首页> 外国专利> COMPRESSOR BLADE, WHICH HAS AERODYNAMIC PRESET PROFILE PART, COMPRESSOR BLADE, WHICH HAS AERODYNAMIC PART WITH THE SIDE OF LOW-PRESSURE PRESET PROFILE AND COMPRESSOR

COMPRESSOR BLADE, WHICH HAS AERODYNAMIC PRESET PROFILE PART, COMPRESSOR BLADE, WHICH HAS AERODYNAMIC PART WITH THE SIDE OF LOW-PRESSURE PRESET PROFILE AND COMPRESSOR

机译:具有气动预设轮廓的压缩机叶片,具有低压预设轮廓和压缩机的气动叶片

摘要

FIELD: machine engineering.;SUBSTANCE: compressor blade has an aerodynamic part of the given profile substantially in accordance with the values of X, Y and Z Cartesian coordinate system, presented in a scalable table, selected from the group of tables consisting of Tables 1-11, in which the X, Y, and Z Cartesian coordinate system are dimensionless values given to convert into the distance by multiplying the dimensional values X, Y, and Z Cartesian coordinate system into a number. Thus X and Y represent coordinates of which, being connected by continuous arcs, define the aerodynamic portion of the profile section at each height Z. Sections aerodynamic profile portion are joined together at each height Z to form a complete aerodynamic profile part.;EFFECT: increase overall efficiency, reduced vibration and improved load-bearing capacity of the wind.;20 cl, 11 tbl, 3 dwg
机译:领域:机械工程;实质:压缩机叶片具有给定轮廓的空气动力学部分,基本上符合X,Y和Z直角坐标系的值,并以可缩放的表格形式显示,该表格选自由表1组成的表格组-11,其中X,Y和Z笛卡尔坐标系是无量纲值,通过将X,Y和Z笛卡尔坐标系的维数乘以一个整数来转换为距离。因此X和Y代表其坐标,这些坐标通过连续弧线连接,在每个高度Z处定义轮廓截面的空气动力学部分。截面空气动力学轮廓部分在每个高度Z处连接在一起以形成完整的空气动力学轮廓部分。提高整体效率,减少振动并提高风的承载能力。; 20 cl,11 tbl,3 dwg

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