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2263 results about "Fluid field" patented technology

Speed change pressure flow field control method applicable to intermittent transonic speed wind tunnel

InactiveCN103123504ARealize the requirements of variable speed pressure flow field controlQuick test effectAerodynamic testingFluid pressure control using electric meansAviationEngineering
The invention provides a speed change pressure flow field control method applicable to an intermittent transonic speed wind tunnel, and relates to the technical field of aerospace industry wind tunnel tests. The speed change pressure flow field control method applicable to the intermittent transonic speed wind tunnel solves the problem that a traditional flow field control method can not meet the requirements of flutter tests. The technical scheme includes: enabling total pressure and main ejector pressure to rise to first stage set value in a given rate after a wind tunnel starts ramming; controlling a mach number to reach set target value in a flow field regulating procedure; controlling a main pressure regulating valve and a main air discharge valve so as to enable the total pressure of the wind tunnel and the main ejector pressure to reach respective target value in a change total pressure regulating procedure; and controlling the current main ejector pressure to gradually drop to set shutdown main ejector pressure and controlling the current wind tunnel total pressure to gradually drop to set wind tunnel total pressure value when the wind tunnel is shut down. The speed change pressure flow field control method applicable to the intermittent transonic speed wind tunnel can meet the requirements of the flutter tests for intermittent transonic speed wind tunnel flow field control, has rapid, accurate and reliable test effects, and furthermore is high in total pressure control and mach number control accuracy.
Owner:INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT

Method and device for simultaneously measuring droplet position, particle sizes and complex refractive index

The invention relates to technology for simultaneously measuring multi-phase flow particles online through multi-parameter, and aims to provide a method and a device for simultaneously measuring droplet positions, particle sizes and a complex refractive index. The method comprises the following steps of: (1) dividing a highly coherent continuous laser beam into two beams after spatial filtering and collimating beam expansion, wherein one beam radiates particles in a detected flow field region, and the other beam is used as a reference beam; (2) mixing scattered light of a lateral 30-degree to 90-degree region of particles in the detected flow field region and the attenuated reference beam to perform interference so as to form a hologram, storing the hologram in a computer after being recorded by a digital camera through an imaging device; (3) acquiring a series of reconstructed images of the detected particles along the depth direction by utilizing digital reconstruction technology; and (4) identifying the reflective spot and the refractive spot of the particles from the reconstructed images by utilizing digital image processing technology so as to acquire space coordinates and scattered light intensity ratios. Compared with rainbow measurement technology, the measurement method has the advantages that: a light path system of the measurement device is relatively simple and is easy to implement.
Owner:ZHEJIANG UNIV

Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment

The invention relates to a method and a device for spreading trace particles in a supersonic PIV (Particle Image Velocimetry) flow field testing experiment. The trace particles are charged by using vacuum suction in a supersonic wind tunnel high-pressure high-temperature large-flow flow field environment, the trace particles are stored in a particle generator before the experiment, after a gas flow is injected, the gas flow and the trace particles are sufficiently mixed, pass through a high-pressure pipeline, are spread by a particle spreader and then enter a wind tunnel pipeline, the trace particles are uniformly spread under the condition of a high-Mach-number flow, and the trace particles are tested through a particle image velocity-measuring system. Compared with the prior art, the method and the device provided by the invention realize that the PIV trace particles are charged and uniformly spread in a high-pressure high-temperature large-flow flow field ambient condition, the probable agglomeration phenomenon of the trace particles in the injection process is effectively avoided, precise sequence control between a PIV system and wind tunnel operation is guaranteed, and the testing scheme corresponding to the spreading concentration satisfying the PIV operation requirement is determined.
Owner:SHANGHAI JIAO TONG UNIV

Two-dimensional reconstruction light distribution optimization method based on laser absorption spectrum technology

ActiveCN103884663AImprove utilization efficiencyImprove the quality of reconstruction resultsThermometers using physical/chemical changesColor/spectral properties measurementsDistribution matrixAdaptive simulated annealing
The invention provides a light distribution optimization method for two-dimensional reconstruction of a combustion flow field by combining a tunable semiconductor laser absorption spectrum technology and a computed tomography technology. The method comprises the following steps: a light matrix calculation step, a combustion flow field reconstruction step and a light distribution optimization step and particularly comprises the following steps: step 1, discretizing a region to be tested; pre-setting a light space distribution manner and calculating the length of light penetrating through the discretized region to obtain a light distribution matrix; step 2, selecting a suitable absorption spectrum line and calculating a light projection result of an initial gas distribution model; reconstructing temperatures and concentrations of the tested flow field by using an algebra iterative algorithm and calculating a reconstruction error and a standard deviation; and step 3, wholly searching by using a self-adaption simulated annealing method to obtain an optimal light distribution range and partially searching by using a sequential quadratic programming method to obtain optimal light distribution.
Owner:PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV

Gas diffusion layer with gradient hole structure and preparation and applications thereof

The invention relates to a gas diffusion layer with a gradient hole structure for fuel batteries and a preparation method and applications thereof. The gas diffusion layer consists of a macroporous carbon-based support body and a micro-porous layer which are overlapped, wherein the material of the micro-porous layer is embedded in the macroporous carbon-based support body from one side, far from the flow field of a battery, of the macroporous carbon-based support body to form a transitional hole layer; the transitional hole layer is composed of the material of the micro-porous layer and the fiber of the macroporous carbon-based support body and is obtained by embedding the material of the micro-porous layer in the side, far from the flow field of a battery, of the macroporous carbon-based support body; and the curvature of reaction gas transfer from the side next to the flow field to the side next to a catalyst layer in the gas diffusion layer increases gradiently and the air permeability gradually reduces from 4-10s/100ml to 100-900s/100ml. By adopting the gas diffusion layer with the structure, the mass transfer curvatures of water and the gas in the gas diffusion layer (GDL) can be effectively increased, the transfer path of the product-water can be prolonged and liquid water in the battery can be maintained; and the gas diffusion layer is particularly suitable for fuel batteries working under low humidity and the cathodes of alkaline fuel batteries.
Owner:DALIAN INST OF CHEM PHYSICS CHINESE ACAD OF SCI

Fully-three-dimensional simulated visualized displacement simulation experiment system of fractured-vuggy oil reservoir

The invention relates to a fully-three-dimensional simulated visualized displacement simulation experiment system of a fractured-vuggy oil reservoir. The fully-three-dimensional simulated visualized displacement simulation experiment system comprises trough, fractured-vuggy model, water injection, air injection, image acquisition and data acquisition simulation unit, a simulation oil groove and a three-phase separator. The trough simulation unit comprises a cubic trough, a glass pipe and a shaft. The fractured-vuggy model simulation unit comprises a cavern model and a crack model. The water injection simulation unit comprises a water injection tank and a water pump. The air injection simulation unit comprises an air compressor, an air storage tank, an emptying valve, a water draining filter and an air dryer. A particle forming test module of the image acquisition simulation unit is arranged on a sliding rod and installed on a support through the sliding rod. A pressure variator of the data acquisition simulation unit is installed at the connecting position of the shaft and the fractured-vuggy model simulation unit. The output end of the three-phase separator is respectively connected with the simulation oil groove and the water injection tank, and the input end of the three-phase separator is connected with the shaft. The fully-three-dimensional simulated visualized displacement simulation experiment system of the fractured-vuggy oil reservoir is simple and reasonable in structural design and capable of timely, intuitively and accurately monitoring a flow field and pressure change in a stratum.
Owner:SOUTHWEST PETROLEUM UNIV

Device and method for use of impeller of laser 3D (three dimensional) -printing pump

The invention discloses a device and a method for the use of an impeller of a laser 3D (three dimensional) -printing pump, and belongs to the field of 3D printing technology. The device comprises a laser system, a gas protection system, a preheating system, a powder feeding system, a powder paving system, a powder recycle system and a computer system. The manufacturing method mainly comprises the following steps that 1, a CAD solid model of the pump impeller is drawn, and the model is subjected to hierarchical slicing along the Z direction; 2, the slice in each layer is zoned into a zone I and a zone II according to the performance requirements of the pump impeller; 3, the zone I of each slice layer is subjected to low-speed sintering by using powder A, and the zone II is subjected to low-speed sintering by using powder B. The surface of a workpiece and the powder flow filed are subjected to the inert gas shielding in the process of printing. According to the device and the method for the use of the impeller of the laser 3D-printing pump, different requirements of different positions of the pump impeller on mechanical performance can be met, the printing quality and speed are also improved, and the manufacturing cost is reduced.
Owner:江苏大学扬州(江都)新能源汽车产业研究所

Ejector-driven closed-loop recirculation temporary impulse supersonic wind tunnel flow field control method

The invention discloses an ejector-driven closed-loop recirculation temporary impulse supersonic wind tunnel flow field control method. An ejector arranged behind a diffusion section is adopted as themain drive of a wind tunnel flow field, under the cooperation of a recirculation regulating valve, an assisting air admission pressure regulating valve and an exhaust throttle valve, a stable supersonic flow field is established, wherein precise control of the total pressure of a stabilizing section is achieved under the mutual action of a pressure regulating valve of the ejector and the assisting air admission pressure regulating valve, and on the basis of the precise control of the total pressure, the establishing of stable supersonic flow fields with different M values under the same operation total pressure in a temporary impulse supersonic wind tunnel can be achieved under the cooperation of a nozzle profile surface and a diffusion section profile surface. By means of the method, thesimulation of negative pressure working conditions can be achieved in a closed-loop recirculation temporary impulse supersonic wind tunnel, the operating envelope and simulation range of the wind tunnel are effectively expanded, and the total pressure of a stabilizing section needed by the establishing of a supersonic flow field when the M value of a traditional temporary impulse wind tunnel is high can be significantly reduced, which facilitates the aerodynamic loading of a model and the improvement of the measuring accuracy of a strain gauge balance of the wind tunnel.
Owner:INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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