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Analysis of Leakage Effects on Outlet Flow Characteristics of a Two-dimensional Piston Pump
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作者 Yu Huang Hanyu Xu +2 位作者 Wei Shao Chuan Ding Li Liu 《Chinese Journal of Mechanical Engineering》 2025年第3期545-557,共13页
Owing to their rolling friction,two-dimensional piston pumps are highly suitable as power components for electro-hydrostatic actuators(EHAs).These pumps are particularly advantageous for applications requiring high ef... Owing to their rolling friction,two-dimensional piston pumps are highly suitable as power components for electro-hydrostatic actuators(EHAs).These pumps are particularly advantageous for applications requiring high efficiency and reliability.However,the ambiguity surrounding the output flow characteristics of individual two-dimensional pumps poses a significant challenge in achieving precise closed-loop control of the EHA positions.To address this issue,this study established a comprehensive numerical model that included gap leakage to analyze the impact of leakage on the output flow characteristics of a two-dimensional piston pump.The validity of the numerical analysis was indirectly confirmed through meticulous measurements of the leakage and volumetric efficiency,ensuring robust results.The research findings indicated that,at lower pump speeds,leakage significantly affected the output flow rate,leading to potential inefficiencies in the system.Conversely,at higher rotational speeds,the impact of leakage was less pronounced,implying that the influence of leakage on the pump outlet flow must be carefully considered and managed for EHAs to perform position servo control.Additionally,the research demonstrates that two-dimensional motion does not have a unique or additional effect on pump leakage,thus simplifying the design considerations.Finally,the study concluded that maintaining an oil-filled leakage environment is beneficial because it helps reduce the impact of leakage and enhances the overall volumetric efficiency of the pump system. 展开更多
关键词 Two-dimensional piston pump LEAKAGE Numerical simulation CLEARANCE
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Multipoint Infrared Telemetry System for Measuring the Piston Temperature in Internal Combustion Engines 被引量:5
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作者 刘金祥 魏春源 +1 位作者 张卫正 郭良平 《Journal of Beijing Institute of Technology》 EI CAS 2002年第4期346-349,共4页
A high precision, high antijamming multipoint infrared telemetry system was developed to measure the piston temperature in internal combustion engine. The temperature at the measuring point is converted into correspon... A high precision, high antijamming multipoint infrared telemetry system was developed to measure the piston temperature in internal combustion engine. The temperature at the measuring point is converted into corresponding voltage signal by the thermo-couple first. Then after the V/F stage, the voltage signal is converted into the frequency signal to drive the infrared light-emitting diode to transmit infrared pulses. At the receiver end, a photosensitive audion receives the infrared pulses. After conversion, the voltage recorded by the receiver stands for the magnitude of temperature at the measuring point. Test results of the system indicate that the system is practical and the system can perform multipoint looping temperature measurements for the piston. 展开更多
关键词 piston temperature measurement infrared telemetry
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基于多CNN的分块镜piston和tip-tilt误差同步检测方法研究 被引量:2
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作者 李响 赵伟瑞 《仪器仪表学报》 EI CAS CSCD 北大核心 2024年第3期188-197,共10页
绝大多数大型望远镜采用分块镜的设计方案,为了获得优质的成像效果,需要控制分块望远镜系统的piston和tip-tilt误差。神经网络误差检测方法相较于传统的检测方法具有一定优势,但存在仅检测单一类型误差的局限性。本文提出一种基于卷积... 绝大多数大型望远镜采用分块镜的设计方案,为了获得优质的成像效果,需要控制分块望远镜系统的piston和tip-tilt误差。神经网络误差检测方法相较于传统的检测方法具有一定优势,但存在仅检测单一类型误差的局限性。本文提出一种基于卷积神经网络的piston和tip-tilt误差同步检测方法,通过在出瞳面设置具有离散孔的光阑,引发分段镜反射的子波发生干涉-衍射现象,构建包含丰富piston和tip-tilt误差信息的数据集。通过粗测网络和精测网络级联,满足大范围和高精度同步检测的需求。结果表明,该方法实现了对输入光源相干长度内纳米级的piston误差检测,并对10μrad范围内的tip-tilt误差实现了亚微弧度检测;对40 dB的CCD噪声表现出良好的抗干扰性,对面形误差的允差为0.05λ0RMS(λ0=600 nm),同时对六子镜系统具有可扩展性。本文方法光路简单,操作便利,具有实际意义。 展开更多
关键词 piston误差 tip-tilt误差 分块镜 卷积神经网络
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Transient simulation of a differential piston warm gas self-pressurization system for liquid attitude and divert propulsion system 被引量:1
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作者 Zhongjian FANG Guozhu LIANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2018年第4期698-709,共12页
In order to obtain the dynamic characteristics of a differential piston warm gas selfpressurization system for liquid attitude and divert propulsion system, a transient model is developed using the modular modeling me... In order to obtain the dynamic characteristics of a differential piston warm gas selfpressurization system for liquid attitude and divert propulsion system, a transient model is developed using the modular modeling method. The system includes the solid start cartridge,pressure-amplified tank with liquid monopropellant, liquid regulator, gas generator, and pipes.The one-dimensional finite-element state-variable model is applied to the pipes and the lumped parameter method is adopted for the other modules. The variations of the system operation parameters over time during the startup, steady-state, and pulsing operational processes are obtained from the transient model, and the characteristics of starting time changing with different system parameters are also analyzed. It is shown that the system startup process can be divided into three distinct processes. The starting time monotonically changes with variations of the liquid regulator parameters, first decreasing and then increasing with the mass change of the solid propellant charge of the start cartridge, initial gas cavity volume of the pressure amplified tank and initial gas cushion of the propellant tank. The starting time can be reduced to less than 1.0 s(0.68–0.75 s for the current system). For meeting the deviation requirements of ±10% of the steady-state propellant tank pressure, the positive deviation requirement is assured by the self-locking pressure and the negative deviation can be assured within an allowable maximum propellant tank volume flowrate(1.6 times the design value for the proposed system) for downstream thrusters for a designed system. The results from the simulation are useful as a guide for further system design and testing. 展开更多
关键词 Differential piston Dynamic characteristics Dynamic models Liquid attitude and divert propulsion system Startup process Warm gas self-pressurization system
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RESEARCH ON THE ON-LINE MEASURING SYSTEM FOR THE MIDDLE-CONVEX AND VARYING ELLIPSE PISTON SKIRT 被引量:1
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作者 Wang Xiankui,Jiang Simin,Qian Lei,Shi Zhongdong,Wu Dan (Department of the Precision Instrument and Mechanics,Qinghua University) 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2001年第4期305-309,共5页
The middle convex and varying ellipse piston is th e key component of an internal combustion engine In general,the piston is mac hined by non circular section CNC lathe,but the measuring of piston profile is man... The middle convex and varying ellipse piston is th e key component of an internal combustion engine In general,the piston is mac hined by non circular section CNC lathe,but the measuring of piston profile is manipulated by off line Because the off line measuring reference is differen t from the machining reference,the measurement result is diverse from the act ual dimension A new method to measure the middle convex and varying ellipse p iston profile, which is known as on line measuring, is presented By using thi s kind of method,the high measurement accuracy can be gained,as well as meeting the production requirement. 展开更多
关键词 Middle-convex and varying ellipse piston On -line measure Non circular section
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Technologies and studies of gas exchange in two-stroke aircraft piston engine:A review 被引量:4
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作者 Yu ZHOU Xueyu LI +6 位作者 Shuiting DING Shuai ZHAO Kun ZHU Longtao SHAO Farong DU Gerui WANG Zheng XU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第1期24-50,共27页
The in-cylinder gas exchange process is crucial to the power performance of two-stroke aircraft piston engines,which is easily influenced by complex factors such as high-altitude performance variation and in-cylinder ... The in-cylinder gas exchange process is crucial to the power performance of two-stroke aircraft piston engines,which is easily influenced by complex factors such as high-altitude performance variation and in-cylinder flow characteristics.This paper reviews the development history and characteristics of gas exchange types,as well as the current state of theory and the validation methods of gas exchange technology,while also discusses the trends of cutting-edge technologies in the field.This paper provides a theoretical foundation for the optimization and engineering design of gas exchange systems and,more importantly,points out that the innovation of gas exchange types,the modification of theoretical models,and the technology of variable airflow organization are the key future research directions in this field. 展开更多
关键词 Aircraft piston engine Aircraft power systems Gas exchange High-altitude performance In-cylinder flow TWO-STROKE Unmanned Aerial Vehicles(UAVs)
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Effect of ultrasonic and mechanical vibration treatments on evolution of Mn-rich phases and mechanical properties of Al−12Si−4Cu−1Ni−1Mg−2Mn piston alloys 被引量:1
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作者 Bo LIN Xiang-xiang HE +3 位作者 Song-chao XIA Hua-qiang XIAO Yu-liang ZHAO Khashayar KHANLARI 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2024年第8期2393-2414,共22页
Effects of ultrasonic vibration(UV)and mechanical vibration(MV)on the Mn-rich phase modification and mechanical properties of Al−12Si−4Cu−1Ni−1Mg−2Mn piston alloys were investigated.The results show that the UV and UV... Effects of ultrasonic vibration(UV)and mechanical vibration(MV)on the Mn-rich phase modification and mechanical properties of Al−12Si−4Cu−1Ni−1Mg−2Mn piston alloys were investigated.The results show that the UV and UV+MV treatments can significantly refine and fragmentize the microstructures.In addition,UV treatment can significantly passivate the primary Mn-rich Al15Mn3Si2 intermetallics.The formation mechanisms of refinement and passivation of the grains and non-dendrite particles were discussed.Compared with the gravity die-cast alloys,the UV and UV+MV treated alloys exhibit improved tensile and creep resistance at room and elevated temperatures.These results can be attributed to the refinement of theα(Al)grains and the secondary intermetallics,the increased proportion of refined heat-resistant precipitates,and the formation of nano-sized Si particles.The ultimate tensile strength of the UV treated alloys at 350℃ exceeds that of commercial piston alloys.This indicates the high application potential of the developed piston alloys in density diesel engines. 展开更多
关键词 Al−Si piston alloys Mn-rich phases mechanical properties ultrasonic vibration mechanical vibration
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Mixing characteristics of three-cylinder valve-controlled energy recovery device based on liquid piston
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作者 Zheng Sun Zean Chen +2 位作者 Weian Li Yue Wang Jing Yang 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2024年第10期83-91,共9页
The isobaric energy recovery device can significantly reduce the energy consumption of the seawater reverse osmosis system by recycling the residual pressure energy of high-pressure concentrated brine.Three-cylinder v... The isobaric energy recovery device can significantly reduce the energy consumption of the seawater reverse osmosis system by recycling the residual pressure energy of high-pressure concentrated brine.Three-cylinder valve-controlled energy recovery device(TC-ERD)solves the fluid pulsation of traditional two-cylinder devices,but the use of a“liquid piston”exacerbates the mixing between brine and seawater.Herein,the evolutionary law of“liquid piston”and the relationship between volumetric mixing degree and operating conditions are explored.The results show that the“liquid piston”first axially expands and then gradually stabilizes,isolating the brine and seawater.Additionally,as long as the volume utilization ratio(U_(R))of the pressure exchange cylinder remains constant,there will not be much difference in the volumetric mixing degree after stabilization of the“liquid piston”(Vm-max)regardless of changes in the processing capacity(Q)and cycle time(T_(0)).Therefore,the equation for Vm-max with respect to the operating parameters(Q,T_(0))is derived,which can not only predict the Vm-max of the TCERD,but also provide an empirical reference for the design of other valve-controlled devices with“liquid piston”.When the Vm-max is 6%,the efficiency of the TC-ERD at design conditions(30 m^(3)·h^(-1),5.0 MPa)is 97.53%. 展开更多
关键词 DESALINATION ENERGY RECOVERY MIXING Liquid piston
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THE NUMERICAL ANALYSIS OF UNSTEADY HEAT TRANSFER OF A PISTON-LINER COUPLED SYSTEM IN AN INTERNAL COMBUSTION ENGINE
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作者 蒋惠强 《Journal of Southeast University(English Edition)》 EI CAS 1993年第2期69-78,共10页
This paper provides a numerical analysis model of unsteady heat trans-fer in piston-liner set of an internal combustion engine.The model simulates the un-steady heat transfer process among the combustion mixture,pisto... This paper provides a numerical analysis model of unsteady heat trans-fer in piston-liner set of an internal combustion engine.The model simulates the un-steady heat transfer process among the combustion mixture,piston set,lubricantfilm,liner and coolant in a whole engine cycle,and can predict the temperature fluc-tuation and distribution on piston crown,inner surface of liner,piston ring and thelubricant film.A computer program is developed to calculate the unsteady heat trans-fer process of piston-liner system in a water-cooled diesel engine. 展开更多
关键词 FEM FDM I.C. Engine temperature distributions transients fluctuation/unsteady heat transfer piston-liner coupled system
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Static and Thermal Analysis of Aluminium (413,390,384 and 332) Piston Using Finite Element Method
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作者 Offei David Inusah Jacob Kwaku Nkrumah Vincent Akolbire Atindana 《Modeling and Numerical Simulation of Material Science》 2024年第1期1-38,共38页
The main objective of this research was to examine the suitability of aluminium alloy to design a piston of an internal combustion engine for improvement in weight and cost reduction. The piston was modelled using Aut... The main objective of this research was to examine the suitability of aluminium alloy to design a piston of an internal combustion engine for improvement in weight and cost reduction. The piston was modelled using Autodesk Inventor 2017 software. The modelled piston was then imported into Ansys for further analysis. Static structural and thermal analysis were carried out on the pistons of the four different materials namely: Al 413 alloy, Al 384 alloy, Al 390 alloy and Al332 alloy to determine the total deformation, equivalent Von Mises stress, maximum shear stress, and the safety factor. The results of the study revealed that, aluminium 332 alloy piston deformed less compared to the deformations of aluminium 390 alloy piston, aluminium 384 alloy piston and aluminium 413 alloy piston. The induced Von Mises stresses in the pistons of the four different materials were found to be far lower than the yield strengths of all the materials. Hence, all the selected materials including the implementing material have equal properties to withstand the maximum gas load. All the selected materials were observed to have high thermal conductivity enough to be able to withstand the operating temperature in the engine cylinders. 展开更多
关键词 Von Mise stress Total deformation Aluminium alloy Thermal analysis. piston Static structural Heat fux
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The Effect of Ignition Parameters on the Combustion Characteristics of an Aviation Piston Engine
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作者 Luda Zhu Wenming Cheng +1 位作者 Eryang Liu Shupeng Wang 《World Journal of Engineering and Technology》 2024年第2期245-257,共13页
A cylinder combustion simulation model was established for a two-stroke aviation piston engine used in a small unmanned aerial vehicle. The influence of different ignition system parameters on the combustion process o... A cylinder combustion simulation model was established for a two-stroke aviation piston engine used in a small unmanned aerial vehicle. The influence of different ignition system parameters on the combustion process of aviation kerosene was studied using this model. The research results showed that under the working conditions of 5500 r/min and 50% throttle opening, as the ignition energy increased, the peak values of average cylinder pressure and average temperature increased, and the combustion duration shortened, The advance of the combustion center of gravity increases the tendency of the engine to knock. Under the same operating conditions, as the ignition timing advances, the peak values of average pressure and average temperature in the cylinder increase, gradually approaching the top dead center, and the tendency of engine detonation increases more significantly. 展开更多
关键词 Aircraft piston Engines Aviation Kerosene IGNITION Combustion Characteristics KNOCK
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气体活塞式压力计超局部化无模型自适应控制研究
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作者 庞桂兵 王思遥 +2 位作者 高腾 杨远超 原浩 《仪器仪表学报》 北大核心 2025年第4期306-314,共9页
活塞式压力计是一种重要的压力溯源检测装备。活塞系统是气体活塞式压力计的核心部件,由于气体介质特性,活塞精准定位和快速稳定是一项难题。通过分析气体活塞式压力计活塞系统的非线性因素,提出超局部化无模型自适应控制(ULMFAC)方法,... 活塞式压力计是一种重要的压力溯源检测装备。活塞系统是气体活塞式压力计的核心部件,由于气体介质特性,活塞精准定位和快速稳定是一项难题。通过分析气体活塞式压力计活塞系统的非线性因素,提出超局部化无模型自适应控制(ULMFAC)方法,采用超螺旋非奇异终端滑模控制(STNTSMC)与有限时间扰动观测器相结合,有效避免了滑模控制中的抖振现象,并显著提高了系统的动态响应特性。由于活塞有效面积、温度和介质泄漏等参数变化,基于超局部化无模型方法建立改进二阶动力学模型,避免基于模型的控制方法对于精确系统模型的约束。设计非奇异终端滑模面,解决了终端滑模控制中的奇异性问题,并利用自适应超螺旋方法抑制不连续控制引起的抖振现象,进一步提高系统的动态响应。构造扰动观测器估计系统的集总不确定性,实现有限时间稳定,通过Lyapunov函数证明了所设计控制方案的稳定性和有限时间收敛性。系统仿真和实验结果表明,ULMFAC方法在0.5、3和6 MPa的不同工况下,能够显著提高系统的鲁棒性、活塞的定位精度和动态响应,对于实现高精度和高效率的压力测量,具有重要的理论意义和实用价值。 展开更多
关键词 压力计 活塞系统 自适应控制 控制策略 鲁棒性
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航空活塞发动机有效功率及空中功率恢复研究
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作者 温占永 田亚明 +1 位作者 孙鹏晖 赵韦东 《科学技术与工程》 北大核心 2025年第16期6760-6765,共6页
针对某型航空活塞发动机提出一种基于中冷系统传热数学仿真的有效功率计算方法,并应用VB语言对该中冷系统传热仿真模型进行开发。通过试验数据对仿真模型的有效性进行验证。结果表明:中冷器冷侧出口温度、热侧出口温度的仿真计算值与试... 针对某型航空活塞发动机提出一种基于中冷系统传热数学仿真的有效功率计算方法,并应用VB语言对该中冷系统传热仿真模型进行开发。通过试验数据对仿真模型的有效性进行验证。结果表明:中冷器冷侧出口温度、热侧出口温度的仿真计算值与试验值误差均在1.5%以内。利用该仿真模型,研究了风扇风量对航空活塞发动机有效功率的影响,并对空中有效功率恢复进行研究。结果表明:随着风扇风量的增加,风扇功率增幅变大,而发动机功率增幅降低。在二者的综合作用下,发动机有效功率随着风扇风量的增加先升高后下降。对于所研究的航空活塞发动机,当风扇风量为1400 m^(3)/h时,发动机有效功率达到最大,其最大值为101.6 kW。当飞行高度在2000 m以下时,随着飞行高度的升高,发动机有效功率恢复系数小幅增加,当飞行高度在2000 m以上时,发动机有效功率随着飞行高度的增加大幅降低。在海平面环境为50℃条件下,在7000 m高度即便维持稳压箱压力不变,发动机有效功率恢复系数仅能达到92.2%。 展开更多
关键词 航空活塞式发动机 中冷系统 电动风扇 稳压箱温度 有效功率
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旋转导向钻井系统微型斜盘式轴向柱塞泵的设计与仿真
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作者 叶哲伟 刘兵 +2 位作者 刘章 周瑜 金存 《机床与液压》 北大核心 2025年第14期149-156,共8页
为了满足井下旋转导向钻井系统液压动力单元中的柱塞泵高转速、小尺寸和高精度的要求,设计一种微型斜盘式轴向柱塞泵,其排量可达0.036 mL/r,工作压力可达30 MPa。分析柱塞位移和斜盘倾角的转换关系,建立柱塞位移转化的数学模型。运用AME... 为了满足井下旋转导向钻井系统液压动力单元中的柱塞泵高转速、小尺寸和高精度的要求,设计一种微型斜盘式轴向柱塞泵,其排量可达0.036 mL/r,工作压力可达30 MPa。分析柱塞位移和斜盘倾角的转换关系,建立柱塞位移转化的数学模型。运用AMESim搭建微型斜盘式轴向柱塞泵各个零部件模型,完成整泵液压系统模型的建立。结果表明:在额定工况下,柱塞泵的输出流量在0.032~0.035 L/min内脉动,平均出口流量为0.033 L/min,出口压力在9~10 MPa内脉动;随着柱塞斜盘倾斜角的减小,泵的输出流量减小,流量脉动变小,当斜盘倾角增大时,柱塞的位移增大,泵的输出流量也增大。对泵样机进行试验,分析了该泵的输出特性和效率曲线,与仿真分析结果进行对比。结果表明:泵的输出流量随着电机转速的增大而增大,其总效率随着工作压力的增大而增大;仿真效果较好,同时验证了仿真方法和结果的可靠性。微型斜盘式柱塞泵在额定工况下的容积效率可达到84.2%。 展开更多
关键词 旋转导向钻井系统 微型斜盘式轴向柱塞泵 AMESIM仿真 斜盘倾角
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活塞式体积管法微小气体流量标准装置 被引量:1
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作者 杨宏明 徐雅 +2 位作者 刘铁军 谢代梁 黄震威 《计量学报》 北大核心 2025年第5期700-708,共9页
为实现对微小气体流量计的便携式计量校准,设计了一种基于活塞式体积管法的微小气体流量标准装置。通过数学建模设计了活塞的几何尺寸,构建了基于光纤传感器的光电检测系统,以满足装置所需的检测时间准确度。利用动网格6DOF技术研究光... 为实现对微小气体流量计的便携式计量校准,设计了一种基于活塞式体积管法的微小气体流量标准装置。通过数学建模设计了活塞的几何尺寸,构建了基于光纤传感器的光电检测系统,以满足装置所需的检测时间准确度。利用动网格6DOF技术研究光纤传感器位置,通过分析活塞运动中的惯性效应,确保在2个光纤传感器之间的匀速运动。为满足现场在线检定智能化系统的需求,开发基于PLC的控制系统,并设计了人机交互控制与数据采集界面。对装置的不确定度进行了分析和评定,结果表明该装置的扩展不确定度为0.38%(k=2)。 展开更多
关键词 流量计量 气体流量标准装置 活塞式体积管 控制系统 不确定度
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A Kind of PWM Pneumatic Servo Control System——Modulation Methods and Dynamic Responses 被引量:2
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作者 姚晓先 陈汉超 《Journal of Beijing Institute of Technology》 EI CAS 1992年第1期50-58,共9页
Vibrations or dither's are features of the PWM servo control system in their steady outputs. On the grounds of analyses and experiments of a PWM pneumatic servo control system, the paper puts forward four varietie... Vibrations or dither's are features of the PWM servo control system in their steady outputs. On the grounds of analyses and experiments of a PWM pneumatic servo control system, the paper puts forward four varieties of PWM modulation methods, and concludes on the relationship between dithers and the different methods, and then discusses the influence of friction to the dithers. Results from experiments regarding the dynamic and static responses on the given system support the theories presented. 展开更多
关键词 pulse width modulation pneumatic piston actuating mechanisms servo control servo valves FRICTION vibration effect
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基于遗传算法的相位差法波前检测piston误差 被引量:2
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作者 曹芳 赵继勇 吴桢 《天文研究与技术》 CSCD 2011年第4期369-373,共5页
光学综合孔径望远镜常常因为子望远镜间的失调大于1λ产生相位差,影响望远镜的分辨能力。基于相位差法的检测技术,可以检测出子望远镜间的微小失调误差。提出了相位差波前检测方法与遗传算法相结合,设计了一个相位差波前传感器,进行综... 光学综合孔径望远镜常常因为子望远镜间的失调大于1λ产生相位差,影响望远镜的分辨能力。基于相位差法的检测技术,可以检测出子望远镜间的微小失调误差。提出了相位差波前检测方法与遗传算法相结合,设计了一个相位差波前传感器,进行综合孔径望远系统的piston误差检测。在计算机模拟成像系统的基础上,仿真结果证明,基于遗传算法的相位差波前检测方法可以较准确地恢复波前相位,检测piston误差。 展开更多
关键词 波前检测 综合孔径望远镜 相位差法 piston误差 遗传算法
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严寒地区地铁活塞风道设置必要性探讨
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作者 马骁 何维 +2 位作者 邢天文 孟鑫 李国庆 《都市快轨交通》 北大核心 2025年第5期136-141,共6页
为研究我国严寒地区地铁活塞风道设置的必要性,本文选取运营中的沈阳地铁1、9号线典型车站公共区和区间隧道,对其最热月开式运行、最冷月闭式运行模式下的温度、二氧化碳浓度和可吸入颗粒物浓度进行测试;并将以温度为代表的热环境和以... 为研究我国严寒地区地铁活塞风道设置的必要性,本文选取运营中的沈阳地铁1、9号线典型车站公共区和区间隧道,对其最热月开式运行、最冷月闭式运行模式下的温度、二氧化碳浓度和可吸入颗粒物浓度进行测试;并将以温度为代表的热环境和以二氧化碳浓度、可吸入颗粒物浓度为代表的空气质量作为评价指标,量化测评沈阳地铁全高非封闭站台门开式通风系统对既有线典型车站公共区和区间隧道的实际环控效果。研究结果表明:沈阳地铁全高非封闭站台门开式通风系统在区间隧道内形成的活塞通风量已大于其温度控制所需,活塞风道对区间隧道热环境的实际调控能力较弱;关闭活塞风道后,车站公共区和区间隧道的空气质量仍可满足设计规范要求;沈阳地铁未来新线可考虑取消活塞风道(井)的活塞通风系统优化设计方案;取消活塞风道(井)对车站公共区和区间隧道的平时、事故工况下的通风模式安全性均无影响。本文的研究成果可为我国严寒地区其他城市地铁的活塞通风系统的优化设计提供参考。 展开更多
关键词 严寒地区地铁 活塞通风系统 活塞风道 开闭式运行 热环境 空气质量
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大型飞机多泵并联液压系统壳体回油干扰研究
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作者 郭团辉 肖文键 +1 位作者 刘继 付永领 《航空工程进展》 2025年第4期188-199,共12页
大型飞机多泵并联液压系统的壳体回流油液相互干扰问题直接影响飞机液压系统的性能和飞行安全。首先,基于对大型飞机液压系统和多泵并联能源系统的分析,建立考虑压力、流量和温度等因素的并联柱塞泵的壳体回油理论模型;然后,在理论研究... 大型飞机多泵并联液压系统的壳体回流油液相互干扰问题直接影响飞机液压系统的性能和飞行安全。首先,基于对大型飞机液压系统和多泵并联能源系统的分析,建立考虑压力、流量和温度等因素的并联柱塞泵的壳体回油理论模型;然后,在理论研究的基础上建立柱塞泵和液压系统的仿真模型,并分析柱塞泵壳体回油压力—流量特性和多泵并联壳体回油干扰现象;最后,结合实例探究多泵并联系统壳体回油干扰对泵体温升的影响,并对壳体回油干扰提出相应的改善方案。结果表明:回油干扰的影响程度随着流量偏差的增加而增大,回油干扰与流量偏差和管路直径密切相关。 展开更多
关键词 大型飞机 液压系统 柱塞泵 多泵并联系统 壳体回油干扰
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耦合缓冲过程的绝热-等温压缩空气储能系统热力性能研究 被引量:3
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作者 陈昊 张宇飞 +2 位作者 李瑞雄 孙昊 王焕然 《热力发电》 北大核心 2025年第2期68-78,共11页
为了确保绝热-等温压缩空气储能系统连续稳定运行,提出了一种耦合缓冲罐的绝热-等温压缩空气储能方法,建立了耦合缓冲罐系统的动态热力学模型,并搭建实验平台对模型进行了验证,揭示了缓冲罐内空气温度及压力的动态演化机理,探究了缓冲... 为了确保绝热-等温压缩空气储能系统连续稳定运行,提出了一种耦合缓冲罐的绝热-等温压缩空气储能方法,建立了耦合缓冲罐系统的动态热力学模型,并搭建实验平台对模型进行了验证,揭示了缓冲罐内空气温度及压力的动态演化机理,探究了缓冲罐设计参数对系统性能的影响规律。研究结果表明:耦合缓冲罐的绝热-等温压缩空气储能系统表现出较好的等温性能,循环过程中空气温度最大温差为30 K;耦合缓冲罐后,储能系统压缩机组的绝热效率提高8百分点;敏感性分析表明,储能功率的变化对储气室内空气热力学参数影响较小,缓冲罐体积随系统储能功率的增大而减小;储能规模的变化对储气室内空气热力学参数影响较小,储气室内空气温度变化呈周期性波动;为保持系统连续稳定运行,增大系统储能规模,缓冲罐体积会随之增加。研究为绝热-等温压缩空气储能系统连续、稳定和高效运行提供了新的方案。 展开更多
关键词 液体活塞 绝热-等温压缩空气储能系统 缓冲罐 热力学分析
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