涡旋压缩机不对称双涡旋齿型线的构建与模拟

采用双涡旋齿涡旋盘结构能够有效地提高涡旋压缩机的吸气量,然而存在内容积比小、允许开设的排气口面积小的缺点。针对此问题,本文提出一种涡旋压缩机的新型不对称双涡旋齿,利用中线法得到了涡旋齿型线的设计方法,并且建立其几何模型;通过三维数值模拟研究其工作腔内部的气体流场,并与现有的双涡旋齿涡旋压缩机进行对比。结果表明:所提出的涡旋压缩机的新型不对称双涡旋齿能够有效地提高涡旋压缩机的排气量和内容积比,并且增大了排气口的开设面积,使得压缩机具有更好的工作性能。     

Energy Analysis of Precooling Air Compressor System

Energy saving is one of the main technique routes for net zero carbon emissions. Air compressor systems take up a large part of energy consumption in the industrial field. A pre-cooling air compressor system was proposed for energy saving by cooling the air before it flows in a compressor. The energy efficiency of the proposed system was analyzed. As additional energy consumption is required for air cooling, the feasibility of the pre-cooling method for energy saving was analyzed. As the efficiency of the pre-cooling air compressor system is mainly influenced by the environment temperature and humidity, applicability of the system in different regions and at different seasons was discussed. A pilot project was performed to verify the technical feasibility and economics of the proposed system. When the precooling temperature of the pilot system was set to 2 °C, the annual pneumatic-electrical ratio of the system can be increased by approximately 2% in several regions of China. This paper shows the pre-cooling air compressor system is feasible for energy saving.     

低温过冷测试平台冷压缩机性能的测试研究

冷压缩机具有工作温度低、尺寸小、功耗低、便于操控等特点,是大型过冷氦低温系统中的关键设备。对低温过冷测试平台的冷压缩机进行测试,方法为采用两台串联的冷压缩机在低温低压下直接抽吸饱和液氦容器,液氦容器内装有电加热器用以模拟超导磁体的热负荷,并调节氦气蒸发速率。测试表明,冷压缩机的稳定工作参数接近设计值,运行过程中冷压缩机始终保持安全运行,未出现喘振情况,液氦容器温度和压力分别达到3 K、22 kPa,满足设计要求。     

离心压气机级三元粘性计算

使用叶片排间隙混合平面概念，完成离心压气机级多叶片排三元N-S方程计算。每个动静叶片排内的流动被认为是定常的且由相对独立的程序段进行运算。这样的串行程序很容易被改造为在并行系统上运行的SPMD并行程序。     

Design of a laser pointer

A laser pointer has been designed using a red diode laser (670 nm). The optics of the pointer consists of a four element collimating lens, two prism compressor and a two lens reversed Galilean afocal. The beam diameter of the laser pointer is 4.2 mm.     

Design and properties analysis of multi-layer dielectric used in pulse compressor gratings

Used in chirped-pulse amplification system and based on multi-layer thin film stack, pulse compressor gratings (PCG) are etched by ion-beam and holographic techniques. Diffraction efficiency and laser-induced damage threshold rely on the structural parameters of gratings. On the other hand, they depend greatly on the design of multi-layer. A theoretic design is given for dielectric multi-layer, which is exposed at 413.1 nm and used at 1053 nm. The influences of coating design on optical characters are described in detail. The analysis shows that a coating stack of H3L (H2L)9H0.5L2.01H meets the specifications of PCG well. And there is good agreement of transmission between experimental and the theoretic design.     

微喷气提高轴流压气机稳定性的研究

在动叶顶部采用稳态微量喷气可以在不影响低速轴流压气机的稳态工作特性下,拓宽其工作范围。为了分析微喷气作用机理,进行了一系列不同喷气结构的实验研究,包括不同喷气角,不同喷嘴安装位置以及不同喷气量.利用高频响动态传感器测量叶尖间隙动态压力谱,分析表明微量喷气可以改变叶尖顶部泄漏涡的轨迹.     

低速轴流压气机单转子旋转失速三维数值模拟和实验比较

本文通过求解三维不可压N-S方程,对三级低速轴流压气机第一级的孤立转子进行数值模拟,在出口加上节流阀进行了非定常计算,得到了失速先兆的特性,并且与压气机失速实验进行了比较。结果表明,计算与实验的特性线符合较好,单转子三维计算与压气机三级实验中第一级转子在失速先兆和失速团的特性一致。并且数值失速过程中动叶通道内部动态压力的变化与实验结果也很接近。     

用SPIV技术测量压气机转子尖区复杂流动

本文将数字式SPIV技术应用到低速大尺寸压气机实验台上,并在设计状态和近失速状态下,对转子槽道内叶尖区域多个截面内的三维瞬态速度场进行了成功测量。测量结果表明SPIV透过机匣视窗及即可直接测量旋涡和二次流的瞬态结构,而且能够解决多级压气机内部流场的测量.在压气机SPIV测量中,激光反光的控制和示踪粒子的均匀稳定散播是决定成败的关键因素。     

进口附面层厚度对弯叶片扩压叶栅损失的影响

本文通过人工加厚叶栅进口附面层厚度，考察了叶搬进口附面层厚度对弯叶片扩压叶栅损失的影响．实验结果表明，进口附面层厚度增加时，叶栅两端区二次流增强，叶栅损失增大．采用正弯曲叶片在参考进口附面层状态和人工加厚附面层时均未得到叶栅损失的降低，而反弯曲叶栅损失的降低出现在参考进口附面层状态下．