on the other side 01 n the compressor to ensure equal return airflow paths. Even then some asymmetry still csistcd and this was found to be due to the support struts of the downstream pedestal (part 3, Fig, I). To reduce the interference ...
Two–dimensionalblade–to–bladeflowthroughcascadesofblades Empiricalperformancemodelsbasedontwodimensionalcascadetests Meridionalthroughflowanalysis;End–wallboundarylayeranalysis Aerodynamicperformanceanalysis Compressorstageaerodynamicdesign Multistageaxial–flowcompressoraerodynamicdesign ...
The axial flow compressor is the second type of dynamic compressor, whose general nature and capabilities were introduced in section 1.3. It absorbs energy from an external power source, raising the pressure of a continuous flow of working fluid by means of its blading geometry and motion. Downlo...
AXIAL-FLOW COMPRESSORPURPOSE: To reduce a loss in a blade row, and provide a highly efficient axial- flow compressor by improving a shape of a blade having a high subsonic speed or supersonic speed inlet flow.TSUDA YOSHIHIRO津田▲吉▼弘KATO YASUHIRO加藤 泰弘...
axial-flow compressor释义 [化] 轴流式压缩机 实用场景例句 全部 The paper analysis control requires of the axial flow compressor. 分析了轴流压缩机工况的控制要求和控制方案. 互联网 The effect of tip injection on the performance of an axial - flow compressor was performed numerically. 采用数值模拟方...
Rotating unit for an axial-flow compressor An axial-flow compressor has at least one stator vane row. At least one blade of the stator vane row is provided as a rotating unit (), with the rotating unit being completely rotatable about a drive axis to act as a rotary compressor an... ...
PURPOSE:To enlarge the stable operation range of an axial-flow compressor, by providing flow deflection plates concentrically to a rotor shaft up-stream to a vane train, supporting the plates rotatably relative to a casing, and providing a means for driving the plates. CONSTITUTION:In a multista...
AXIAL-FLOW COMPRESSOR 专利名称：AXIAL-FLOW COMPRESSOR 发明人：TAKAHASHI YASUO,高橋 康雄,MYOREN CHIHIRO,明連 千尋,KAWAMURA KOTA,川村 康 太 申请号：JP2017146809 申请日：20170728 公开号：JP2017190779A 公开日：20171019 专利内容由知识产权出版社提供 专利附图：摘要：PROBLEM TO BE SOLVED: To provide an ...
ig 1 onvergencehistoryofmassflowrate 流量误差波动比较大 计算步数超过 17 以后 流量误差仍可达到 1% 以下 O 到了 8 % 换算转速 9 1 第 1 期 刘前智 : 多级轴流压气机非设计性能的数值预估 的情况下 . 由于计算的流动状态偏离设计点比较 多 . 计算时流量误差要满足收敛标准所需的时间 步数大大增加 ...
United States Patent US3422625 Note: If you have problems viewing the PDF, please make sure you have the latest version ofAdobe Acrobat. Back to full text