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Finished products having aerodynamic often wonder profile of the finished product, having aerodynamic parts on the LOW PRESSURE preset profiles, and a compressor

机译:具有空气动力学性能的成品通常会询问最终产品的轮廓,在LOW PRESSURE预设轮廓上具有空气动力学部件的部件以及压缩机

摘要

1. The finished product having the predetermined part of the aerodynamic profile substantially in accordance with the values ​​of X, Y and Z Cartesian coordinates given in Table 1, scalable, in which the values ​​X, Y and Z Cartesian coordinate system are dimensionless values ​​that can be transformed into dimensional distance by multiplying the specified values ​​X, Y and Z into a number, and the coordinates X and Y represent coordinates of which being connected continuing arcs, define airfoil profile sections at parts each height Z, wherein the airfoil section of the profile at each height Z smoothly connected to each other to form a complete airfoil shape chasti.2. The finished product according to claim 1, comprising an aerodynamic chast.3. The finished product according to claim 1, comprising a guide vane outlet, intended for use with kompressorom.4. The finished product according to claim 1, wherein the shape of the airfoil portion lies in an envelope within at least one of: +/- 5% of the chord length in a direction perpendicular to the place of the aerodynamic surface portion; and +/- 0.25 inches (6.35 mm) in a direction perpendicular to the place chasti.5 aerodynamic surface. The finished product according to claim 1, wherein the number used to convert dimensionless values ​​in the dimensional distance is at least one of a fraction, a decimal fraction, integer and mixed chislo.6. The finished product according to claim 1, whose height is approximately 1 inch to 15 inches (2.54 cm to 38.1 cm) .7. The finished product having a portion with reduced aerodynamic pressure side of a predetermined profile on susches
机译:1.成品具有基本上符合表1中给出的X,Y和Z笛卡尔坐标值的空气动力学轮廓的预定部分,其中X,Y和Z笛卡尔坐标系的值是无量纲值,可以通过将指定值X,Y和Z乘以一个数字来转换成尺寸距离,并且坐标X和Y表示连接连续弧的坐标,分别在零件上定义翼型轮廓截面高度Z,其中轮廓的翼型截面在每个高度Z处彼此平滑连接,以形成完整的翼型形状。 2.根据权利要求1所述的成品,其特征在于,所述成品具有空气动力。 2.根据权利要求1所述的成品,其特征在于,包括用于kompressorom.4的导向叶片出口。 2.根据权利要求1所述的成品,其特征在于,所述翼型部分的形状位于在与所述空气动力学表面部分的位置垂直的方向上的弦长的+/- 5%的至少其中之一内的包络中;在垂直于位置5空气动力学表面的方向上+/- 0.25英寸(6.35毫米)。 2.根据权利要求1所述的成品,其特征在于,用于在尺寸距离中转换无量纲值的数是小数,小数,整数和混合数的至少其中之一.6。 2.根据权利要求1所述的成品,其高度为约1英寸至15英寸(2.54cm至38.1cm).7。成品具有在基座上具有预定轮廓的减小的气动压力侧的部分

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