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Computer program describing turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for a two stage axial flow turbine

机译：描述涡轮空气动力学要求，近似外部叶片几何形状和两级轴流式涡轮机的冷却剂流量要求的计算机程序

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摘要

Computer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbine

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作者
Evans, D. G.; Furgalus, K. A.; Vanco, M. R.;
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年度 1971
页码 1-61
总页数 61
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; AXIAL FLOW TURBINES; COMPUTER AIDED DESIGN; COMPUTER PROGRAMS; THERMODYNAMIC PROPERTIES; TWO STAGE TURBINES; AIR COOLING; MATHEMATICAL MODELS; TIP SPEED; TURBINE BLADES;

机译：空气动力学特征;轴流式涡轮机;计算机辅助设计;电脑程序;热力学性质;两级涡轮;空气冷却;数学模型;提示速度; TURBINE BLaDEs;

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专利

1. Fully Cooled Single Stage HP Transonic Turbine-Part Ⅰ: Influence of Cooling Mass Flow Variations and Inlet Temperature Profiles on Blade Internal and External Aerodynamics [J] . C. W. Haldeman, M. G. Dunn, R. M. Mathison Journal of turbomachinery . 2012,第3期

机译：完全冷却的单级高压跨音速涡轮机-第一部分：冷却质量流量变化和进气温度曲线对叶片内部和外部空气动力学的影响
2. Aerodynamics of Tip Leakage Flows Near Partial Squealer Rims in an Axial Flow Turbine Stage [J] . Cengiz Camci, Debashis Dey, Levent Kavurmacioglu Journal of turbomachinery . 2005,第1期

机译：轴流式水轮机阶段部分阻风门边缘附近的尖端泄漏流的空气动力学
3. Visualization and Analysis of Supersonic Flow in Rotating Turbine Stage (3rd Report, Influence of a Supersonic Turbine Stage on Flows of Subsequent Stationary Blades) [J] . Masashi Akiba, Tadashi Tanuma, Kenichiro Mochizuki 日本機械学会論文集. B編 . 1997,第605期

机译：涡轮级超音速流的可视化和分析（第三次报告，超音速级对后续固定叶片流的影响）
4. Effect of Rim Seal Purge Flow on the Aerodynamic Performance of Turbine Stage and Cooling Effectiveness of Rotor Blade Endwall Part I: Coolant Flow Rate [C] . Jun LI, Qing GAO, Zhigang LI, International Symposium on Air Breathing Engines . 2017

机译：边缘密封吹扫流动对转子叶片胎筒阶段空气动力学性能的影响及转子叶片端包件I的冷却效果I：冷却剂流速
5. An Investigation of Using Tip Leakage Interrupter and Blade Slit to Mitigate Aerodynamic Losses in Axial Turbine Stage [D] . ?Andichamy, Veerandra Chakkaravarthy 2019

机译：使用尖端泄漏断路器和刀片切口的研究，以减轻轴向汽轮机阶段的气动损失
6. Effect of Various Coolant Mass Flow Rates on Sealing Effectiveness of Turbine Blade Rim Seal at First Stage Gas Turbine Experimental Facility [O] . Seok Min Choi, Seungyeong Choi, Hyung Hee Cho 2020

机译：各种冷却剂质量流速对第一阶段燃气轮机实验设施涡轮叶片边缘密封密封有效性的影响
7. Computer Program Describing Turbine Aerodynamic Requirements, Approximate External Blade Geometries, and Coolant Flow Requirements for a Two Stage Axial Flow Turbine [R] . Evans, D. G., Furgalus, K. A., Vanco, M. R. 1971

机译：计算机程序描述两级轴流式涡轮机的涡轮机空气动力学要求，近似外部叶片几何形状和冷却剂流量要求

Computer program describing turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for a two stage axial flow turbine

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