首页> 外国专利> radial annular flane of a rotor or stator element, coupling of rotor or stator elements of a turbomachine and a turbomachine, such as a turnoreactor or a turboprop

radial annular flane of a rotor or stator element, coupling of rotor or stator elements of a turbomachine and a turbomachine, such as a turnoreactor or a turboprop

机译:转子或定子元件的径向环形叶片,涡轮机和涡轮机(例如,电抗器或涡轮螺旋桨发动机)的转子或定子元件的耦合

摘要

A radial annular flange of a rotor or stator element of a turbomachine including, at an inner/outer periphery, alternating solid portions and hollow portions, the solid portions including orifices for passing fastener bolts. The flange in the bottom of at least one hollow portion has a radius relative to the axis of the turbomachine that is less/greater than the radius of a circle that is tangential to the outsides/insides of the orifices for passing bolts through the solid portions.
机译:涡轮机的转子或定子元件的径向环形凸缘,其在内/外圆周上包括交替的实心部分和中空部分,实心部分包括用于使紧固件螺栓通过的孔。至少一个中空部分的底部中的凸缘相对于涡轮机的轴线的半径小于/大于与使螺栓穿过实心部分的孔的外侧/内侧相切的圆的半径。 。

著录项

  • 公开/公告号BRPI0912030A2

    专利类型

  • 公开/公告日2015-10-06

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号BR2009PI12030

  • 申请日2009-04-27

  • 分类号F01D5/02;F01D5/06;F01D25/24;

  • 国家 BR

  • 入库时间 2022-08-21 15:16:00

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