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COMPRESSOR VANE, METHOD OF PRODUCTION AND COMPRESSOR VANE APPLICATION

机译:压缩机叶片,生产方法和压缩机叶片的应用

摘要

FIELD: motors and pumps.;SUBSTANCE: invention relates to the compressor (9) vanes (50), which are provided with tailpiece (55), platform (59) and adjoining vane profile (61) with profile end along the main axis. The vane profile (61) is made up with convex wall (69) from the suction side and perpendicular to the wall (69) from the side of concave wall (67) at pressure side. With regard to flow medium, the above surfaces stretch from inlet edge (63) to outlet edge (65) and middle line (71) of profile is in-between. The end surface (73) stretches crosswise with regard to the main axis (53) on the end (72) of profile. Packing bevel (75) is available, at least, partially, on the end surface from the inlet edge (63) to outlet edge (65). The vane profile (61) is also available on the end surface, including packing bevel (74). The vane profile (61) has vane profile height (H), which goes along the main axis (53) direction. In order to produce efficient and improved from aerodynamics point of view compressor vane with the modified packing bevel with unchangeable packing action, it is proposed to reduce packing bevel (74) height (HL) by 2% from the vane profile (61) height (H).;EFFECT: efficient and improved from aerodynamics point of view compressor vane.;9 cl, 3 dwg
机译:技术领域本发明涉及压缩机(9)的叶片(50),其具有尾翼(55),平台(59)和邻接的叶片轮廓(61),其轮廓末端沿着主轴线。叶片轮廓(61)由从吸入侧起的凸壁(69)构成,并从压力侧的凹壁(67)侧垂直于壁(69)。关于流动介质,上述表面从入口边缘(63)延伸到出口边缘(65),并且轮廓的中线(71)在它们之间。端面(73)在型材的端部(72)上相对于主轴线(53)横向延伸。在从入口边缘(63)到出口边缘(65)的端面上,至少部分有填充斜面(75)。叶片轮廓(61)也可在端面上使用,包括填料斜角(74)。叶片轮廓(61)具有沿主轴(53)方向延伸的叶片轮廓高度(H)。为了从空气动力学的角度出发生产高效且改进的压缩机叶片,其具有经过修改的填料斜角且具有不可改变的填料作用,建议将填料斜角(74)的高度(HL)从叶片轮廓(61)的高度降低2%( H).;效果:从空气动力学的角度来看高效且经过改进的压缩机叶片; 9 cl,3 dwg

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