首页> 外国专利> Turbine i.e. low pressure turbine, distributor sector for turbomachine, has relaxing units each include slit with end that leads to curve portion shaped slit having shape of circle arc whose radius is ten times higher than thickness of slit

Turbine i.e. low pressure turbine, distributor sector for turbomachine, has relaxing units each include slit with end that leads to curve portion shaped slit having shape of circle arc whose radius is ten times higher than thickness of slit

机译:涡轮机,即低压涡轮机,涡轮机的分配器部分,具有松弛单元,每个松弛单元包括具有端部的狭缝,该狭缝的末端导致弯曲部分形状的狭缝,该狭缝具有圆弧形状,其半径比狭缝的厚度高十倍

摘要

The sector has a fixed blade (12) fixed between an outer platform (20) and an inner platform that includes a radial hook. The outer platform has upstream and downstream hooks (28, 30) for fixing the outer platform on a hood of a turbomachine, where the downstream hook includes free relaxing units (34). Each unit has a slit (36) with an open end (36a) and an end (36b) that is opposite to the open end. The end (36b) leads to a curve portion shaped slit (38) of the unit, where the slit (38) has a shape of a circle arc whose radius is ten times higher than thickness of the slit (36).
机译:该扇形具有固定的刀片(12),该刀片固定在外部平台(20)和包括径向钩的内部平台之间。外部平台具有上游和下游钩(28、30),用于将外部平台固定在涡轮机的机罩上,其中下游钩包括自由松弛单元(34)。每个单元具有狭缝(36),该狭缝(36)具有开口端(36a)和与开口端相对的端部(36b)。端部(36b)通向单元的弯曲部分形状的狭缝(38),其中狭缝(38)具有圆弧形状,其半径比狭缝(36)的厚度高十倍。

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