首页> 外国专利> ARTICULATED TRANSITION DUCT IN TURBOMACHINE, WHERE THIS INVENTION WAS MADE WITH GOVERNMENT SUPPORT UNDER CONTRACT NUMBER DE-FC26-05NT42643 AWARDED BY DEPARTMENT OF ENERGY AND GOVERNMENT HAS CERTAIN RIGHTS IN THIS INVENTION

ARTICULATED TRANSITION DUCT IN TURBOMACHINE, WHERE THIS INVENTION WAS MADE WITH GOVERNMENT SUPPORT UNDER CONTRACT NUMBER DE-FC26-05NT42643 AWARDED BY DEPARTMENT OF ENERGY AND GOVERNMENT HAS CERTAIN RIGHTS IN THIS INVENTION

机译:在涡轮机中的过渡过渡管道中,本发明是根据能源和政府部门授予的合同号DE-FC26-05NT42643给予政府支持的,在该发明中拥有某些权利

摘要

PROBLEM TO BE SOLVED: To provide combustor sections and transition ducts thereof which allow and accommodate thermal growth of the ducts.SOLUTION: Turbine systems 10 are provided. A turbine system comprises a transition duct comprising an inlet, an outlet, and a duct passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The duct passage includes an upstream portion and a downstream portion. The upstream portion extends from the inlet between an inlet end and an aft end. The downstream portion extends from the outlet between an outlet end and a head end. The turbine system further includes a joint coupling the aft end of the upstream portion and the head end of the downstream portion together. The joint is configured to allow movement of the upstream portion and the downstream portion relative to each other about or along at least one axis.
机译:要解决的问题:提供燃烧器部分及其过渡管道,以允许并适应管道的热增长。解决方案:提供了涡轮机系统10。涡轮机系统包括过渡管道,该过渡管道包括入口,出口以及在入口和出口之间延伸并限定纵向轴线,径向轴线和切向轴线的管道通道。过渡导管的出口沿纵向轴线和切线轴线从入口偏移。管道通道包括上游部分和下游部分。上游部分在入口端和后端之间从入口延伸。下游部分从出口在出口端和头端之间延伸。涡轮系统还包括将上游部分的后端和下游部分的头端联接在一起的接头。接头构造成允许上游部分和下游部分绕着或沿着至少一个轴线相对于彼此移动。

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