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Cover turbine nozzle patterned for noise reduction jet nozzle and associated turbine.

机译:盖上为降低噪音的喷嘴设计的涡轮喷嘴和相关的涡轮。

摘要

Annular cover (14, 16) for a turbine nozzle having a plurality of patterns (26) arranged in the extension of a trailing edge (14a, 16a) of said shell and circumferentially spaced apart, each drawing substantially a form quadrilateral with a base (28) formed by a portion of the trailing edge of the cover and two vertices (30a, 30b) spaced downstream from the base and spliced ​​thereto by two sides (32a, 32b), each drawing asymmetrical with respect to a median plane (P) of the drawing passing through a longitudinal axis (XX) of said casing and having a first portion (34a) inclined radially inwardly of the cover and a second part (34b) inclined radially outwardly of the cover, characterized in that the sides (30a, 30b) each have a drawing substantially parabolic shape.
机译:用于涡轮机喷嘴的环形盖(14、16),其具有多个布置在所述壳体后缘(14a,16a)的延伸部分中的图案(26),并在圆周方向上隔开一定距离,每个图案都与底面大致呈四边形( 28)由盖的后缘的一部分和两个顶点(30a,30b)组成,这些顶点与底部下游间隔开,并通过两侧(32a,32b)拼接在一起,每个侧面相对于中间平面(图中的P)穿过所述壳体的纵轴(XX),并具有从盖径向向内倾斜的第一部分(34a)和从盖径向向外倾斜的第二部分(34b),其特征在于,侧面( 30a,30b)分别具有基本为抛物线的形状。

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