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Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

机译:具有非人字形内表面的人字形的涡轮机喷嘴

摘要

A nozzle of a turbomachine is provided with chevrons with a non-axisymmetric inner face. A cover for the nozzle of longitudinal axis L-L includes an internal wall having a section with a predetermined abscissa on the L-L axis defining, on the wall, a neck line. The cover has, downstream from the abscissa, indentations in the trailing edge of the cover delimiting chevrons distributed in the circumferential direction, in which, on the cover, from the abscissa the internal wall moves away radially towards the outside of the upstream tangent, to the top of an indentation, the outer wall of the cover moves towards the upstream tangent to the top of an indentation, and the internal wall moves away radially towards the inside of the upstream tangent, to the tip of a chevron.
机译:涡轮机的喷嘴设置有具有非轴对称内表面的人字形。纵向轴线L-L的喷嘴的盖包括内壁,该内壁具有在L-L轴上具有预定横坐标的部分,该部分在壁上限定颈线。所述盖在横坐标的下游具有在盖的后缘中的凹痕,这些凹痕限定了沿周向分布的人字形,在该V形中,内壁从横坐标朝着上游切线的外侧径向地移开,以在凹痕的顶部,盖的外壁朝着凹痕的顶部向上游切线移动,而内壁朝着上游切线的内部向人字形尖端径向移动。

著录项

  • 公开/公告号GB201601112D0

    专利类型

  • 公开/公告日2016-03-09

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号GB20160001112

  • 发明设计人

    申请日2014-07-15

  • 分类号F02K1/34;F02K1/38;F02K1/46;

  • 国家 GB

  • 入库时间 2022-08-21 14:08:11

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