超声波－蒸汽蒸馏萃取技术富集沉积物样品中的氯代农药和多氯联苯

为方便快速分离沉积物中含氯农药和多氯联苯，将超声波技术和蒸汽蒸馏萃取技术相结合，萃取沉积物中的微量含氯农药和多氯联苯，所得萃取物不需进一步的净化和浓缩，可直接用于色谱分析．实验表明，在进行蒸汽蒸馏萃取之前，使用辅助的超声波技术可将大部分待测物的回收率提高２０％－３０％，较好地解决了由于沉积物的吸附作用而导致的蒸汽蒸馏萃取回收率偏低的缺陷．该法使沉积物样品中的氯代农药和多氯联苯的蒸汽蒸馏萃取富集成为可能．     

基于风险的检验在高温高压管廊蒸汽管道的应用

高含硫天然气净化装置高温高压管廊蒸汽管道由于不能停车,在现有技术条件下无法开展全面检验,存在安全运行的风险。简述了基于风险的检验技术的基本理念。讨论了蒸汽管道开展基于风险的检验的合规性、损伤模式及机理、风险评估方法和程序。通过综合考虑失效可能性和失效后果,制定最优检验策略并实施,解决了高温高压管廊蒸汽管道到期不能检验的问题,及时发现隐患并整改,确保管道合法合规安全运行。研究结果表明,采用基于风险的检验技术,既能节约大量的停车和检验维修费用,又能有效地提高重点设备管线的安全性和管理水平。     

汽轮机联锁保护在 DCS上的实现

阐述了汽轮机联锁保护的具体内容，并在此基础上根据需要给出了该联锁系统在DCS上的实现方法。     

用于燃料电池的甲醇水蒸气重整反应制氢的研究

研究了甲醇水蒸气重整制氢反应过程中各种因素对Cu／ZnO／Al2O3催化剂的活性和选择性的影响。结果表明：Cu／Zn比为2．0的催化剂在250℃反应时，催化剂效果较好，最合适反应条件是：压力0．1MPa，温度250℃，n(H2O)：n(CH3OH)=1．0-1．2，液体流速0．1mL／min。在Cu／ZnO／Al2O3)，催化剂上，甲醇水蒸气重整、甲醇分解和水气转换反应随反应条件的不同而发生相互抑制或促进作用。     

利用燃气轮机回收工业尾气

火炬瓦斯放空问题一直是石化行业的一个重点研究课题。我们经过不断地摸索、探讨，开发了燃气轮机回收火炬瓦斯的技术。采用燃气轮机回收火炬瓦斯，是消灭火炬的手段之一。介绍了燃气轮机的原理、流程及效果，在推广使用方面具有实用性。     

新型射汽抽气消声器

介绍了一种自行设计的、新型的汽轮机启动抽气器排汽消声装置，并对其结构原理和设计特点进行了较详细的叙述。应用实践表明，此种消声器降噪效果明显。     

主汽管噪声原因分析及处理对策

随着环保要求的日益严格，工业噪声作为一大污染源越来越受到人们的关注。通过对噪声产生机理的分析，确定了主汽管噪声的生成原因，介绍了几种降噪措施及其效果，对电厂管道设计和阀门选型具有借鉴意义。     

汽爆麦草固态发酵木质素酶

木质素是地球上主要的可再生芳香族化合物 ,是地球上仅次于纤维素的第二丰富可再生天然资源 ,然而 ,对它的利用研究却很少 ,是天然高分子中未开发的领城[1] .80年代初发现了木质素过氧化物酶 (ＬｉＰ) [2 ,3] 和锰过氧化物酶 (ＭｎＰ) [4 ] 以后 ,木质素酶和木质素生物降解研究取得了一定进展 .但木质素微生物转化降解研究中仍存在许多问题 .( 1)由于木质素酶解是一种非专一性的、以自由基为基础的链反应过程[5] .因此 ,木质素酶在化学工业、煤化学和环境保护方面具有很大的开发前景 .而现在木质素酶的生产大多用合成培养基 ,必需添加昂贵的…     

Performance improvement of airfoils for wind blade with the groove

This study was a basic one to explore how much the aerodynamic characteristics of wind blade improve. The extent of improvement according to the shapes of groove placed on the surface of airfoil (NACA0015) was analyzed through computational analysis. A commercial computational fluid dynamics (CFD) code, the ANSYS Fluent 13, was used in this study. In this study, regarding with the positions and shapes of groove, the end of groove was placed at a certain distance (length, l) from both the front and back of separation starting point, the depth and the width were designated as h and d respectively. Analysis was conducted at the 7° angle of attack under the following conditions; the thickness (δ) of boundary layer to the depth (h) of groove ratio (h/δ) 0.6–1.0, the depth (h) of groove to the width (d) of groove ratio (h/d) 0.1–1.4, and the length (l) between the end of groove and separation point to the thickness (δ) of boundary layer ratio (l/δ) ?0.5–0.5. Among these conditions, the best improvement of lift to drag ratio, standing at 15.3%, was under h/δ = 1.0, h/d = 0.12, and l/δ = –0.5 (7° AOA, Re = 360k). In addition, throughout the range of angle of attack, 2–14°, lift to drag ratio improved by 0.8%, 5.1%, 3.2%, and 1.8% each when Reynolds numbers were 280k, 360k, 450k, and 530k. It is also confirmed that the shape of groove contributed to recovering velocity around airfoil wall and the lift to drag ratio improvements by groove were maintained at the given range of Reynolds number and around the angle of attack, 7°.     

Experimental investigation of a 250-kW turbine organic Rankine cycle system for low-grade waste heat recovery

An organic Rankine cycle (ORC) is generally used for converting low-grade heat into electricity. In this study, an extensive literature survey was conducted to identify current research gaps on experimental ORC systems. Specifically, there is limited experimental data and limited details on thermal and expander efficiencies of ORC systems. In order to address these gaps, the objective of this study included developing a turbine ORC with a power output exceeding 50 kW and thermal efficiency exceeding 8% for a heat source temperature < 120°C. The experimental results indicated that the system achieved a net power output of 242.5 kW and a thermal efficiency of 8.3% (the highest value for a turbine ORC system for the heat source temperature below 120°C). Thus, the study addressed the gaps identified in the research area of ORCs.