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 contains rotating stator blades. 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 1-2, 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: increased compressor's efficiency.;20 cl, 2 tbl, 3 dwg
机译:领域:机械工程;;实质:压缩机包含旋转的定子叶片。压缩机叶片具有基本符合X,Y和Z直角坐标系值的给定轮廓的空气动力学部分,该值出现在可缩放表中,该表选自表1-2,其中表X包括Y和Z直角坐标系是无量纲的值,可以通过将X,Y和Z直角坐标系乘以一个数来转换为距离。因此,X和Y表示其坐标,这些坐标通过连续的弧线连接,在每个高度Z处定义轮廓段的空气动力学部分。在每个高度Z处,截面空气动力学轮廓部分连接在一起以形成完整的空气动力学轮廓部分。 :提高压缩机效率。; 20 cl,2 tbl,3 dwg

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