Impact pressure of waves generated by landslides on bank slopes

Impulse waves that are generated by landslides in narrow reservoir areas threaten the stability of buildings and bank slopes.To discuss the action process and evolution law of the wave pressure on bank slopes,a three-dimensional physical model test that considers impulse waves generated by landslides was performed,and factors including landslide width,thickness,slope angles of the sliding surface,and bank slope angle were considered.Based on wave forms on the bank slopes,wave pressure curve characteristics,and peak value,the action process of wave pressure could be divided into the following stages:maximum pulsating pressure stage,wave impact stage(when waves break),and stationary pulsation stage.It was found that wave breaking is dependent on the value of the surf similarity parameterξ.The distribution pattern of impact pressure decays linearly on both sides of the maximum impact pressure point,and the attenuation degree decreases when it attains 40%of the maximum value.Thus,it is proposed that the prediction formula for the maximum effective impact pressure of the bank slope be related to the reciprocal of wave steepness,relative water depth,and slope rate.The prediction formula provides strong theoretical support for early safety warning and for predicting the bank slope under impulse waves generated by landslides.

Pressure pulsation in stages of electric submersible pump at shut-off under various speeds

Electric submersible pumps were widely used in agricultural fields,petroleum and various other industries. The pressure pulsation caused fatigue failure due to vibration in electric submersible pump and affects the life and performance of its system. The objective of this study was to experimentally investigate the characteristics of pressure pulsation which were generated at various stages of a multistage electric submersible pump during closed valve operation at different speeds. An electric submersible pump with five stages was selected for conducting experiments. A variable frequency drive( VFD)was used to operate the electric submersible pump at five different speed settings from 40 to 60 Hz. Piezoresistive pressure transducers were mounted at each stage of the electric submersible pump to capture the unsteady pressure signals. At each speed setting,the electric submersible pump was operated at the shut-off condition and the signals of unsteady pressure from all the five stages were captured. A fast fourier transformation( FFT) was carried out on the pressure signals to convert into frequency domain.From the spectra of pressure pulsation signals,the characteristics of pressure pulsation are obtained for each stage and for various speed settings which were then used to understand its variation with speed and stages.

A two-stage blade-packing rotating packed bed for intensification of continuous distillation

A two-stage blade-packing rotating packed bed(TSBP-RPB) was designed and developed for the intensification of continuous distillation. The mass transfer parameters of the TSBP-RPB were investigated using a chemisorption system. Continuous distillation experiments were conducted in the TSBP-RPB by the methanol–water binary system. Experimental results showed that values of the effective interfacial area and liquid-side mass transfer coefficient of the TSBP-RPB were 93–337 m^2·m^(-3) and 0.05–0.19 cm·s^(-1), respectively. The height of equivalent theoretical plate(HETP) of the TSBP-RPB ranged from 1.9 to 10 cm. Moreover, the TSBP-RPB is easy to be manufactured, which shows great potential for the application of continuous distillation.

Effects of stator bending on pressure field and loss of transonic turbine stage

To study effects of the upstream flow field changing on the downstream flow field of transonic turbine, different three-dimensional bowed blades, which are the stator blades of transonic turbine stage, were designed in this paper. And then numerical calculations were carried out. The effects on downstream flow field were studied and analyzed in detail. Results show that, at the middle of stator blades, although the increasing Mach number causes the increase of shock-wave strength and friction, the middle flow field of downstream rotors is improved obviously. It is an important change in transonic condition. This causes the loss of the rotor’s middle part decreased greatly. Correspondingly, efficiency of the whole transonic stage can be increased.

Tests and numerical simulation on curved blade of super-critical adjust stage

Tests and numerical simulations of super-critical adjust stage blade were carried out and the effect of bowed blade on flow characteristics and the secondary flow were analyzed. The simulation and test results show that the adjust stage blade with aft-loading and big front-edge radius has good flow characteristics by meridian shrink. The numerical studies were carried out with software of NUMECA in order to investigate the aerodynamic characteristics of adjust stage blades,which include prototype blade(tested blade) ,positive curved blade (15°) and negative curved blade(-15°) . The simulation results show that the positive curved blade forms a negative static pressure gradient in the lower region of the cascade along the blade height and a positive static pressure gradient in the upper region. This leads to the reduction of the streamwise vortices intensity and the aerodynamic load on both sides of the blade and the endwall. Therefore,the crosswise secondary flow losses of endwall can be decreased considerably.

Experimental Investigation of Unsteady Pressure on an Axial Compressor Rotor Blade Surface

The inherent unsteady pressure fluctuations on the rotating blade suction surface of an axial compressor were experimentally measured by directly mounting five high response miniature pressure transducers into the rotor blade along a streamline at 50% span respectively. The results show that the unsteady pressure fluctuations of rotor blade surface could be measured successfully by this means. The relations about the period, altitude of unsteady pressure with rotating speed, the discipline of pressure fluctuation along the streamwise direction were obtained.

Manual Uterine Fundal Pressure in the Spontaneous Delivery during the Second Stage of Labor: A Pilot Case-Control Study Following an Analysis of Questionnaire Survey

Background: Recent obstetrical practice tends to avoid the use of manual uterine fundal pressure (MUFP);however, data showed that MUFP is actually employed. We here attempted 1) to determine the obstetricians’ attitudes towards MUFP via questionnaire, and 2) to examine whether MUFP shortens the 2nd stage of labor, with the latter tested as a pilot study. Methods: A questionnaire-based study was carried out (n = 122) at meetings of Obstetrics on May 5, 2017. Then, we conducted a pilot case-control study from August 23 to September 6, 2020. Participants (n = 29) were divided into two groups;women who did and did not want MUFP;i.e., MUFP (n = 14) vs. (Non-MUFP) group (n = 15). Results: Of 122 doctors, 99.18% (121/122) used MUFP at cesarean section. 95.90% (117/122) of institutions used MUFP in spontaneous delivery. 95.08% (116/122) obstetricians considered MUFP effective and helpful. 85.24% (104/122) considered that MUFP should be employed after station +3. In the case control study, MUFP vs. Non-MUFP group showed the second-stage-duration of 58.5 (50.25 - 71.25) vs. 48 (39 - 59) minutes, without statistical significance (P = 0.101). However, importantly, MUFP, compared with Non-MUFP group, showed a significantly shorter duration from head visible on introitus (apparition) to delivery;i.e., 21.26 ± 7.32 vs. 30.13 ± 10.61 minutes (P = 0.014). Conclusions: MUFP is still used widely and MUFP shortened the duration of head apparition to delivery time. Larger-sample studies are needed to confirm the efficacy and safety of MUFP.

Analogy Theory and Application of Pressure Difference of Wind Turbine Blade Profile

This paper aims to design an optimized blade for Horizontal Axis Wind Turbine(HWAT).Since airfoil is a basic component of blade design,an optimized airfoil(referred as SJX)was proposed based on the line theory through the weight analogy to pressure distribution of air flow.Its lift,drag,lift⁃to⁃drag ratio were compared with those NACA2409⁃34,NACA2410,and RK40 airfoils by using Profili software at fixed wind velocity and under different angles of attack.The NACA2409⁃34 airfoil was found to be greatly similar with the SJX airfoil.Based on the Wilson method,blades using SJX and NACA2490⁃34 airfoils were developed and different performance parameters such as velocity distribution,pressure distribution,and power were compared under variable wind velocities and different angles of attack ranging from-4°to 6°at different radius from the center of rotor using computational fluid dynamics(CFD)in ANSYS FLUENT.Results of the study suggested that the performance of the SJX based airfoil and blade was much more optimized.

Numerical analysis and optimization of the inlet stage of a multi-stage high pressure compressor

An opti mization process is used to redesign blades of a high-pressure compressor.An artificial neural network (ANN) method is coupled to Navier-Stokes solvers and is applied to three different redesigns.A newrotor blade of a transonic compressor is designed by modifying thick,stacking line andinlet angle using a 3Dapproach,with a significant efficiencyi mprovement at the design point.The off-design behavior of this new compressor is also checked afterwards,which shows that the whole performance of the inlet stage is improved over a wide range of mass flow.The losses are reduced,proving the good performance of the opti mum.The whole results indicate that the opti mization method can find i mproved design and can be integrated in a design procedure.

叶片数对无轴泵喷推进器性能的影响

为丰富无轴泵喷推进器噪声性能优化理论,研究了叶片数对无轴泵喷推进器性能的影响,重点探究了不同叶片数下无轴泵喷推进器内的压力脉动变化规律。基于计算流体力学中的有限体积法离散RANS方程,应用RNG k-ε湍流模型封闭计算模型,采用SIMPLEC进行压力-速度耦合,对不同叶片数下的无轴泵喷推进器内部流场进行了非定常数值模拟计算,并对计算结果进行了详细的对比分析。研究结果表明:随叶片数的增加,无轴泵喷推进器模型的扬程、效率和推力均逐渐增大,叶片表面压力分布更加均匀,叶轮轮缘和中部的压力脉动均明显降低,叶轮进出口主频处的压力脉动幅值从轮缘向中心逐渐减小。

压力敏感涂料测量技术在掠型叶栅表面测压中的应用

为了获得某掠型叶片吸力面压力分布,对一稠度为1.53,掠角为10.7°的掠叶栅进行了光路布局以及压力敏感涂料(PSP)压力测量,利用图像处理和三维重构算法得到了可读性高、便于数据提取的三维叶片吸力面压力分布,并和测压孔测量结果进行了对比。结果表明:利用自主发展的光路布局方法,有效解决了叶片表面光照辐照度不均匀、拍摄视角受限的问题;得到了高信噪比的原始压敏图像以及宽范围多工况的掠叶栅吸力面全域压力分布。与测压孔测量相比,PSP测量误差在5%以内,并且PSP测量结果还捕捉到了峰值等熵马赫数位置沿弦向的迁移以及叶片尾缘的气流分离现象。对不同攻角和来流马赫数下的掠型叶片吸力面压力分布进行分析:掠型叶片在零攻角和正攻角下存在明显的径向压力梯度,促使后掠型叶片气流向前掠迁移,增加了前掠下流低能流体的能量,使得前掠更有利于延迟角区分离,后掠则更容易发生角区分离;掠型叶片在低来流马赫数下展向压力对称性良好,掠设计的影响不显著,高来流马赫数则放大了前后掠对角区分离控制效果的不同。相比传统测压孔有限的压力分辨率,PSP测量可为掠型叶片设计和流动机理分析提供丰富可靠的压力实验数据。

涡轮钻具定转子三维叶型的设计方法研究

为了研究涡轮三维叶型的水力性能,基于等环量法提出了一种涡轮三维叶型的理论造型方法,并推导出了该涡轮三维叶型的特性参数计算方法。利用ANSYS Fluent对同尺寸下的涡轮三维叶型和二维叶型进行了数值模拟分析其水力特性。研究结果表明:与二维叶型相比,涡轮三维叶型的压降减小约50%,水力效率提高约5%。对比了三维叶型涡轮扭矩的理论计算结果与仿真结果,发现它们的误差在10%左右,在实际工程允许范围内。研究结果可为涡轮三维叶型的设计提供理论依据。

一种引入过渡阶段和高斯变异的改进算术优化算法

针对算术优化算法收敛精度低、易陷入局部最优等问题,提出了一种改进的过渡高斯算术优化算法,该算法将新的非线性过渡阶段与改进的高斯变异策略相结合.首先,为了更好地从勘探阶段的高离散度策略过渡到开发阶段的低离散度策略,提出过渡阶段策略,并通过比较三种曲线实验重构数学优化加速函数.其次,引入具有算术优化算法特性的高斯变异策略和边界函数策略,加强算法跳出局部区域的能力.最后,将改进后的算术优化算法与几种著名算法进行对比,并进行不同维度的可扩展性分析,验证了所提算法的有效性.此外,该算法在压力容器设计问题中进行了测试.实验结果表明,TGAOA具有优异的收敛精度、收敛速度和鲁棒性.

叶片破损对压气机性能的影响

为了研究叶片破损对压气机内部流场的影响机理,本文针对带有破损的跨音速压气机叶片进行气动性能变化规律和机理研究。通过NASA rotor 37实验结果验证了计算方法的准确性,利用数值仿真研究了叶片破损对压气性能的影响规律,并对2种典型工况下叶片破损前后的流场结构进行对比分析,探讨引起性能变化的具体原因。研究表明:叶片破损会导致压气机的压比降低0.6631%、绝热效率降低0.7877%,且压气机的稳定裕度降低更为明显。叶尖破损主要对叶顶流场结构产生影响,使叶顶区域泄漏流增强,当其与激波相互作用时,通道内产生了流动堵塞和流动损失。本文研究成果可为实际服役中的航空发动机特性评定提供理论参考。

The Third-Order Viscoelastic Acoustic Model Enables an Ice-Detection System for a Smart Deicing of Wind-Turbine Blade Shells

The present work is based on the third-order partial differential equation (PDE) of acoustics of viscoelastic solids for the quasi-equilibrium (QE) component of the average normal stress. This PDE includes the stress-relaxation time (SRT) for the material and is applicable at any value of the SRT. The notion of a smart deicing system (SDS) for blade shells (BSs) of a wind turbine is specified. The work considers the stress in a BS as the one caused by the operational load on the BS. The work develops key design issues of a prospective ice-detection system (IDS) able to supply an array of the heating elements of an SDS with the element-individual spatiotemporal data and procedures for identification of the material parameters of atmospheric-ice (AI) layer accreted on the outer surfaces of the BSs. Both the SDS and IDS flexibly allow for complex, curvilinear and space-time-varying shapes of BSs. The proposed IDS presumes monitoring of the QE components of the normal stresses in BSs. The IDS is supposed to include an array of pressure-sensing resistors, also known as force-sensing resistors (FSRs), and communication hardware, as well as the parameter-identification software package (PISP), which provides the identification on the basis of the aforementioned PDE and the data measured by the FSRs. The IDS does not have hardware components located outside the outer surfaces of, or implanted in, BSs. The FSR array and communication hardware are reliable, and both cost- and energy-efficient. The present work extends methods of structural-health/operational-load monitoring (SH/OL-M) with measurements of the operational-load-caused stress in closed solid shells and, if the prospective PISP is used, endows the methods with identification of material parameters of the shells. The identification algorithms that can underlie the PISP are computationally efficient and suitable for implementation in the real-time mode. The identification model and algorithms can deal with not only the single-layer systems such as the BS layer without the AI layer or two-layer systems but also multi-layer systems. The outcomes can be applied to not only BSs of wind turbines but also non-QE closed single- or multi-layer deformable solid shells of various engineering systems (e.g., the shells of driver or passenger compartments of ships, cars, busses, airplanes, and other vehicles). The proposed monitoring of the normal-stress QE component in the mentioned shells extends the methods of SH/OL-M. The topic for the nearest research is a better adjustment of the settings for the FSR-based measurement of the mentioned components and a calibration of the parameter-identification model and algorithms, as well as the resulting improvement of the PISP.

左室压力-应变环评估终末期肾病透析患者左室收缩功能的临床价值

目的探讨左室压力-应变环(LV-PSL)评估终末期肾病血液透析和腹膜透析患者左室收缩功能的临床应用价值。方法选取于我院就诊的79例慢性肾脏病5期患者,其中血液透析组29例、腹膜透析组27例及未透析组23例,均行常规超声心动图检查并获取相关参数,应用自动心肌功能成像分析软件获取左室整体纵向应变(GLS)及心肌做功指数(MWI),包括整体做功指数(GWI)、整体有效功(GCW)、整体无效功(GWW)、整体做功效率(GWE),比较各组上述参数的差异。分析MWI与常规超声心动图参数、GLS、血压、透析时间、透析方式的相关性。结果各组常规超声心动图参数和GLS比较差异均无统计学意义。血液透析组GWI、GCW均低于腹膜透析组和未透析组,GWW高于腹膜透析组和未透析组,GWE低于腹膜透析组,差异均有统计学意义(均P<0.05)。相关性分析显示,GWI、GCW与GLS、左室射血分数(LVEF)、收缩压、舒张压均呈正相关,与室间隔厚度(IVS)、透析时间、透析方式均呈负相关(均P<0.05);GWW与透析方式呈正相关,与GLS呈负相关(均P<0.05);GWE与GLS、LVEF均呈正相关,与IVS、左室后壁厚度、透析方式均呈负相关(均P<0.05)。结论血液透析对终末期肾病患者左室收缩功能的影响较腹膜透析更大,LV-PSL能准确评估该类患者左室收缩功能,具有较好的临床应用价值。

火电机组低负荷运行对末叶片可靠性的影响

在双碳目标下,为了配合新能源的发展,火电机组的调峰能力得到了前所未有的关注。结合电力需求增速放缓的现状,火电机组将较长时间运行在低负荷工况下。本文选取某660 MW空冷机型末三级级段进行了多个低负荷工况下的CFD分析,获得了负荷下降过程中末级流场的变化特征,并分析了相关变化对末叶片可靠性的影响,介绍了相关的解决措施。

胜利油田油藏数值模拟技术新进展及发展方向

油藏数值模拟技术是油藏分析的重要手段,是油田开发人员编制开发方案、开展动态跟踪调整、进行提高油藏采收率研究等工作的有力工具。为明确胜利油田油藏数值模拟技术的未来发展方向,回顾了胜利油田60年以来油藏数值模拟应用技术和自主知识产权软件研发的发展历程,着重总结了“十三五”以来适配油田当前地质及开发特征的特高含水期精细油藏描述、低渗透油藏压驱开发、非均相复合驱、稠油油藏多元热复合驱、CO_(2)高压混相驱、页岩油大规模压裂整体开发等多个领域的数值模拟应用技术创新性进展;介绍了涵盖水驱、化学驱、微观、智能模拟等不同方向的多款胜利特色油藏数值模拟软件的研发及应用情况。最后指出在当前胜利油田的开发形势下,油藏数值模拟在精细程度、规模、效率和协作方式等方面面临着更大的挑战,油藏数值模拟需要进一步向一体化、并行化、智能化方向发展,为胜利油田开发提质增效提供技术支撑。

南芬选矿厂北山矿石选矿工艺试验

为配合南芬铁矿绿色矿山选矿提效及高效利用北山原矿石,在工艺矿物学研究的基础上,对北山矿石进行了选矿工艺流程试验。试验结果表明:采用辊磨前干抛—高压辊磨—辊磨产品湿式抛尾—阶段磨矿—弱磁选工艺,干抛和湿抛可提前抛除合计产率23.26%的尾矿,大幅降低了后续入磨矿量,提升了入磨矿样铁品位,最终获得的铁精矿产率为30.77%,TFe和mFe含量分别为68.17%和60.22%,TFe和mFe回收率分别为66.63%和98.16%。