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Preliminary performance of a Brayton-cycle- power-system gas loop operating with krypton over a turbine inlet temperature range of 1200 F to 1600 F

机译：布雷顿循环动力系统气体回路的初步性能，使用氪气在1200 F至1600 F的涡轮机入口温度范围内运行

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摘要

Brayton cycle power system gas loop operating with krypton over turbine inlet temperature of 1200 F to 1600 F

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作者
Asadourian, A. S.; Hecker, T. P.; Kruchowy, R.; Macosko, R. P.; Valerino, A. S.;
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年度 1970
页码 1-41
总页数 41
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BRAYTON CYCLE; KRYPTON; TURBINES; COMPRESSOR EFFICIENCY; HEAT EXCHANGERS; HIGH TEMPERATURE TESTS;

机译：布雷顿循环;氪;汽轮机。压缩机效率;换热器;高温测试;

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1. Effect of Operating Parameters and Compressor Inlet Temperature on Exergetic Performance of an In-service Gas-Turbine Plant [J] . F. I. Abam, D. C. Onyejekwe, G. O. Unachukwu International Journal of Applied Engineering Research . 2010,第16期

机译：操作参数和压缩机入口温度对役燃气轮机厂锻炼性能的影响
2. Operating Experience milestone in gas turbine inlet cooling: Tractebel Power's Ripon facility has operated an inlet air cooling system designed by Kohlenberger-KACE Energy Corp. for eighteen months [J] . Don Adams Turbomachinery International . 1998,第7期

机译：燃气轮机进气冷却的操作经验里程碑：Tractebel Power的Ripon工厂已经运行了由Kohlenberger-KACE Energy Corp.设计的进气冷却系统。
3. Performance evaluation of the 100kW automotive ceramic gas turbine at the turbine inlet gas temperature of 1350℃ [J] . Ogita Hirosi, Takahasi Masayuki, Kawaguchi Yoshihiro Bulletin of GTSJ . 2000,第2000期

机译：100kW汽车陶瓷燃气轮机在涡轮进气温度为1350℃时的性能评估
4. CFD BASED ANALYSIS OF BURNER FUEL AIR MIXING OVER A RANGE OF AIR INLET AND FUEL PRE-HEAT TEMPERATURES FOR A SIEMENS V94.3A GAS TURBINE BURNER [C] . O.R Darbyshire, C.W Wilson, A. Evans, ASME(American Society of Mechanical Engineers) Turbo Expo vol.1; 20060506-11; Barcelona(ES) . 2006

机译：基于CFD的西门子V94.3A燃气轮机燃烧器在进气孔和燃油预热温度范围内的燃烧器空气混合
5. Experimental and computational investigation of inlet temperature profile and cooling effects on a one and one-half stage high-pressure turbine operating at design-corrected conditions. [D] . Mathison, Randall Melson. 2009

机译：在设计校正的条件下运行的一台和半台高压涡轮机的入口温度曲线和冷却效果的实验和计算研究。
6. FEM Modeling of the Temperature Influence on the Performance of SAW Sensors Operating at GigaHertz Frequency Range and at High Temperature Up to 500 °C [O] . Jean Claude Asseko Ondo, Eloi Jean Jacques Blampain, Gaston N’Tchayi Mbourou, 2020

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7. Effect of Turbine and Compressor Inlet Temperatures and Air Bleeding on the Comparative Performance of Simple and Combined Gas Turbine Unit [O] . Basharat Salim, Jamal Orfi, Shaker Saeed Alaqel 2020

机译：汽轮机和压缩机入口温度和空气流出对简单燃气机组的比较性能的影响
8. Preliminary Performance of a Brayton-Cycle- Power-System Gas Loop Operating with Krypton over a Turbine Inlet Temperature Range of 1200 F to 1600 F [R] . Asadourian, A. S., Hecker, T. P., Kruchowy, R., 1970

机译：布雷顿循环动力系统气体回路的初步性能，使用氪气在1200°F至1600°F的涡轮机进气温度范围内运行

Preliminary performance of a Brayton-cycle- power-system gas loop operating with krypton over a turbine inlet temperature range of 1200 F to 1600 F

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