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实用新型
CN203670007U 具有翼型件的过渡管以及用于涡轮机的热气体路径组件 失效 - 权利终止

具有翼型件的过渡管以及用于涡轮机的热气体路径组件
摘要：
本实用新型涉及一种具有翼型件的过渡管以及用于涡轮机的热气体路径组件，提供了过渡管、热气体路径组件、以及涡轮机。一种热气体路径组件包括外部支承环、内部支承环、以及联接到外部支承环和内部支承环的过渡管。该过渡管包括管道，该管道限定了在进口与出口之间延伸的通路。进口和出口大体沿纵向轴线对准。该过渡管还包括翼型件，该翼型件布置于管道内并且被构造成改变热气体流方向。
摘要（英）：

The utility model relates to a transition pipe provided with airfoil profile pieces and a hot gas path assembly used for a turbine, and provides the transition pipe, the hot gas path assembly and the turbine. The hot gas path assembly comprises an external bearing ring, an internal bearing ring and the transition pipe connected to the external bearing ring and the internal bearing ring, wherein the transition pipe comprises a pipeline limiting a channel extended between an inlet and an outlet; the inlet and the outlet are aligned along the longitudinal axis approximately; and the transition pipe further comprises the airfoil profile pieces which are distributed in the pipeline and is structured to change the hot gas flow direction.

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