multiple convergence criteria such as a mean value, a variance, the cross entropy and the like of the thermal physical quantities are met, obtaining the distribution of the equivalent heat conduction coefficient of the composite material, the material temperature gradient field and the thermal flux density field, and establishing a corresponding relationship between a microscopic structure and a macroscopic property. According to the method, heterogeneous characteristics and existent physical dispersity in the composite material are fully considered and judgment bases are provided for how to determine the critical size of the PRVE in thermal analysis of the composite material, so that the corresponding relationship between the microscopic structure and the macroscopic property can be established more accurately.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Magnetic interference heavy medium cyclone

The invention discloses a heavy medium cyclone separation device applied to separation of non-magnetic ore such as coarse slime. The heavy medium cyclone separation device comprises a cyclone column, and a cyclone cone arranged at the lower end of the cyclone column, wherein a cyclone feeding pipe is arranged at the upper part of the cyclone column; a cyclone center pipe which stretches into the cyclone column is arranged in the cyclone column; an inner magnetic pole excitation coil is arranged on the exposed section of the cyclone center pipe; an outer magnetic pole group is arranged at the periphery of the lower part of the cyclone column; the outer magnetic pole group consists of multiple electromagnets; outer magnetic pole excitation coils of the electromagnets are connected in series together and load exciting current I1together, and the inner magnetic pole excitation coils load current I2; the magnetic polarity on one side, which is close to the cyclone column, of the electromagnets is different from the magnetic polarity at the lower end of the cyclone center pipe. The magnetic field distribution in a cyclone area of the cyclone is controlled by adjusting the current of inner and outer dual-control electromagnetic pole coils, and motion of magnetic mineral powder in a special heavy medium cyclone is subjected to magnetic interference, so that a density field inside the cyclone is changed, and an effect of controlling separation of the heavy medium cyclone is achieved.
Owner:CHINA UNIV OF MINING & TECH

Polarization imaging based supersonic/hypersonic flow field measurement method

The invention discloses a polarization imaging based supersonic / hypersonic flow field measurement method. The method comprises the following steps: optimizing a line-biased laser light source for incident illumination such that the polarization degree of the incident line-biased laser is within a set threshold range; adjusting the polarization direction of the incident line-biased laser and the receiving angle of a polarization imaging system so as to make a scattering signal of nanoparticles at the imaging angle of the polarization imaging system strongest; using the polarization imaging system to image the supersonic / hypersonic flow field to obtain a polarization-related result of the scattered light signal of the nanoparticles, wherein the polarization-related result includes the polarization degree, the polarization angle, and the ellipsometric angle of the scattered light of the nanoparticles; and converting the density field of the supersonic / hypersonic flow field based on the polarization information to obtain density distribution of the supersonic / hypersonic flow field. The invention utilizes the polarization parameter information of the scattering signal of the nanoparticles to realize the visualization and fine measurement of the flow field, and has good anti-interference ability and high precision.
Owner:NAT UNIV OF DEFENSE TECH

Method for enriching flame simulation details through turbulence equation

The invention relates to a method for enriching flame simulation details through a turbulence equation. The method comprises the steps that (1) an Euler method based on a grid is adopted, a Navier-Stokes equation is solved in an accelerated mode through a CUDA, and a speed field of flames, a density field of the flames and a temperature field of the flames are obtained; (2) the standard k-e turbulence equation is simplified by the adoption of the particle method, and the CUDA is used for accelerating solving to obtain the turbulence energy and the energy dissipation rate of a particle; (3) a narrowband random texture field is generated, then the rotation is solved to obtain the speed field, and sampling is conducted in the random speed field according to the position of the particle to obtain the speed of the position where the particle is located; (4) the turbulence speed of the particles is synthesized, then the speed is used for disturbing the speed of the positions of network nodes in a neighborhood of the particle at the Gauss attenuation weight, and the density field and the temperature field are driven to move; (5) the CUDA and mapping of a buffer area of an OpenGL are used for directly rendering a data field worked out by the CUDA, and flame surface patches are obtained.
Owner:BEIHANG UNIV
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