CN206832296U - A kind of gas jet characteristic comprehensive measurement device - Google Patents
A kind of gas jet characteristic comprehensive measurement device Download PDFInfo
- Publication number
- CN206832296U CN206832296U CN201720704213.1U CN201720704213U CN206832296U CN 206832296 U CN206832296 U CN 206832296U CN 201720704213 U CN201720704213 U CN 201720704213U CN 206832296 U CN206832296 U CN 206832296U
- Authority
- CN
- China
- Prior art keywords
- real
- gas
- gas jet
- time acquisition
- jet
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000005259 measurement Methods 0.000 title claims abstract description 23
- 238000007664 blowing Methods 0.000 claims abstract description 50
- 238000002347 injection Methods 0.000 claims abstract description 42
- 239000007924 injection Substances 0.000 claims abstract description 42
- 238000012360 testing method Methods 0.000 claims abstract description 25
- 230000001105 regulatory effect Effects 0.000 claims abstract description 9
- 239000007789 gas Substances 0.000 description 84
- 238000000034 method Methods 0.000 description 11
- 239000012530 fluid Substances 0.000 description 10
- 239000002245 particle Substances 0.000 description 10
- 238000010586 diagram Methods 0.000 description 7
- 238000009826 distribution Methods 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 7
- 230000008569 process Effects 0.000 description 6
- 239000000700 radioactive tracer Substances 0.000 description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 239000001301 oxygen Substances 0.000 description 4
- 229910052760 oxygen Inorganic materials 0.000 description 4
- 238000000917 particle-image velocimetry Methods 0.000 description 4
- 238000011160 research Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 238000011056 performance test Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 238000003723 Smelting Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 2
- 238000009795 derivation Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000691 measurement method Methods 0.000 description 2
- 238000005272 metallurgy Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000005305 interferometry Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000010310 metallurgical process Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000000827 velocimetry Methods 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Landscapes
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
本实用新型涉及一种气体射流特性综合测量装置,包括气体射流发生装置和测试数据实时采集系统,所述气体射流发生装置包括依次通过供气管道连接的高压气源、稳压罐、调节阀、截止阀、喷吹装置;所述测试数据实时采集系统包括气体管道压力实时采集装置、气体管道流量实时采集装置、气体射流喷吹力实时采集装置、采集模块以及计算机。本实用新型一种气体射流特性综合测量装置,首次通过同时直接测量射流的流量、管道压力以及喷吹力描述射流的物理行为,比描述射流的速度流场更直接反映气体射流对熔池液面的作用,能够多维度综合描述射流装置或喷头性能。
The utility model relates to a gas jet characteristic comprehensive measurement device, which comprises a gas jet generating device and a real-time test data acquisition system. The gas jet generating device includes a high-pressure gas source connected sequentially through a gas supply pipeline, a pressure-stabilizing tank, a regulating valve, Stop valve, injection device; the test data real-time collection system includes a gas pipeline pressure real-time collection device, a gas pipeline flow real-time collection device, a gas jet injection force real-time collection device, a collection module and a computer. The utility model is a comprehensive measurement device for gas jet characteristics, which describes the physical behavior of the jet by directly measuring the flow rate, pipeline pressure and blowing force of the jet at the same time for the first time. It can comprehensively describe the performance of fluidic devices or nozzles in multiple dimensions.
Description
技术领域technical field
本实用新型属于流体力学的气体射流测量技术领域,涉及一种气体射流特性综合测量装置。The utility model belongs to the technical field of gas jet flow measurement of fluid mechanics, and relates to a comprehensive measurement device for gas jet flow characteristics.
背景技术Background technique
气体射流技术在航空航天、冶金、化工、食品加工领域广泛应用。在冶金领域,气体射流被应用于转炉、电炉冶炼、RH真空精炼等冶金过程,喷吹气体射流冲击到熔池液面引起反应器内熔池的穿透、喷溅、流动等复杂物理现象。在吹炼过程中,喷吹气体射流对熔池液面的冲击力对于熔池内的冶金效率、成渣速率和钢液飞溅情况有较大影响。故而,顶吹装置的喷吹性能测试和喷吹气体射流特性的研究成为顶吹技术研究的重点和难点。鉴于冶炼环境具有高温等特殊条件,无法直接观察、测量喷吹气体射流的流体特性和对熔池液面的物理行为,通常采用冷态试验对气体射流特性进行研究。Gas jet technology is widely used in aerospace, metallurgy, chemical industry, and food processing fields. In the field of metallurgy, gas jets are used in metallurgical processes such as converters, electric furnace smelting, and RH vacuum refining. The impact of the injected gas jets on the liquid surface of the molten pool causes complex physical phenomena such as penetration, splashing, and flow of the molten pool in the reactor. During the blowing process, the impact force of the injected gas jet on the liquid surface of the molten pool has a great influence on the metallurgical efficiency, slagging rate and molten steel splashing in the molten pool. Therefore, the injection performance test of the top blowing device and the research on the characteristics of the injection gas jet have become the focus and difficulty of the top blowing technology research. In view of the special conditions such as high temperature in the smelting environment, it is impossible to directly observe and measure the fluid characteristics of the injected gas jet and the physical behavior of the liquid surface of the molten pool. The characteristics of the gas jet are usually studied by cold test.
皮托管测速法是一种应用较为普遍的气体射流测量方法,将皮托管放入气体射流测量射流中某一点的总压和静压的压差,根据伯努利方程计算得到该点的流体流速,进而测得气体射流的流体特性。但测量超音速射流时,皮托管的置入会造成流场扰动,给测量带来困难。Pitot tube velocimetry is a commonly used gas jet measurement method. Put the pitot tube into the gas jet to measure the pressure difference between the total pressure and the static pressure at a certain point in the jet, and calculate the fluid flow rate at this point according to the Bernoulli equation. , and then measure the fluid characteristics of the gas jet. However, when measuring supersonic jet flow, the placement of pitot tube will cause flow field disturbance, which will bring difficulties to the measurement.
粒子图像测速(PIV)技术是一种非侵入式流体测量技术,通过在射流中投入示踪粒子,利用图像记录系统(如CCD相机等)记录不同时刻下示踪粒子在流场中的位置,利用图像处理技术计算示踪粒子的位移和速度,从而得到粒子所在位置的流体速度和相关运动参数。Particle image velocimetry (PIV) technology is a non-invasive fluid measurement technology, by injecting tracer particles into the jet, using an image recording system (such as a CCD camera, etc.) to record the position of the tracer particles in the flow field at different times, Using image processing technology to calculate the displacement and velocity of the tracer particles, so as to obtain the fluid velocity and related motion parameters at the particle location.
激光相位多普勒粒子分析(PDPA)技术通过在射流中投放示踪粒子,利用多普勒分析仪测量激光照射下示踪粒子散射光的多普勒频移,根据多普勒频移计算粒子速度,进而得到粒子所在位置的流体速度。Laser Phase Doppler Particle Analysis (PDPA) technology puts tracer particles in the jet, uses a Doppler analyzer to measure the Doppler frequency shift of the scattered light of the tracer particles under laser irradiation, and calculates the particle size based on the Doppler frequency shift. Velocity, and then get the fluid velocity at the position of the particle.
实用新型专利申请201410146590.9公开了一种气体喷射流场的测量方法。利用沃拉斯顿棱镜光学元件组成差分干涉测量系统,对测试段空间流场中心剖面成像,采集气流喷射前和气流喷射时任一时刻的带有载波条纹的差分干涉条纹图,进而获得全场的条纹级数分布和流体光学折射率梯度,并同时获得流体的密度梯度场,密度场,温度场,温度梯度场。Utility model patent application 201410146590.9 discloses a measurement method of gas jet flow field. The Wollaston prism optical element is used to form a differential interferometry system to image the center section of the space flow field in the test section, and collect the differential interference fringe pattern with carrier fringes at any time before and during the airflow injection, and then obtain the whole field The fringe series distribution and fluid optical refractive index gradient, and simultaneously obtain the fluid density gradient field, density field, temperature field, and temperature gradient field.
实用新型专利申请201510644060.1公开了一种贴壁射流速度场和浓度场的同步测量装置和方法,通过使用PIV相机拍摄贴壁射流中PIV粒子在主气流中的流动轨迹,以及高速CCD摄像机拍摄氧敏涂层壁面随射流中氧浓度变化的显色规律,实现贴壁射流与主气流相互作用过程中速度场和浓度场的同步测量。Utility model patent application 201510644060.1 discloses a device and method for synchronously measuring the velocity field and concentration field of the wall-adhering jet, by using a PIV camera to shoot the flow trajectory of PIV particles in the main airflow in the wall-attached jet, and a high-speed CCD camera to shoot oxygen-sensitive The color development law of the coating wall surface changes with the oxygen concentration in the jet, and realizes the simultaneous measurement of the velocity field and concentration field during the interaction between the wall-attached jet and the main airflow.
文献《喷管性能测试系统开发》公开了一种喷管性能测试系统,该系统利用测压探针、负压传感器、压差传感器、位移电位器等测量喷管前后压力的比值来反映喷管中不同截面处的压力变化,并通过所测压差计算流体流量。The document "Development of Nozzle Performance Test System" discloses a nozzle performance test system, which uses pressure measuring probes, negative pressure sensors, differential pressure sensors, displacement potentiometers, etc. to measure the ratio of the pressure before and after the nozzle to reflect the pressure of the nozzle. The pressure change at different cross-sections in the medium, and the fluid flow is calculated from the measured pressure difference.
文献《火箭燃气冲击载荷识别平台的设计与研究》公开了一种火箭燃气射流冲击载荷识别的通用测量平台,该系统基于Stewart平台的衍生机构3-(2SPS)并联机构,将一维拉压力传感器通过并联机构组合为六维力测量平台。当测量平台上的被测模型受到冲击载荷时,通过对六根驱动杆上一维拉压力传感器的输出值进行耦合,可测得被测模型所受的力载荷。该系统可直接测量射流的冲击载荷,但存在平台结构复杂、测量系统标定过程困难繁琐的缺点。The document "Design and Research of Rocket Gas Shock Load Identification Platform" discloses a general measurement platform for rocket gas jet impact load identification. A six-dimensional force measurement platform is combined through a parallel mechanism. When the model under test on the measuring platform is subjected to impact loads, the force load on the model under test can be measured by coupling the output values of the one-dimensional pressure sensors on the six driving rods. The system can directly measure the impact load of the jet, but it has the disadvantages of complex platform structure and difficult and cumbersome calibration process of the measurement system.
文献《顶吹气体平面射流对熔池穿透深度的冷态试验研究》公开了一种测量喷吹射流冲击力的方法,通过测量气体射流对水面的冲击深度,根据冲击深度和水表面张力推导计算喷吹射流冲击力。该方法能较直观地反应气体射流的冲击效果,但仅适用于模型实验,难以实施于实际工程现场喷吹装置的射流特性评价,且存在推导计算过程繁琐、无法描述射流发散程度等其他射流特性等缺点。The document "Cold Experimental Research on Penetration Depth of Top-blown Gas Plane Jet to Melt Pool" discloses a method for measuring the impact force of the jet. By measuring the impact depth of the gas jet on the water surface, it is derived from the impact depth and water surface tension. Calculate the blowing jet impact force. This method can reflect the impact effect of the gas jet more intuitively, but it is only suitable for model experiments, and it is difficult to implement the evaluation of the jet characteristics of the injection device in the actual engineering site, and there are other jet characteristics such as cumbersome derivation and calculation process, and the inability to describe the degree of jet divergence. and other shortcomings.
现有的气体射流测量技术大部分通过测量射流流速描述气体射流的流场特性,无法多维度综合描述射流装置或喷头性能,并存在测试系统复杂、成本高昂、计算推导过程繁琐等缺点,且难以在实际工程现场实施、测量评价喷吹装置的射流特性。Most of the existing gas jet measurement technologies describe the flow field characteristics of the gas jet by measuring the jet flow velocity, which cannot comprehensively describe the performance of the jet device or nozzle in multiple dimensions, and have the disadvantages of complex test system, high cost, cumbersome calculation and derivation process, and difficult Implement, measure and evaluate the jet characteristics of the injection device at the actual project site.
实用新型内容Utility model content
有鉴于此,本实用新型的目的在于提供一种一种气体射流特性综合测量装置。In view of this, the purpose of this utility model is to provide a kind of gas jet characteristic comprehensive measurement device.
为达到上述目的,本实用新型提供如下技术方案:In order to achieve the above object, the utility model provides the following technical solutions:
一种气体射流特性综合测量装置,包括气体射流发生装置和测试数据实时采集系统;所述测试数据实时采集系统包括气体管道压力实时采集装置、气体管道流量实时采集装置、气体射流喷吹力实时采集装置、采集模块以及计算机,所述气体射流喷吹力实时采集装置正对气体射流发生装置设置并可相对气体射流发生装置移动,所述气体管道压力实时采集装置、气体管道流量实时采集装置设置在气体射流发生装置的气体通道入口处,所述气体射流喷吹力实时采集装置、气体管道压力实时采集装置、气体管道流量实时采集装置均通过采集模块连接计算机。A gas jet characteristic comprehensive measurement device, comprising a gas jet generating device and a real-time test data acquisition system; the test data real-time acquisition system includes a gas pipeline pressure real-time acquisition device, a gas pipeline flow real-time acquisition device, and a gas jet injection force real-time acquisition device, acquisition module and computer, the gas jet blowing force real-time acquisition device is set up against the gas jet generation device and can move relative to the gas jet generation device, and the gas pipeline pressure real-time acquisition device and gas pipeline flow real-time acquisition device are set at At the entrance of the gas channel of the gas jet generating device, the gas jet blowing force real-time acquisition device, the gas pipeline pressure real-time acquisition device, and the gas pipeline flow real-time acquisition device are all connected to the computer through the acquisition module.
进一步,所述气体射流发生装置设置在测试平台上。Further, the gas jet generating device is set on a test platform.
进一步,所述气体射流发生装置包括依次通过供气管道连接的高压气源、稳压罐、调节阀、截止阀、喷吹装置,所述气体射流喷吹力实时采集装置正对喷吹装置设置并可相对喷吹装置移动,所述气体管道压力实时采集装置、气体管道流量实时采集装置设置在喷吹装置的气体通道入口处。Further, the gas jet generating device includes a high-pressure gas source, a surge tank, a regulating valve, a shut-off valve, and a blowing device that are sequentially connected through a gas supply pipeline, and the real-time collection device for the blowing force of the gas jet is set facing the blowing device And it can move relative to the blowing device. The gas pipeline pressure real-time acquisition device and the gas pipeline flow real-time collection device are arranged at the gas channel inlet of the blowing device.
进一步,所述气体射流喷吹力实时采集装置设置在喷吹装置喷头的中心线正下方。Further, the real-time collection device for the blowing force of the gas jet is arranged directly below the center line of the nozzle of the blowing device.
进一步,所述气体射流喷吹力实时采集装置包括测力盘、测力盘支架、力传感器、固定装置,所述测力盘可拆卸地设置在测力盘支架上,通过力传感器固定在固定装置上,所述固定装置的高度可调节。Further, the gas jet blowing force real-time acquisition device includes a force measuring disc, a force measuring disc support, a force sensor, and a fixing device. On the device, the height of the fixing device is adjustable.
本实用新型的有益效果在于:本实用新型一种气体射流特性综合测量装置,首次通过同时直接测量射流的流量、管道压力以及喷吹力描述射流的物理行为,比描述射流的速度流场更直接反映气体射流对熔池液面的作用,能够多维度综合描述射流装置或喷头性能。本实用新型所述测量装置简单、测试成本低廉,所述方法数据处理过程简单直观,实施难度低,可在实际工程中现场测试评价喷吹装置的射流特性。The beneficial effect of the utility model is that: the utility model is a comprehensive measurement device for gas jet characteristics, which is the first time to directly measure the jet flow, pipeline pressure and blowing force to describe the physical behavior of the jet, which is more direct than describing the velocity flow field of the jet Reflecting the effect of the gas jet on the liquid level of the molten pool, it can comprehensively describe the performance of the jet device or nozzle in multiple dimensions. The measuring device of the utility model is simple, the test cost is low, the data processing process of the method is simple and intuitive, the implementation difficulty is low, and the jet characteristics of the injection device can be tested and evaluated on the spot in actual engineering.
附图说明Description of drawings
为了使本实用新型的目的、技术方案和有益效果更加清楚,本实用新型提供如下附图进行说明:In order to make the purpose, technical solutions and beneficial effects of the utility model clearer, the utility model provides the following drawings for illustration:
图1是本实用新型气体射流特性综合测量装置的连接示意图;Fig. 1 is the connection schematic diagram of the comprehensive measuring device of gas jet characteristic of the present utility model;
图2是喷吹装置a和喷吹装置b的入口压力、流量和喷吹射流喷吹力对比图;Fig. 2 is the inlet pressure of injection device a and injection device b, flow rate and injection jet injection force contrast figure;
图3是喷吹装置a和喷吹装置b的集束性对比图;Fig. 3 is a cluster comparison diagram of injection device a and injection device b;
图4是喷吹装置a和喷吹装置b的发散度对比图;Fig. 4 is a divergence comparison diagram of injection device a and injection device b;
图5是1200mm处喷吹装置a的喷吹力分布图。Fig. 5 is a distribution diagram of the blowing force of the blowing device a at 1200 mm.
具体实施方式detailed description
下面将结合附图,对本实用新型的优选实施例进行详细的描述。The preferred embodiments of the present utility model will be described in detail below in conjunction with the accompanying drawings.
如图1所示,本实用新型一种气体射流特性综合测量装置的连接示意图,包括气体射流发生装置和测试数据实时采集系统,所述气体射流发生装置包括依次通过供气管道连接的高压气源、稳压罐1、调节阀3、截止阀4、喷吹装置8;所述测试数据实时采集系统包括气体管道压力实时采集装置5、气体管道流量实时采集装置6、气体射流喷吹力实时采集装置、采集模块13以及计算机14,本实施例气体射流喷吹力实时采集装置包括测力盘10、测力盘支架15、力传感器11、固定装置12,测力盘10可拆卸地设置在测力盘支架15上,通过力传感器11固定在固定装置12上述固定装置12的高度可调节。气体射流喷吹力实时采集装置正对设置在喷吹装置8喷头的下方,固定装置12可上下调节高度,从而改变喷头离测力盘10的距离,气体管道压力实时采集装置5、气体管道流量实时采集装置6设置在喷嘴装置的气体通道入口处,所述气体射流喷吹力实时采集装置、气体管道压力实时采集装置5、气体管道流量实时采集装置6均通过采集模块13连接计算机14。As shown in Figure 1, the connection schematic diagram of a gas jet characteristic comprehensive measurement device of the utility model includes a gas jet generating device and a real-time test data acquisition system, and the gas jet generating device includes a high-pressure gas source connected sequentially through a gas supply pipeline , surge tank 1, regulating valve 3, shut-off valve 4, blowing device 8; said test data real-time collection system includes gas pipeline pressure real-time collection device 5, gas pipeline flow real-time collection device 6, gas jet injection force real-time collection Device, acquisition module 13 and computer 14, the real-time acquisition device of gas jet blowing force in this embodiment includes a force measuring plate 10, a force measuring plate support 15, a force sensor 11, a fixing device 12, and the force measuring plate 10 is detachably arranged on the measuring plate On the force plate support 15, the height of the above-mentioned fixing device 12 is adjustable through the force sensor 11 fixed on the fixing device 12. The real-time acquisition device for the gas jet blowing force is located directly below the spray head of the blowing device 8, and the height of the fixing device 12 can be adjusted up and down to change the distance between the spray head and the force measuring plate 10. The real-time acquisition device for gas pipeline pressure 5, the flow rate of the gas pipeline The real-time acquisition device 6 is arranged at the entrance of the gas channel of the nozzle device. The real-time acquisition device for the gas jet injection force, the real-time acquisition device 5 for gas pipeline pressure, and the real-time acquisition device 6 for gas pipeline flow are all connected to the computer 14 through the acquisition module 13.
高压气源,压缩空气储气罐1,储气罐压力为0.6~0.67MPa,容积5m3,通过供气管道2与调节阀3法兰连接,用于提供测试介质压缩空气;High-pressure air source, compressed air storage tank 1, the pressure of the gas storage tank is 0.6-0.67MPa, the volume is 5m 3 , it is connected with the flange of the regulating valve 3 through the air supply pipeline 2, and is used to provide compressed air as the test medium;
调节阀3,通过供气管道1一端与气源法兰连接,另一端与截止阀4法兰连接,用于调节入口压力;The regulating valve 3 is connected to the air source flange through the air supply pipeline 1 at one end, and the other end is connected to the shut-off valve 4 flange to adjust the inlet pressure;
截止阀4,通过供气管道2一端与调节阀3法兰连接,另一端与气体通道入口7法兰连接,用于开启或切断气路;The shut-off valve 4 is flange-connected to the regulating valve 3 through the gas supply pipeline 2 at one end, and the other end is flange-connected to the gas channel inlet 7 for opening or cutting off the gas circuit;
气体管道压力实时采集装置5,采用压力变送器,量程0-1MPa,规格2线制4-20mA,安装于气体通道入口7处,用于测量、采集入口压力大小;The gas pipeline pressure real-time acquisition device 5 adopts a pressure transmitter with a range of 0-1MPa and a specification of 2-wire system of 4-20mA, installed at the inlet 7 of the gas channel for measuring and collecting the inlet pressure;
气体管道流量实时采集装置6,采用涡街流量计,型号DLTUGE13 06-P2,规格DN65法兰式,PN1.6MPa,量程0-1200Nm3/h,安装于气体通道入口7处,用于测量、采集气体流量大小;The gas pipeline flow real-time acquisition device 6 adopts a vortex flowmeter, model DLTUGE13 06-P2, specification DN65 flange type, PN1.6MPa, range 0-1200Nm 3 /h, installed at the entrance 7 of the gas channel, used for measurement, Acquisition gas flow rate;
喷吹装置8,本实施例采用的喷吹装置为喷吹装置a和喷吹装置b,分别测试喷吹装置a和喷吹装置b,进行比较;Blowing device 8, the blowing device that present embodiment adopts is blowing device a and blowing device b, respectively tests blowing device a and blowing device b, compares;
测试平台9,用于安装供气管道2、调节阀3、截止阀4、压力变送器、涡街流量计和喷吹装置7;The test platform 9 is used to install the gas supply pipeline 2, the regulating valve 3, the shut-off valve 4, the pressure transmitter, the vortex flowmeter and the blowing device 7;
测力盘10,面积分别为0.5m2和1m2的圆盘,安装在气体射流喷吹力实时采集装置上;Force measuring discs 10 , discs with areas of 0.5m2 and 1m2 respectively, are installed on the real-time acquisition device for gas jet blowing force;
气体射流喷吹力实时采集装置,型号NW50,最大称重范围:50KG,通过固定装置12安装于喷头中心线下,用于测量、采集射流喷吹力大小;Gas jet blowing force real-time acquisition device, model NW50, maximum weighing range: 50KG, installed under the center line of the nozzle through the fixing device 12, used to measure and collect the size of the jet blowing force;
固定装置12,用于安装测力盘10、测力盘支架15、力传感器11,固定装置12高度可调节。The fixing device 12 is used for installing the dynamometer 10 , the dynamometer support 15 , and the force sensor 11 , and the height of the fixing device 12 can be adjusted.
采集模块13和计算机14,用于数据采集、记录和显示。The collection module 13 and the computer 14 are used for data collection, recording and display.
顶吹气体射流特性综合测量的具体实施步骤如下:The specific implementation steps of the comprehensive measurement of the top-blowing gas jet characteristics are as follows:
(1)如图1所示连接好管路,将供气管道2连接至喷吹装置b的氧气通道入口7,连接仪表线路,调试就绪;(1) Connect the pipeline as shown in Figure 1, connect the gas supply pipeline 2 to the oxygen channel inlet 7 of the blowing device b, connect the instrument circuit, and the debugging is ready;
(2)对储气罐充气到0.65~0.67MPa备用,通过调节阀3调整入口压力为0.45MPa;(2) Inflate the gas storage tank to 0.65-0.67MPa for standby, and adjust the inlet pressure to 0.45MPa through the regulating valve 3;
(3)将0.5m2测力盘10安装在气体射流喷吹力实时采集装置上,测力盘10距喷口1200mm;( 3 ) 0.5m dynamometer 10 is installed on the gas jet blowing force real-time acquisition device, dynamometer 10 is 1200mm away from the nozzle;
(4)开启截止阀4,其间自动采集入口压力、流量及喷吹力,同时记录大气温度、气压,30秒后关闭截止阀3;(4) Open the shut-off valve 4, automatically collect inlet pressure, flow and injection force, record the atmospheric temperature and air pressure simultaneously, and close the shut-off valve 3 after 30 seconds;
(5)重复测试3次以上;(5) Repeat the test more than 3 times;
(6)更换不同测力盘10和气体射流喷吹力实时采集装置的位置进行测试,气体射流喷吹力实时采集装置依次安装在喷头中心线下距喷头1200mm、1700mm、2200mm、2700mm距离,分别测量0.5m2和1m2面积的圆盘上的射流喷吹力。(6) Change the positions of different force measuring discs 10 and real-time acquisition devices for gas jet injection force for testing. The real-time acquisition devices for gas jet injection force are installed successively at distances of 1200mm, 1700mm, 2200mm, and 2700mm from the nozzle, respectively, under the center line of the nozzle. Measure the jet blowing force on discs of 0.5m2 and 1m2 area.
(7)将供气管道1连接至喷吹装置a的氧气通道入口,重复步骤(2)~(6)。(7) Connect the gas supply pipeline 1 to the inlet of the oxygen channel of the blowing device a, and repeat steps (2) to (6).
测试完毕后,对试验数据进行处理和分析。如图2所示,喷吹力随测力盘10与出口距离的增大而逐渐减小,小测力盘和大测力盘所测喷吹力的差值逐渐增大,意味着射流随离开喷口的距离发散;测力盘10与出口距离相同条件下,喷吹装置a喷吹力小于喷吹装置b,意味着喷吹装置a对钢液面的冲击力小于喷吹装置b。After the test is completed, the test data is processed and analyzed. As shown in Figure 2, the blowing force gradually decreases with the increase of the distance between the force measuring disc 10 and the outlet, and the difference between the blowing force measured by the small force measuring disc and the large force measuring disc gradually increases, which means that the jet flow increases with the The distance from the nozzle diverges; under the condition that the distance between the dynamometer 10 and the outlet is the same, the injection force of the injection device a is smaller than that of the injection device b, which means that the impact force of the injection device a on the molten steel surface is smaller than that of the injection device b.
对喷吹过程中入口压力稳定段的喷吹力求平均值,以喷吹力为指标评价射流的集束性和发散度。集束性是指同一射流截面上射流喷吹力分布的集中程度;发散度是指距喷口不同距离下、同一受力面积上的射流喷吹力相对于喷口处相同受力面积上射流喷吹力的损失程度。按下式计算喷吹射流的集束性和发散度:Calculate the average value of the injection force in the stable inlet pressure section during the injection process, and use the injection force as an index to evaluate the concentration and divergence of the jet. Convergence refers to the degree of concentration of jet blowing force distribution on the same jet section; divergence refers to the jet blowing force on the same force-bearing area at different distances from the nozzle relative to the jet blowing force on the same force-bearing area at the nozzle. degree of loss. Calculate the concentration and divergence of the spray jet according to the following formula:
如图3所示是喷吹装置a和喷吹装置b的集束性对比图,圆孔喷头与环孔喷头的集束性相当。图4是喷吹装置a和喷吹装置b的发散度对比图,射流的发散度随距出口距离的增加而增大,在较小测力面积上,射流发散度的增加尤为显著。同时,随着距出口距离的增加,射流发散的程度更快、更明显;在该试验条件下,喷吹装置a的射流发散度大于喷吹装置b。As shown in Figure 3, it is a comparison diagram of the clustering of the spraying device a and the spraying device b, and the clustering of the circular hole nozzle and the ring hole nozzle is equivalent. Figure 4 is a comparison diagram of the divergence of the injection device a and the injection device b. The divergence of the jet increases with the increase of the distance from the outlet, and the increase of the divergence of the jet is particularly significant on a small force-measuring area. At the same time, as the distance from the outlet increases, the degree of jet divergence is faster and more obvious; under this test condition, the jet divergence of injection device a is greater than that of injection device b.
如图5所示,针对1200mm处喷吹装置a的喷吹力分布,通过采用不同面积(半径)大小的测力盘,可测得射流截面不同面积上的平均喷吹力大小,进而获得该截面上的喷吹力分布情况。可以发现,所采用的的测力盘越多、所测范围的面积(半径)分辨率越高,测试得到的喷吹力分布情况则越接近真实的喷吹力分布情况。As shown in Figure 5, for the distribution of the blowing force of the blowing device a at 1200 mm, the average blowing force on different areas of the jet cross-section can be measured by using force measuring discs with different areas (radii), and then the The distribution of injection force on the cross-section. It can be found that the more force measuring discs are used and the higher the area (radius) resolution of the measured range is, the closer the injection force distribution obtained from the test is to the real injection force distribution.
最后说明的是,以上优选实施例仅用以说明本实用新型的技术方案而非限制,尽管通过上述优选实施例已经对本实用新型进行了详细的描述,但本领域技术人员应当理解,可以在形式上和细节上对其作出各种各样的改变,而不偏离本实用新型权利要求书所限定的范围。Finally, it is noted that the above preferred embodiments are only used to illustrate the technical solutions of the present utility model without limitation. Although the utility model has been described in detail through the above preferred embodiments, those skilled in the art should understand that it can be described in the form Various changes can be made in the above and in the details without departing from the scope defined by the claims of the present invention.
Claims (5)
- A kind of 1. gas jet characteristic comprehensive measurement device, it is characterised in that:Including gas jet generating means and test data Real-time acquisition system;The test data real-time acquisition system includes gas pipeline pressure real-time acquisition device, gas pipeline stream Measure real-time acquisition device, gas jet injection power real-time acquisition device, acquisition module and computer, the gas jet injection Power real-time acquisition device face gas jet generating means set and can opposing gas jet flow generating apparatus move, the flue The gas passage that road pressure real-time acquisition device, gas pipeline flow real-time acquisition device are arranged on gas jet generating means enters At mouthful, the gas jet injection power real-time acquisition device, gas pipeline pressure real-time acquisition device, gas pipeline flow are real-time Harvester connects computer by acquisition module.
- A kind of 2. gas jet characteristic comprehensive measurement device according to claim 1, it is characterised in that:The gas jet Generating means is arranged on test platform.
- A kind of 3. gas jet characteristic comprehensive measurement device according to claim 1 or 2, it is characterised in that:The gas Jet flow generating apparatus includes passing sequentially through the high-pressure air source of steam line connection, vacuum tank, regulating valve, stop valve, blowing device, The gas jet injection power real-time acquisition device face blowing device sets and can moved relative to blowing device, the flue Road pressure real-time acquisition device, gas pipeline flow real-time acquisition device are arranged at the gas channel inlet of blowing device.
- A kind of 4. gas jet characteristic comprehensive measurement device according to claim 3, it is characterised in that:The gas jet Injection power real-time acquisition device is arranged on immediately below the center line of blowing device shower nozzle.
- A kind of 5. gas jet characteristic comprehensive measurement device according to claim 4, it is characterised in that:The gas jet Being blown power real-time acquisition device includes dynamometry disk, dynamometry disc carrier, force snesor, fixing device, and the dynamometry disk is removably Be arranged on dynamometry disc carrier, by force snesor fix on the securing means, the fixing device it is Height Adjustable.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720704213.1U CN206832296U (en) | 2017-06-16 | 2017-06-16 | A kind of gas jet characteristic comprehensive measurement device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720704213.1U CN206832296U (en) | 2017-06-16 | 2017-06-16 | A kind of gas jet characteristic comprehensive measurement device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206832296U true CN206832296U (en) | 2018-01-02 |
Family
ID=60776254
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720704213.1U Active CN206832296U (en) | 2017-06-16 | 2017-06-16 | A kind of gas jet characteristic comprehensive measurement device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206832296U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107014445A (en) * | 2017-06-16 | 2017-08-04 | 中冶赛迪工程技术股份有限公司 | A kind of gas jet characteristic comprehensive measurement device and method |
CN109974972A (en) * | 2019-04-25 | 2019-07-05 | 扬州大学 | An experimental device for a pulsed jet impinging on a rotating wall for particle image velocimetry and its velocity measurement method |
-
2017
- 2017-06-16 CN CN201720704213.1U patent/CN206832296U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107014445A (en) * | 2017-06-16 | 2017-08-04 | 中冶赛迪工程技术股份有限公司 | A kind of gas jet characteristic comprehensive measurement device and method |
CN109974972A (en) * | 2019-04-25 | 2019-07-05 | 扬州大学 | An experimental device for a pulsed jet impinging on a rotating wall for particle image velocimetry and its velocity measurement method |
CN109974972B (en) * | 2019-04-25 | 2024-03-29 | 扬州大学 | Experimental device for pulse jet impact rotation wall surface for particle image velocimetry and velocimetry method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN107014445A (en) | A kind of gas jet characteristic comprehensive measurement device and method | |
Narayanan et al. | An experimental study of fluid mechanics and heat transfer in an impinging slot jet flow | |
WO2021057860A1 (en) | Experimental device for researching jet fire of natural gas long-distance pipeline based on obstacle placement condition | |
CN107631958A (en) | A kind of small test device for testing super hydrophobic material resistance reducing performance | |
Zanoun | Flow characteristics in low-speed wind tunnel contractions: Simulation and testing | |
CN206832296U (en) | A kind of gas jet characteristic comprehensive measurement device | |
Azzopardi et al. | Detailed measurements of vertical annular two-phase flow—part I: drop velocities and sizes | |
Amini et al. | Measurements of jet flows impinging into a channel containing a rod bundle using dynamic PIV | |
CN110763265B (en) | System and method for testing atomization spraying effect of natural gas drag reducer | |
Bian et al. | Experimental study on spray characteristics of pressure-swirl nozzle in China advanced PWR containment | |
Zaidi et al. | A comparative study of phase Doppler and laser diffraction techniques to investigate drop sizes in annular two-phase flow | |
Berridge et al. | Measurements and computations of second-mode instability waves in several hypersonic wind tunnels | |
CN109856016A (en) | A kind of device and method of the aspherical particle drag coefficient measurement based on gravitational difference | |
Pietrzyk | Experimental study of the interaction of dense jets with a crossflow for gas turbine applications | |
Tezuka et al. | Assessment of effects of pipe surface roughness and pipe elbows on the accuracy of meter factors using the ultrasonic pulse Doppler method | |
CN207439632U (en) | Visualize guide's cobalt target piece cobalt stick Flow vibration experimental provision | |
CN107830979B (en) | Visual pilot cobalt target cobalt rod flow induced vibration experimental device | |
Zhang et al. | The Development of Top-Hat Flow Field in a Circular Symmetrical Subsonic Nozzle | |
CN106644364B (en) | The method that shock wave enhancing Supersonic Gas membrane fluid mixing is measured based on presser sensor paint | |
CN213148017U (en) | System for acquiring flow state of fluid in flowmeter and analysis system | |
Cutler et al. | Analysis of intermittency and probe data in a supersonic flow with injection | |
Behrouzi et al. | Experimental data for CFD validation of the intake ingestion process in STOVL aircraft | |
Stewart | Effects of spacing and geometry of distributed roughness elements on a two-dimensional turbulent boundary layer | |
Liu et al. | Impacts of inflow conditions on the measurement stability of a turbulence-mitigation based liquid concentration detection system | |
Zheng et al. | Measurement of spray droplet velocity and size distribution by a tapered optical fiber probe |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |