Selection of a Heat-Recovery Turbine Unit for a Self-Contained Power Supply of Compressor Stations in Gas Mains

IF 0.9 Q4 ENERGY & FUELS
V. E. Mikhailov, M. A. Vertkin, S. B. Esin, P. A. Kruglikov, D. A. Sobolev, Yu. G. Sukhorukov, L. A. Khomenok
{"title":"Selection of a Heat-Recovery Turbine Unit for a Self-Contained Power Supply of Compressor Stations in Gas Mains","authors":"V. E. Mikhailov, M. A. Vertkin, S. B. Esin, P. A. Kruglikov, D. A. Sobolev, Yu. G. Sukhorukov, L. A. Khomenok","doi":"10.1134/s0040601524030042","DOIUrl":null,"url":null,"abstract":"<h3 data-test=\"abstract-sub-heading\">Abstract</h3><p>Two design options for a heat-recovery turbine unit (HRTU), which generates electricity for self-contained power supply of gas mains’ compressor stations (GMCSs) using the heat of exhaust gases from gas-turbine engines (GTEs) driving gas-pumping units (GPUs), are examined. The working fluid of the recovery circuit is octafluorocyclobutane (c-C<sub>4</sub>F<sub>8</sub>, engineering name is RC318) in one of the two HRTUs and the exhaust gases of GPU GTE in the other HRTU. The HRTU operating on RC318 has a three-circuit cycle, including three turbines, three recuperative heat exchangers, three RC318 heaters, and one common condenser. An alternative design of HRTU is a vacuum-type GTU consisting of an overexpansion gas turbine, whose inlet is connected with the exhaust of GPU GTE, exhaust gas coolers, a cooled gas compressor, and an induced-draft fan. The excess power of this HRTU above the current power demand at the GMCS is used to create a vacuum at the exhaust of the gas turbine of the GPU GTE. The results are presented of the comparative balance calculations of parameters and characteristics of both HRTUs as applied to a 16-MW Ural GPU GTE. They were performed using the updated initial data and the software library RefProp (in the CoolProp high-level interface) for the calculation of thermodynamic parameters of working fluids. It has been demonstrated that a more compact and easier to implement gas-type HRTU (with an overexpansion gas turbine), although having a lower power than the RC318-type HRTU, can still fully cover the demand of the GMCS for high-quality power and also to solve the problem of substituting imported gas piston and diesel generators at the GMCS within the shortest possible time and with the lowest capital and operating expenditures.</p>","PeriodicalId":799,"journal":{"name":"Thermal Engineering","volume":null,"pages":null},"PeriodicalIF":0.9000,"publicationDate":"2024-04-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Thermal Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1134/s0040601524030042","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0

Abstract

Two design options for a heat-recovery turbine unit (HRTU), which generates electricity for self-contained power supply of gas mains’ compressor stations (GMCSs) using the heat of exhaust gases from gas-turbine engines (GTEs) driving gas-pumping units (GPUs), are examined. The working fluid of the recovery circuit is octafluorocyclobutane (c-C4F8, engineering name is RC318) in one of the two HRTUs and the exhaust gases of GPU GTE in the other HRTU. The HRTU operating on RC318 has a three-circuit cycle, including three turbines, three recuperative heat exchangers, three RC318 heaters, and one common condenser. An alternative design of HRTU is a vacuum-type GTU consisting of an overexpansion gas turbine, whose inlet is connected with the exhaust of GPU GTE, exhaust gas coolers, a cooled gas compressor, and an induced-draft fan. The excess power of this HRTU above the current power demand at the GMCS is used to create a vacuum at the exhaust of the gas turbine of the GPU GTE. The results are presented of the comparative balance calculations of parameters and characteristics of both HRTUs as applied to a 16-MW Ural GPU GTE. They were performed using the updated initial data and the software library RefProp (in the CoolProp high-level interface) for the calculation of thermodynamic parameters of working fluids. It has been demonstrated that a more compact and easier to implement gas-type HRTU (with an overexpansion gas turbine), although having a lower power than the RC318-type HRTU, can still fully cover the demand of the GMCS for high-quality power and also to solve the problem of substituting imported gas piston and diesel generators at the GMCS within the shortest possible time and with the lowest capital and operating expenditures.

Abstract Image

为天然气主管道中的压缩机站自备电源选择热回收涡轮机组
摘要 研究了热回收涡轮机组(HRTU)的两种设计方案,该热回收涡轮机组利用燃气涡轮发动机(GTE)驱动燃气泵组(GPU)产生的废气热量发电,为燃气总管压缩机站(GMCS)提供独立电源。两个 HRTU 中的一个回收回路的工作流体为八氟环丁烷(c-C4F8,工程名称为 RC318),另一个 HRTU 的工作流体为 GPU GTE 的废气。使用 RC318 的 HRTU 采用三回路循环,包括三个涡轮机、三个换热器、三个 RC318 加热器和一个普通冷凝器。HRTU 的另一种设计是真空型 GTU,由一台过膨胀燃气轮机(其进气口与 GPU GTE 的排气口相连)、废气冷却器、一台冷却气体压缩机和一台引风机组成。该 HRTU 超过 GMCS 当前功率需求的多余功率用于在 GPU GTE 燃气轮机排气口形成真空。本文介绍了应用于 16-MW Ural GPU GTE 的两种 HRTU 的参数和特性的比较平衡计算结果。计算使用了最新的初始数据和用于计算工作流体热力学参数的软件库 RefProp(CoolProp 高级界面)。结果表明,更紧凑、更易于实施的燃气型 HRTU(采用过膨胀燃气轮机)虽然功率低于 RC318 型 HRTU,但仍能完全满足 GMCS 对高质量电力的需求,并能在最短时间内以最低的资本和运营成本解决 GMCS 替代进口燃气活塞和柴油发电机的问题。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
CiteScore
1.30
自引率
20.00%
发文量
94
文献相关原料
公司名称 产品信息 采购帮参考价格
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信