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用于天然气液体回收和液化天然气的制冷新工艺一一混合冷剂制冷循环 被引量:2
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作者 王志强 《石油与天然气化工》 CAS 1988年第3期31-35,共5页
一、前言混合冷剂制冷是对单一纯组份制冷和阶式制冷而言.热力学分析表明,在天然气液体回收和液化天然气装置上使用混合冷剂制冷,改善了能量的利用,不仅效率高、简单、而且易于控制和实现整个工艺操作的最佳化. 自第一套混合冷剂制冷循... 一、前言混合冷剂制冷是对单一纯组份制冷和阶式制冷而言.热力学分析表明,在天然气液体回收和液化天然气装置上使用混合冷剂制冷,改善了能量的利用,不仅效率高、简单、而且易于控制和实现整个工艺操作的最佳化. 自第一套混合冷剂制冷循环装置于六十年代末在利比亚建成以来,混合冷剂的工艺流程和设备制造有了很大的发展.美国气体及化学产品公司、西德林德公司和法国液态空分公司在液化天然气装置的方案设计上,都采用混合冷剂制冷流程.目前世界上已建成几十套采用混合冷剂制冷的循环装置,并已投入使用. 展开更多
关键词 天然气液体回收 液化天然气 制冷 新工艺 混合冷剂 制冷循环
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世界天然气和天然气液体原始可采储量及最大可采资源量估算表
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作者 彭立纯 《中国海上油气(地质)》 1989年第2期48-48,共1页
关键词 世界 天然气 天然气液体 原始可采储量 最大可采资源量 估算表
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21世纪的天然气合成液体烃技术和市场前景
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作者 李建雄 《山东工业技术》 2019年第5期78-78,共1页
本文首先对我国现有技术和工厂情况进行了详细的分析,然后对21世纪的天然气合成液体烃技术和市场前景进行了相关探讨,希望能够对相关人员有所帮助。
关键词 21世纪 天然气合成液体烃技术 市场前景
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超低温截止阀阀杆的技术改进 被引量:1
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作者 陆孝绍 《石油化工自动化》 CAS 2018年第3期82-83,86,共3页
超低温截止阀广泛应用于石油石化撬装系统和液态天然气(LNG),其运行的稳定性直接影响低温工况下的整体管道乃至撬装系统的运行效率。超低温截止阀密封结构和阀杆之间的摩擦系数,直接影响到整个撬装系统的寿命。在某低温撬装项目中,通过... 超低温截止阀广泛应用于石油石化撬装系统和液态天然气(LNG),其运行的稳定性直接影响低温工况下的整体管道乃至撬装系统的运行效率。超低温截止阀密封结构和阀杆之间的摩擦系数,直接影响到整个撬装系统的寿命。在某低温撬装项目中,通过对超低温截止阀阀杆的技术改进,解决了超低温截止阀在使用过程中出现的微泄漏问题,取得了良好的效果。 展开更多
关键词 超低温阀 撬装系统 深冷处理 液体天然气
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Flow Pattern and Pressure Fluctuation of Severe Slugging in Pipeline-riser System 被引量:12
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作者 罗小明 何利民 马华伟 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2011年第1期26-32,共7页
During the exploitation of offshore oil and gas,it is easy to form severe slugging which can cause great harm in the riser connecting wellheads and offshore platform preprocessing system.The flow pattern and pressure ... During the exploitation of offshore oil and gas,it is easy to form severe slugging which can cause great harm in the riser connecting wellheads and offshore platform preprocessing system.The flow pattern and pressure fluctuation of severe slugging were studied in an experimental simulation system with inner diameter of 0.051 m.It is found that severe slugging can be divided into three severe slugging regimes:regime I at low gas and liquid flow rates with large pressure fluctuation,intermittent flow of liquid and gas in the riser,and apparent cutoff of liquid phase,regime II at high gas flow rate with non-periodic fluctuation and discontinuous liquid outflow and no gas cutoff,regime III at high liquid flow rate with degenerative pressure fluctuation in form of relatively stable bubbly or plug flow.The results indicate that severe slugging still occurs when the declination angle of pipeline is 0,and there are mainly two kinds of regimes:regime I and regime II.As the angle increases,the formation ranges of regime I and regime III increase slightly while that of regime II is not affected.With the increase of gas superficial velocity and liquid superficial velocity,the pressure fluctuation at the bottom of riser increases initially and then decreases.The maximum value of pressure fluctuation occurs at the transition boundary of regimes I and II. 展开更多
关键词 multiphase flow severe slugging pipeline-riser system flow regime pressure fluctuation
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COSMO-RS: An ionic liquid prescreening tool for gas hydrate mitigation
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作者 Cornelius B.Bavoh Bhajan Lal +3 位作者 Omar Nashed Muhammad S.Khan Lau K.Keong Mohd.Azmi Bustam 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2016年第11期1619-1624,共6页
Recently ionic liquids(ILs) are introduced as novel dual function gas hydrate inhibitors. However, no desired gas hydrate inhibition has been reported due to poor IL selection and/or tuning method. Trial & error a... Recently ionic liquids(ILs) are introduced as novel dual function gas hydrate inhibitors. However, no desired gas hydrate inhibition has been reported due to poor IL selection and/or tuning method. Trial & error as well as selection based on existing literature are the methods currently employed for selecting and/or tuning ILs. These methods are probabilistic, time consuming, expensive and may not result in selecting high performance ILs for gas hydrate mitigation. In this work, COSMO-RS is considered as a prescreening tool of ILs for gas hydrate mitigation by predicting the hydrogen bonding energies(E_(HB)) of studied IL inhibitors and comparing the predicted E_(HB) to the depression temperature(?) and induction time. Results show that, predicted EHBand chain length of ILs strongly relate and significantly affect the gas hydrate inhibition depression temperature but correlate moderately(R = 0.70) with average induction time in literature. It is deduced from the results that, ? increases with increasing IL EHBand/or decreases with increasing chain length. However, the cation–anion pairing of ILs also affects IL gas hydrate inhibition performance. Furthermore, a visual and better understanding of IL/water behavior for gas hydrate inhibition in terms of hydrogen bond donor and acceptor interaction analysis is also presented by determining the sigma profile and sigma potential of studied IL cations and anions used for gas hydrate mitigation for easy IL selection. 展开更多
关键词 Gas hydrates COSMO-RS Hydrogen bonding energies Ionic liquids Tuning
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Conceptual Design for a Kerosene Fuel-rich Gas-generator of a Turbopump-fed Liquid Rocket Engine 被引量:3
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作者 Min Son Jaye Koo +1 位作者 Won Kook Cho Eun Seok Lee 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第5期428-434,共7页
A design method for a kerosene fuel-rich gas-generator of a liquid rocket engine using turbopumps to supply propellant was performed at a conceptual level. The gas-generator creates hot gases, enabling the turbine to ... A design method for a kerosene fuel-rich gas-generator of a liquid rocket engine using turbopumps to supply propellant was performed at a conceptual level. The gas-generator creates hot gases, enabling the turbine to operate the turbopumps. A chemical non-equilibrium analysis and a droplet vaporization model were used for the estimation of the burnt gas properties and characteristic chamber length. A premixed counter-flow flame analysis was performed for the prediction of the burnt gas properties, namely the temperature, the specific heat ratio and heat capacity, and the chemical reaction time. To predict the vaporization time, the Spalding model, using a single droplet in convective condition, was used. The minimum residence time in the chamber and the characteristic length were calculated by adding the reaction time and the vaporization time. Using the characteristic length, the design methods for the fuel-rich gas-generator were established. Finally, a parametric study was achieved for the effects of the O/F ratio, mass flow rate, chamber pressure, initial droplet temperature, initial droplet diameter and initial droplet velocity. 展开更多
关键词 Liquid rocket engine Conceptual design Fuel-rich gas-generator Sensitivity analysis
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