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A numerical investigation in buoyancy effects on micro jet diffusion flame 被引量:1
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作者 LIU Lei ZHAO Ming +2 位作者 CHEN Yi-kun FAN Ai-wu LI Dan 《Journal of Central South University》 SCIE EI CAS CSCD 2020年第3期867-875,共9页
The buoyancy effect on micro hydrogen jet flames in still air was numerially studied.The results show that when the jet velocity is relatively large(V≥0.2 m/s),the flame height,width and temperature decrease,whereas ... The buoyancy effect on micro hydrogen jet flames in still air was numerially studied.The results show that when the jet velocity is relatively large(V≥0.2 m/s),the flame height,width and temperature decrease,whereas the peak OH mass fraction increases significantly under normal gravity(g=9.8 m/s^2).For a very low jet velocity(e.g.,V=0.1 m/s),both the peak OH mass fraction and flame temperature under g=9.8 m/s^2 are lower than the counterparts under g=0 m/s^2.Analysis reveals that when V≥0.2 m/s,fuel/air mixing will be promoted and combustion will be intensified due to radial flow caused by the buoyancy effect.However,the flame temperature will be slightly decreased owing to the large amount of entrainment of cold air into the reaction zone.For V=0.1 m/s,since the heat release rate is very low,the entrainment of cold air and fuel leakage from the rim of tube exit lead to a significant drop of flame temperature.Meanwhile,the heat loss rate from fuel to inner tube wall is larger under g=9.8 m/s^2 compared to that under g=0 m/s^2.Therefore,the buoyancy effect is overall negative at very low jet velocities. 展开更多
关键词 micro jet diffusion flame buoyancy effect flame structure flame temperature air entrainment preheating effect
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Microjet flow control in an ultra-compact serpentine inlet 被引量:9
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作者 Da Xingya Fan Zhaolin +3 位作者 Fan Jianchao Zeng Liquan Rui Wei Zhou Run 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2015年第5期1381-1390,共10页
Microjets are used to control the internal flow to improve the performance of an ultra-compact serpentine inlet. A highly offset serpentine inlet with length-to-diameter ratio of 2.5 is designed and static tests are c... Microjets are used to control the internal flow to improve the performance of an ultra-compact serpentine inlet. A highly offset serpentine inlet with length-to-diameter ratio of 2.5 is designed and static tests are conducted to analyze the internal flow characteristics in terms of pressure recovery, distortion and flow separation. Flow separation is encountered in the second S-turn, and two strong counter-rotating vortices are formed at the aerodynamic interthce plane (AIP) face which occupy a quarter of the outlet area and result in severe pressure loss and distortion. A flow control model employing a row of microjets in the second turn is designed based on the internal flow characteristics and simplified CFD simulations. Flow control tests are conducted to verify the control effectiveness and understand the characteristics as a function of inlet throat Mach number, injection mass flow ratio, jet Mach number and momentum coefficient. At all test Mach numbers, microjet flow control (MFC) effectively improves the recovery and reduces the distortion intensity. Between inlet throat Mach number 0.2 and 0.5, the strong flow separation in the second S-turn is suppressed at an optimum jet flow ratio of less than 0.65%, resulting in a maximum improvement of 4% for pressure recovery coefficient and a maximum decrease of 75% for circumferential distortion intensity at cruise. However, in order to suppress the flow separation, the injection rate should retain in an effective range. When the injection rate is higher than this range, the flow is degraded and the distortion contour is changed from 90° circumferential distortion pattern to 180° circumferential distortion pattern. Detailed data analysis shows that this optimum flow ratio depends on inlet throat Mach number and the monlcntunl coefficient affects the control effectiveness in a dual stepping manner. 展开更多
关键词 Active flow control Distortion intensity:micro jet Pressure recovery Serpentine inlet
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Partially-Premixed Combustion Characteristics and Thermal Performance of Micro Jet Array Burners with Different Nozzle Spacings 被引量:1
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作者 YANG Haolin WU Yong +2 位作者 ZENG Xiaojun WANG Xiaohan ZHAO Daiqing 《Journal of Thermal Science》 SCIE EI CAS CSCD 2021年第5期1718-1730,共13页
In order to develop a burner with uniform temperature field,the combustion characteristics and thermal performance of partially premixed methane/air jet flames were experimentally studied by using micro jet array burn... In order to develop a burner with uniform temperature field,the combustion characteristics and thermal performance of partially premixed methane/air jet flames were experimentally studied by using micro jet array burners.The circular tubes of 1.0-mm inner diameter and 1.5-mm outer diameter were used as nozzles.The effects of nozzle spacing and equivalence ratio on flame phenomenology,temperature distribution and pollutant emissions were respectively investigated by camera photography,thermocouple measurement and sampling analysis.Results show that there are two clean flame patterns:clean merged-flame and clean non-merging flames.The flame patterns depend on the strength of flame interaction,the equivalence ratio of the mixture and the quantity of air entrainment through the gap between nozzles.The burners with small nozzle spacing such as 2 mm and 2.5 mm tend to produce fully merged flame with low equivalence ratio limit and the corresponding temperature fields are very uniform with fluctuations less than 0.3%,but a small increase in equivalence ratio will lead to rapid deterioration of combustion property.The burner with a medium spacing of 3 mm can produce partially merged flame in a wide equivalence ratio range with low emissions,and the temperature fluctuation can be less than 0.5%(<7 K)in the optimal region.The burner with a large spacing of 4 mm will basically form independent array flames with the largest temperature fluctuation over 1%,while it can achieve clean combustion under high equivalence ratio due to large air entrainment.Comprehensive analysis shows that the micro jet array burner with medium nozzle spacing of 3 mm has the best combustion characteristics and thermal performance. 展开更多
关键词 micro jet array burner flame interaction methane/air flame temperature fluctuation thermal performance
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Experimental and numerical study on a micro jet cooling solution for high power LEDs 被引量:13
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作者 LUO XiaoBing LIU Sheng +1 位作者 JIANG XiaoPing CHENG Ting 《Science China(Technological Sciences)》 SCIE EI CAS 2007年第4期478-489,共12页
An active cooling solution based on close-looped micro impinging jet is proposed for high power light emitting diodes (LEDs). In this system, a micro pump is utilized to enable the fluid circulation, impinging jet is ... An active cooling solution based on close-looped micro impinging jet is proposed for high power light emitting diodes (LEDs). In this system, a micro pump is utilized to enable the fluid circulation, impinging jet is used for heat exchange between LED chips and the present system. To check the feasibility of the present cooling system, the preliminary experiments are conducted without the intention of parameter optimization on micro jet device and other system components. The experiment results demonstrate that the present cooling system can achieve good cooling effect. For a 16.4 W input power, the surface temperature of 2 by 2 LED array is just 44.2°C after 10 min operation, much lower than 112.2°C, which is measured without any active cooling techniques at the same input power. Experimental results also show that increase in the flow rate of micro pump will greatly enhance the heat transfer efficiency, however, it will increase power consumption. Therefore, it should have a trade-off between the flow rate and the power consumption. To find a suitable numerical model for next step parameter optimization, numerical simulation on the above experiment system is also conducted in this paper. The comparison between numerical and experiment results is presented. For two by two chip array, when the input power is 4 W, the surface average temperature achieved by a steady numerical simulation is 34°C, which is close to the value of 32.8°C obtained by surface experiment test. The simulation results also demonstrate that the micro jet device in the present cooling system needs parameter optimization. 展开更多
关键词 high power LEDS CLOSED system micro IMPINGING jets thermal management
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A review on the erosion mechanisms in abrasive waterjet micromachining of brittle materials 被引量:3
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作者 T Nguyen J Wang 《International Journal of Extreme Manufacturing》 2019年第1期111-124,共14页
The fabrication of miniature structures on components with high-integrity surface quality represents one of the cutting edge technologies in the 21st century.The materials used to construct such small structures are o... The fabrication of miniature structures on components with high-integrity surface quality represents one of the cutting edge technologies in the 21st century.The materials used to construct such small structures are often difficult-to-machine.Many other readily available technologies either cannot realise necessary precision or are costly.Abrasive waterjet(AWJ)is a favourable technology for the machining of difficult-to-machine materials.However,this technology is generally aimed at large stock removal.A reduction in the scale of this technology is an attractive avenue for meeting the pressing need of industry in the production of damage-free micro features.This paper reviews some of the work that has been undertaken at UNSW Sydney about the development of such an AWJ technology,focusing on the system design currently employed to generate a micro abrasive jet,the erosion mechanisms associated with processing some typical brittle materials of both single-and two-phased.Processing models based on the findings are also presented.The review concludes on the viability of the technology and the prevailing trend in its development. 展开更多
关键词 micro abrasive jet abrasive waterjet ductile erosion viscous flow difficult to machine materials
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Efect of Micro Abrasive Slurry Jet Polishing on Properties of Coated Cemented Carbide Tools
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作者 Rongjuan Wang Chengyong Wang 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2023年第5期109-119,共11页
Owing to the popularization of coating technology, physical Vapor Deposition (PVD) coated tools have become indispensable in the cutting process. Additionally, the post-treatment of coated tools applied to industrial ... Owing to the popularization of coating technology, physical Vapor Deposition (PVD) coated tools have become indispensable in the cutting process. Additionally, the post-treatment of coated tools applied to industrial production can efectively enhance the surface quality of coating. To improve the processing performance of coated tools, micro abrasive slurry jet (MASJ) polishing technology is frst applied to the post-treatment of coated tools. Subsequently, the efects of process parameters on the surface quality and cutting thickness of coating are investigated via single-factor experiments. In the experiment, the best surface roughness is obtained by setting the working pressure to 0.4 MPa, particle size to 3 μm, incidence angle to 30°, and abrasive mass concentration to 100 g/L. Based on the results of the single-factor experiments, combination experiments are designed, and three types of coated tools with diferent surface qualities and coating thicknesses are obtained. The MASJ process for the post-treatment of coated tools is investigated based on a tool wear experiment and the efects of cutting parameters on the cutting force and workpiece surface quality of three types of cutting tools. The result indicates that MASJ machining can efectively improve the machining performance of coated tools. 展开更多
关键词 micro abrasive slurry jet POST-TREATMENT Coated tools Turning Surface roughness
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A Voice Coil Powered Controllable Micro-Jet Injection System
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作者 Kai Chen Laiwu Miao Zhigang Feng 《Journal of Biomedical Science and Engineering》 2015年第9期632-642,共11页
A medical device of micro-jet injection for drug delivery is described in this paper. The device is powered by a Lorentz force driver (or voice coil motor, VCM) and is able to perform pulsed injection through controll... A medical device of micro-jet injection for drug delivery is described in this paper. The device is powered by a Lorentz force driver (or voice coil motor, VCM) and is able to perform pulsed injection through controlling the direction of the current passing through the device. The driving force and the resulting injection pressure are also controllable through control of the current intensity of the VCM. A physical model was established by combining the existing jet injection model with the relationship of the driving force obtained from a finite-element-method (FEM) analysis, and was verified by experimental measurements. The numerical calculation of the physical model reveals the relationship between the injection pressure and the current intensity of VCM under system conditions. In normal cases, the injection dose can be varied. Thus the relationship between the current intensity of VCM and the dose value was numerically obtained under the condition for the maximum injection pressure to be above a threshold value. These results can be used for optimization of the device. 展开更多
关键词 jet INJECTION micro-jet Trans-Dermal DRUG Delivery
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3种根管封闭剂根尖封闭性能的Micro-CT研究 被引量:2
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作者 赵麒桐 王艳茹 +3 位作者 张敏 张琪 李谨 雷港 《口腔医学》 CAS 2024年第6期443-447,共5页
目的使用微计算机断层扫描技术(micro-computed tomography,Micro-CT)分析比较3种根管封闭剂(C-Root SP、iRoot SP和AH-Plus Jet)在单尖法根管充填中对根管充填封闭性能。方法收集90颗符合纳入标准的下颌单根管离体前磨牙,使用ProTaper ... 目的使用微计算机断层扫描技术(micro-computed tomography,Micro-CT)分析比较3种根管封闭剂(C-Root SP、iRoot SP和AH-Plus Jet)在单尖法根管充填中对根管充填封闭性能。方法收集90颗符合纳入标准的下颌单根管离体前磨牙,使用ProTaper Next预备至X3,然后随机分为3个实验组C-Root SP组(A组)、iRoot SP组(B组)、AH-Plus Jet组(C组),均采用单尖法进行根管充填,并进行1周的口腔环境模拟,最后用Micro-CT测量根管内气泡体积及其所占比例来评价比较3种根管封闭剂的封闭性能。结果A、B、C组在根管的不同部位(下1/3段、中1/3段、上1/3段)均存在可识别的气泡。在下1/3段中,A组的气泡体积(0.01±0.01)mm3与C组(0.12±0.08)mm^(3)相比存在统计学差异(P<0.05),与B组(0.02±0.01)mm^(3)相比则没有统计学差异;在中1/3段与上1/3段,组间无统计学差异。在根管全长范围内,A组的气泡总体积最小(0.15±0.03)mm^(3),B、C两组分别为(0.22±0.11)mm^(3)、(0.34±0.28)mm^(3),A组与B组相似,均优于C组。结论C-Root SP的根尖封闭性能与iRoot SP接近,且优于AH-Plus Jet,C-Root SP可以作为良好的根管封闭剂选择。 展开更多
关键词 C-Root SP iRoot SP AH-Plus jet micro-CT 根管封闭剂
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The Enhanced Measurements of Laser Micro-jet Processing
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作者 Xizhao Lu Haihe Xie +1 位作者 Chun Lin Yuanqing Huang 《Journal of Modern Physics》 2011年第3期109-112,共4页
In the paper, the enhanced measurements of the laser micro-jet processing are discussed. In fact, within pure water breakdown threshold of laser, the less focal which focused with the appropriate focusing lens and the... In the paper, the enhanced measurements of the laser micro-jet processing are discussed. In fact, within pure water breakdown threshold of laser, the less focal which focused with the appropriate focusing lens and the small nozzle of water chamber enhance the laser power density ,at the same time, the laser beam transport in the wave guided water with the proper total reflection angle. The laser power which depended on the properties of the diameter, the coupling water chamber and the coupling efficiency of the micro-jet and laser beam expect of the properties of laser. 展开更多
关键词 Focusing Lens FOCAL Spot Size Nozzle of Water CHAMBER LASER micro-jet Flat-Topped BREAKDOWN Threshold
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Rapid manufacturing of SiC molds with micro-sized holes using abrasive water jet 被引量:1
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作者 Bo-Sung SHIN Kang-Su PARK +5 位作者 Yeon-Kyoung BAHK Sun-Ki PARK Jung-Han LEE Jeung-Sang GO Myung-Chang KANG Chae-Moon LEE 《中国有色金属学会会刊:英文版》 CSCD 2009年第B09期178-182,共5页
Silicon carbide (SiC) is highly wear resistant with good mechanical properties, including high temperature strength, excellent chemical resistance, and high thermal conductivity and thermal shock resistance. SiC molds... Silicon carbide (SiC) is highly wear resistant with good mechanical properties, including high temperature strength, excellent chemical resistance, and high thermal conductivity and thermal shock resistance. SiC molds, which can be produced with diverse microstructural features, are now widely used in glass molding owing to their excellent characteristics, and also have potential applicability in IT industries. SiC molds are traditionally fabricated by silicon micromachining or dicing. The fabrication cost of silicon micromachining is very high, however, because several expensive masks are needed. Furthermore, the fabrication time is very long. Meanwhile, it is difficult to make micro-patterned molds with arbitrary shapes using dicing saws. Abrasive water jet (AWJ) is widely applied to cut and drill very brittle, soft and fibrous materials. It offers high energy density, the absence of a heat affected zone(HAZ), high performance, and an environment friendly process. In spite of these advantages, micro-hole drilling via conventional AWJ processing suffers from notable shortcomings. We proposed a new abrasive supplying method of AWJ. The proposed method reduces frosting phenomena, and provides micro-machining of AWJ. The characteristics of a hole machined was investigated by the proposed AWJ process according to the ratio of water and abrasives. With the optimal experimental conditions, 3×3 array SiC molds with the diameter of 700 μm and depth of 900 μm were successfully manufactured. 展开更多
关键词 快速模具制造 磨料水射流 碳化硅 微型 硅微加工 型孔 最佳实验条件 机械性能
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基于微多普勒信号的无人机回波检测技术研究
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作者 闫军 顾村锋 +1 位作者 孔德永 龚江昆 《空天防御》 2025年第1期10-16,23,共8页
近年来,随着无人机的广泛应用,反无人机雷达技术得到了迅猛发展。然而,由于常见无人机具有体积小、雷达散射面积(RCS)有限、运动速度较慢等特点,其雷达回波往往被强烈的背景杂波淹没。传统的基于回波信噪比(SNR)的检测方法存在漏警率高... 近年来,随着无人机的广泛应用,反无人机雷达技术得到了迅猛发展。然而,由于常见无人机具有体积小、雷达散射面积(RCS)有限、运动速度较慢等特点,其雷达回波往往被强烈的背景杂波淹没。传统的基于回波信噪比(SNR)的检测方法存在漏警率高和探测距离短的问题。为此,本文提出了一种创新的检测方法:通过分析无人机旋翼产生的微多普勒信号,即旋翼调制(JEM)效应对应的微多普勒信号,设计了基于回波信杂比(SCR)的检测技术,以实现对目标回波的相对检测。通过微波暗室和雷达外场实验,发现四旋翼无人机和垂直起降无人机在多个雷达测试波段均显著产生微多普勒信号。对比实验结果表明,在海杂波环境下,SCR检测相较于SNR检测具有更好的稳定性、更高的检测效率以及更低的漏警率。 展开更多
关键词 反无人机雷达 无人机探测 漏警率 微多普勒 旋翼调制 信杂比
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前混合水射流组合喷丸的机理与试验研究
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作者 马泳涛 张越江 +3 位作者 刘兰荣 李春凡 孙万顺 孙宝成 《表面技术》 北大核心 2025年第9期225-238,共14页
目的对18CrNiMo7-6渗碳钢进行不同丸粒条件下的混合射流喷丸研究。方法基于Hertz理论分析,构建一次喷丸工艺的残余应力场解析预测模型,并进行试验验证,在此基础上获取达到残余应力场近饱和的喷丸试验参数;选择不同的丸粒类型、压力等试... 目的对18CrNiMo7-6渗碳钢进行不同丸粒条件下的混合射流喷丸研究。方法基于Hertz理论分析,构建一次喷丸工艺的残余应力场解析预测模型,并进行试验验证,在此基础上获取达到残余应力场近饱和的喷丸试验参数;选择不同的丸粒类型、压力等试验参数来探究二次微细喷丸处理渗碳钢对其残余应力、表面质量的影响规律。结果在一次喷丸(First-shot peening)处理获得饱和残余应力场的条件下,采用ϕ0.1 mm的铸钢丸和ϕ0.05 mm的强化钢丸/玻璃丸进行二次喷丸(Secondary-shot peening)时,随着喷丸强度的提高,铸钢丸喷丸处理出现了过喷,并发生残余应力消退(消残)现象,在最高强度下残余应力最大值所在深度降低了约50μm,总影响深度降低了约120μm,表面粗糙度Ra随之增大,由0.78μm升至1.78μm;微细强化钢丸未对已有残余应力场造成过大的影响,表面粗糙度先减小后增大,最低为0.81μm;微细玻璃丸对试样的残余应力场、表面粗糙度的影响不大。铸钢丸在压力2 MPa、喷嘴移速16 mm/s,或微细强化钢丸在6 MPa、4 mm/s时,其喷丸效果更好。结论二次喷丸工艺中,在适宜的喷丸强度下使用微细丸粒不仅能增强原有的残余应力场,还可以显著提高一次喷丸处理后的表面质量。 展开更多
关键词 前混合水射流 二次喷丸 微细喷丸 粗糙度 残余应力 饱和残余应力场
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界面邻近效应对激波诱导重气柱演化的影响
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作者 杨欢欢 张恩来 +1 位作者 李欣竹 邹立勇 《高压物理学报》 北大核心 2025年第5期1-13,共13页
针对实际应用中激波与物质近表面杂质及孔洞等相互作用中的界面邻近效应,通过数值模拟开展了下游平面重-轻界面对激波诱导重气柱演化影响的简化机理研究。结果表明,激波冲击气柱形成的衍射和透射波系依次冲击下游界面,在气柱与下游界面... 针对实际应用中激波与物质近表面杂质及孔洞等相互作用中的界面邻近效应,通过数值模拟开展了下游平面重-轻界面对激波诱导重气柱演化影响的简化机理研究。结果表明,激波冲击气柱形成的衍射和透射波系依次冲击下游界面,在气柱与下游界面之间形成来回反射的波系结构,这些波系不仅影响气柱的界面演化,而且在下游界面诱导产生射流。在不同的界面间距条件下,气柱外部衍射波系在下游界面的反射波系不同,这些反射波系及气柱内部聚焦波系冲击气柱右极点的先后顺序也存在差异。当界面间距较小时,气柱射流可以穿透气柱与下游界面之间的间隙流体,并与下游界面射流耦合,显著促进气柱射流的演化。随着界面间距的增大,射流耦合现象逐渐减弱,重气柱演化涡对抑制了气柱射流的发展。当界面间距进一步增大时,气柱射流又会因下游界面反射稀疏波系的拉伸作用而被促进。此外,在不同的界面间距条件下,下游界面的存在均对气柱界面宽度、高度的发展及环量沉积起到促进作用。 展开更多
关键词 激波 RICHTMYER-MESHKOV不稳定性 气柱 射流 微喷射 环量
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推进剂微射流冷却对高温非平衡气动热的影响机理
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作者 邢旭雯 杨肖峰 +1 位作者 刘磊 杜雁霞 《空气动力学学报》 北大核心 2025年第4期20-29,I0001,共11页
飞行器在高速飞行时,可利用自身携带的推进剂通过微孔射流实现冷却,达到主动热防护效果。但在高温非平衡流条件下,可压缩外流与微射流交汇、射流排挤/掺混/反应多过程交织,微射流冷却主导性机制和影响因素复杂。本文建立了微射流黏性壁... 飞行器在高速飞行时,可利用自身携带的推进剂通过微孔射流实现冷却,达到主动热防护效果。但在高温非平衡流条件下,可压缩外流与微射流交汇、射流排挤/掺混/反应多过程交织,微射流冷却主导性机制和影响因素复杂。本文建立了微射流黏性壁面边界模型,开展了微射流作用下高温非平衡流场数值模拟,探讨了射流孔径、速度和孔间距对冷却效果的影响规律,发现高温非平衡流条件下推进剂微射流冷却由边界层排挤、多相催化弱化两个基本过程主导:(1)低温微射流喷出对边界层产生排挤作用,改变边界层剖面形态,降低紧邻壁面处的温度法向梯度,从而降低壁面法向导热,实现冷却;(2)低温氧分子工质微射流排挤近壁氧原子,弱化氧催化效应,导致催化热降低。参数化研究结果表明:质量流量不变,增大射流孔大小,降热率与冷却范围均下降;射流孔面积不变,增大微射流速度,降热率与冷却范围增大;质量流量不变,减小孔间距,展向平均降热率峰值减小,但孔下游冷却范围增大,呈现较均匀的冷却效果。以上研究可对未来微射流冷却主动热防护的设计与优化提供重要的理论支撑和技术参考。 展开更多
关键词 微射流冷却 非平衡流动 气动热 壁面催化 数值模拟
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壁面微缺陷影响下的介观尺度冲击射流流场特性
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作者 洪睿 胡建军 +3 位作者 肖洋 金瑶兰 姚静 孔祥东 《中国机械工程》 北大核心 2025年第10期2215-2223,2231,共10页
为研究射流管阀喷嘴-接受器前置级长期服役后,冲蚀磨损及气穴气蚀现象造成的微缺陷对流场流动规律和流体能量转换特性的影响,利用显微粒子图像测速技术对原始介观尺度近距离射流冲击微缺陷靶板时方腔内的流动结构和涡旋分布进行直接试... 为研究射流管阀喷嘴-接受器前置级长期服役后,冲蚀磨损及气穴气蚀现象造成的微缺陷对流场流动规律和流体能量转换特性的影响,利用显微粒子图像测速技术对原始介观尺度近距离射流冲击微缺陷靶板时方腔内的流动结构和涡旋分布进行直接试验观测,探究了微缺陷大小、形状与位置对涡旋形态及其演化规律的影响,揭示了方腔内涡核分裂与归一现象背后蕴含的机理。研究结果表明:壁面微缺陷的存在直接影响壁面射流能量的传递与耗散,导致射流间隙和方腔内的涡旋结构和能量分布与无缺陷时显著不同;随着微凹坑尺寸的增大,两侧方腔内类圆形涡旋对呈现出逐渐分裂并远离底部壁面的趋势;而随着微凸起尺寸的增大,两侧方腔内类茧形涡旋对呈现出逐渐归一并靠近底部表面的演化规律。 展开更多
关键词 射流管伺服阀 介观尺度 冲击射流 微缺陷 显微粒子图像测速(micro-PIV)
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基于FreeRTOS的微喷射3D打印机控制系统设计及稳定性验证
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作者 常佳俊 赵巍 叶春生 《新技术新工艺》 2025年第3期24-30,共7页
鉴于微喷射3D打印机控制系统的二次开发难度大和可移植性弱等问题,设计了一款以STM32F103VET6芯片为核心,采用赛尔(XAAR)喷头,基于FreeRTOS实时操作系统的微喷射3D打印控制系统。并结合XAAR喷头通讯逻辑、三轴步进电机控制和打印定位精... 鉴于微喷射3D打印机控制系统的二次开发难度大和可移植性弱等问题,设计了一款以STM32F103VET6芯片为核心,采用赛尔(XAAR)喷头,基于FreeRTOS实时操作系统的微喷射3D打印控制系统。并结合XAAR喷头通讯逻辑、三轴步进电机控制和打印定位精度等要素,设计了硬件电路与控制系统软件。对纯Al_(2)O_(3)、Al_(2)O_(3)掺杂0~6wt%Y_(2)O_(3)和Al_(2)O_(3)掺杂0~4wt%SiO_(2)这3种类型粉末进行了打印测试,结果表明,对应组分试样3个成形轴的打印尺寸偏差值均小于0.3 mm,说明FreeRTOS实时操作系统在控制打印驱动方面表现出良好的稳定性和准确性。此外,适量Y_(2)O_(3)和SiO_(2)的掺杂可以起到填充Al_(2)O_(3)孔隙的作用,从而改善生坯试样的相对密度和孔隙率,但过量时易引起粉末流动性下降而导致性能降低。 展开更多
关键词 STM32 微喷射3D打印 FREERTOS Al_(2)O_(3)陶瓷 材料成形 尺寸精度 孔隙率
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超声辅助磨料水射流微晶玻璃微孔加工试验装置设计
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作者 孙浩程 侯荣国 +2 位作者 吕哲 云昊 徐景沛 《机床与液压》 北大核心 2025年第15期86-90,共5页
微晶玻璃微孔加工时,存在微孔表面质量不理想与加工效率低的问题。基于磨料水射流加工技术,设计超声辅助磨料水射流微晶玻璃微孔加工试验装置。该装置通过使用双气液增压泵和蓄能器,提高了射流压力,稳定了射流流量,最终改善了加工后的... 微晶玻璃微孔加工时,存在微孔表面质量不理想与加工效率低的问题。基于磨料水射流加工技术,设计超声辅助磨料水射流微晶玻璃微孔加工试验装置。该装置通过使用双气液增压泵和蓄能器,提高了射流压力,稳定了射流流量,最终改善了加工后的工件表面质量。在工件表面法向方向上施加超声振动,提高微孔加工效率。试验结果表明:磨料目数为800目、射流压力为15 MPa时,相比于未施加超声振动,孔壁锥度由35°降低至18°,降低了48%,孔深度由91.5μm提高至119.2μm,提高了30.3%;微孔加工时,施加超声振动后的材料去除率有10%左右的提升。超声辅助磨料水射流有效改善了微晶玻璃表面加工质量,提高了加工效率,为微晶玻璃精密加工提供了新型加工技术。 展开更多
关键词 微晶玻璃 磨料水射流 超声振动 微孔加工装置
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采用DC Arc Plasma JetCVD方法沉积微/纳米复合自支撑金刚石膜 被引量:3
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作者 戴风伟 陈广超 +7 位作者 兰昊 J.Askari 宋建华 李成明 佟玉梅 李彬 黑立富 吕反修 《人工晶体学报》 EI CAS CSCD 北大核心 2006年第6期1200-1202,1208,共4页
在30kW级直流电弧等离子体喷射化学气相沉积(DC Arc P lasm a Jet CVD)设备上,采用Ar-H2-CH4混合气体,通过调节甲烷浓度以及控制其他沉积参数,在Mo衬底上沉积出微/纳米复合自支撑金刚石膜。实验表明,当微米金刚石膜层沉积结束后,在随后... 在30kW级直流电弧等离子体喷射化学气相沉积(DC Arc P lasm a Jet CVD)设备上,采用Ar-H2-CH4混合气体,通过调节甲烷浓度以及控制其他沉积参数,在Mo衬底上沉积出微/纳米复合自支撑金刚石膜。实验表明,当微米金刚石膜层沉积结束后,在随后的沉积中,随着甲烷浓度的增加,金刚石膜表面的晶粒大小是逐渐减小的。当甲烷浓度达到20%以上时,金刚石膜生长面晶粒呈现菜花状的小晶团,膜体侧面已经没有了粗大的柱状晶,而是呈现出光滑的断口,对该层进行拉曼谱分析显示,位于1145 cm-1附近有一定强度的散射峰出现。这说明所沉积的晶粒全部变为纳米级尺寸。 展开更多
关键词 直流电弧等离子体喷射化学气相沉积 微/纳米复合自支撑金刚石膜 二次形核 拉曼光谱
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基于射流脉冲的微喷带喷洒性能
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作者 武文婧 王新坤 +2 位作者 赵擎 贾宗瑾 杨凡 《排灌机械工程学报》 北大核心 2025年第10期1072-1080,共9页
为解决微喷带灌水均匀度低于一般喷灌设备等问题,文中设计了一种适用于微喷带的脉冲三通,旨在提高其灌水均匀性及用水效率.以3种管径分别为Φ28,Φ32和Φ40的微喷带流量压力关系为基础,确定脉冲三通结构参数的取值范围,设计32组正交试... 为解决微喷带灌水均匀度低于一般喷灌设备等问题,文中设计了一种适用于微喷带的脉冲三通,旨在提高其灌水均匀性及用水效率.以3种管径分别为Φ28,Φ32和Φ40的微喷带流量压力关系为基础,确定脉冲三通结构参数的取值范围,设计32组正交试验进行计算流体力学(computational fluid dynamics,CFD)数值模拟,确定最优脉冲三通结构参数.基于最优脉冲三通样机进行脉冲性能试验,压力损失、脉冲振幅和脉冲频率3项参数的试验结果与CFD数值模拟结果偏差小于10%,证明最优脉冲三通在实际应用中的可靠性及CFD数值模拟在脉冲三通选择过程中的可行性.进行微喷带单条和组合脉冲喷洒性能试验,并设置普通三通对照组,以准确评估脉冲三通对微喷带喷洒性能的影响.在20~40 kPa压力下,相较于普通三通微喷带,脉冲三通微喷带流量降低0.004~0.011 m^(3)/h,湿润宽度增加0~0.25 m,列平均喷洒强度峰值降低8.6%~18.8%,灌水均匀性变化幅度为-0.50%~11.10%.40 kPa压力下,3种管径的微喷带组合脉冲喷洒试验结果显示,脉冲微喷带的组合喷洒强度峰值降低,灌水均匀性提高8.40%~10.20%,说明脉冲三通能有效改善微喷带的喷洒效率,从而提高灌水质量. 展开更多
关键词 微喷带 脉冲三通 计算流体力学 正交试验 喷洒性能
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亚声速斜冲击喷流噪声控制技术试验研究
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作者 陈保 李伟鹏 +1 位作者 吴飞 羌晓青 《航空动力学报》 北大核心 2025年第6期412-421,共10页
舰载机起飞过程中,发动机喷流冲击偏流板产生高强度噪声,危害了甲板人员听觉健康和设备结构安全。通过施加锯齿喷口和微结构冲击板,在亚声速喷流斜冲击试验条件下,研究了两种降噪措施对冲击喷流噪声的控制作用,分析了锯齿齿数、内切角... 舰载机起飞过程中,发动机喷流冲击偏流板产生高强度噪声,危害了甲板人员听觉健康和设备结构安全。通过施加锯齿喷口和微结构冲击板,在亚声速喷流斜冲击试验条件下,研究了两种降噪措施对冲击喷流噪声的控制作用,分析了锯齿齿数、内切角和齿长对冲击喷流噪声特性的影响规律,探索研究了三角顺流沟槽、金字塔凸起、内嵌圆孔、三角横流沟槽这4种微结构冲击板对冲击喷流噪声指向性及强度的影响,考察了锯齿喷口与微结构冲击板之间的降噪叠加效应。研究结果表明:锯齿喷口有效地抑制了冲击喷流噪声,增大内切角可以提高降噪水平;微结构冲击板可以降低低频段噪声,其中三角横流沟槽板具有最好的抑制效果,在下游的总声压级最大降噪量达3.68 dB;组合降噪方案对下游噪声控制显著,且呈现出一定的非线性叠加机制。研究结论对于抑制舰载机冲击喷流噪声具有工程指导价值。 展开更多
关键词 冲击喷流噪声 亚声速喷流 锯齿喷口 微结构冲击板 噪声控制
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