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

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, formed substantially in accordance with the values ​​of X, Y and Z Cartesian coordinates given in Table scalable selected from the group consisting of Tables 1-11, in which the values ​​of X, Y and Z Cartesian coordinate system are dimensionless values ​​given to convert into a dimensional distance by multiplying the values ​​of X, Y and Z Cartesian coordinate system into a number, and the coordinates X and Y represent coordinates koto rye, being connected continuing arcs, define the airfoil profile section portion at each height Z, wherein the sectional profile of the airfoil portion at each height Z are joined together 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 rotor blade, designed 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 20 inches (2.54 cm to 50.8 cm) .7. The finished product, having AER
机译:1.成品具有空气动力学轮廓的预定部分,基本上根据表可缩放的表中给出的X,Y和Z直角坐标的值形成,选自表1-11,其中表1-11 X,Y和Z笛卡尔坐标系是无量纲值,通过将X,Y和Z笛卡尔坐标系的值乘以一个数字来转换成尺寸距离。坐标X和Y表示坐标相连的连续圆弧的黑麦黑麦在每个高度Z处定义了机翼轮廓截面部分,其中在每个高度Z处的机翼部分截面轮廓连接在一起以形成完整的机翼形状形状。 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,包括设计用于kompressorom.4的转子叶片。 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20英寸(2.54cm至50.8cm).7。成品,具有AER

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号