首页> 外国专利> Pu00c1 for turbine eu00d3lica with low emission of noise in urban environment.

Pu00c1 for turbine eu00d3lica with low emission of noise in urban environment.

机译:涡轮e u00d3lica的P u00c1在城市环境中具有低噪音排放。

摘要

The present invention relates to a turbine eu00d3lica horizontal axis (1), with a root (7), one end (8), a leading edge (9), a trailing edge (10), a extradorso convex (11) and a soffit (12) cu00d4ncavo, convex or in the form of a the form of the 's'.It is characterized by construu00cdda with a single profile with modification of its line media to satisfy a load distribution profile along the axial cord of the pu00c1, with reduction of the peak pressure in the section of the pu00c1 to high angles of impact of flow and r. Pressure ecuperau00c7u00c3o smooth from the point of maximum suction and the trailing edge of the profile.This profile is constituu00cddo by sections (17) along the wingspan, built from a set of dimensionless coordinates, with a coefficient of maximum pressure of 1.5 and reduced emission of noise from aerodynamics.In the X / C and Y / C are dimensionless coordinates that correspond to the coordinates and dimensions of the profile of the section of the real pu00c1 divided by the length of the rope of the same 'C' used for the construction of a profile aerodinu00c2mico (17).
机译:涡轮机本发明涉及一种涡轮机,其水平轴(1)具有根部(7),一端(8),前缘(9),后缘(10),凸外凸(11)和一个拱腹(12)c u00d4ncavo,凸形或呈's'形式的形式,其特征是constru ucdcdda具有单个轮廓并对其线介质进行了修改,以满足沿轴向的载荷分布轮廓降低了p u00c1截面中的峰值压力,从而减小了流量和r的高冲击角度。从最大吸力点到型材的后缘,压力杯的表面光滑。此型材由翼展上的截面(17)组成,由一组无量纲坐标构建,具有最大压力系数降低了1.5并减少了空气动力学噪声的排放.X / C和Y / C是无量纲坐标,它们对应于实际p u00c1截面轮廓的坐标和尺寸除以绳索的长度用于构造剖面aerodin u00c2mico(17)的相同“ C”。

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