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Single-Stage Axial Compressor Component Development for Small Gas Turbines. Volume III. Supersonic Compressor Stage Development

机译：小型燃气轮机单级轴流压缩机组件开发。第三卷。超音速压缩机级开发

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The report describes the development of the complete stage for the 2.8:1 supersonic axial compressor design. The performance of the overall stage including the exit stators and interconnecting duct was evaluated through experimental testing with the rotor and inlet guide vanes developed under the previous phase of this program. The experimental results are analyzed and compared with the design data and criteria for each of the blade rows as well as the overall stage. (Author)

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Muller, C. H.; Cox, L. R.;
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年度 1969
页码 p.1-132
总页数 132
原文格式 PDF
正文语种 eng
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关键词
Gas turbines ; Axial-flow compressors ; design ; Axial-flow turbine rotors ; Gas turbine blades ; Configuration ; Geometry ; Manufacturing methods ; Tolerances(Mechanics) ; Duct inlets ; Supersonic flow ; Test methods;

机译：燃气轮机;轴流式压缩机;设计;轴流式涡轮转子;燃气轮机叶片;结构;几何;制造方法;公差（机械）;管道入口;超音速流动;试验方法;

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2. Investigation of the effect of roughness of duct surfaces of a supersonic high-pressure stage of an axial compressor on its characteristics [J] . Inozemtsev A. A., Plotnikov A. I. Journal of Applied Mechanics and Technical Physics . 2015,第2期

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3. ASSESSMENT OF THE PROSPECTS OF DEVELOPMENT OF MEDIUM-PRESSURE SINGLE-STAGE PISTON COMPRESSOR UNITS [J] . V. L. Yusha, S. S. Busarov, A. Yu. Gromov Chemical and Petroleum Engineering . 2017,第7a8期

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4. Understanding of an Effect of Plenum Volume of a Low Porosity Bend Skewed Casing Treatment on the Performance of Single-Stage Transonic Axial Flow Compressor [C] . Darshan P. Pitroda, Dilipkumar Bhanudasji Alone, Harish S. Choksi National Aerospace Propulsion Conference . 2021

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5. Experimental investigation of the flow field in a transonic, axial flow compressor with respect to the development of blockage and loss [D] . Suder, Kenneth Lee 1996

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6. Development of a PVDF Sensor Array for Measurement of the Dynamic Pressure Field of the Blade Tip in an Axial Flow Compressor [O] . Jiqing Cong, Jianping Jing, Changmin Chen, 2019

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7. The Development of Supersonic Axial Compressor Boost Stages for Small Gas Turbines [O] . C. H. Muller, A. Sabatiuk 1969

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Single-Stage Axial Compressor Component Development for Small Gas Turbines. Volume III. Supersonic Compressor Stage Development

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