发明名称 Axial turbine with containment shroud
摘要 Various methods and systems are provided for an axial turbine including a containment shroud. In one example, an axial turbine for use in an engine system comprises a turbine disc/blisk and a shroud housing the turbine disc/blisk, the shroud including a first region, a second region, and a third region. A thickness of the second region is dependent on a length between the first region and the third region, and the third region has a burst strength that under a burst condition retains one or more fragments of the turbine disc/blisk.
申请公布号 US9546563(B2) 申请公布日期 2017.01.17
申请号 US201213440676 申请日期 2012.04.05
申请人 General Electric Company 发明人 Panambur Suresha Kumar;Prabhakar Nagamohan Govinahalli;Shankar Subramanya;Loringer Daniel;Johnson Lukas;Victor Andrew Theogift Jeyanth Selwyn
分类号 F01D21/04;F01D11/14;F01D25/24;F02C6/12 主分类号 F01D21/04
代理机构 Global Patent Operation 代理人 Kramer John A.;Global Patent Operation
主权项 1. An axial turbine for use in an engine system, comprising: a turbine element configured to move a shaft upon action of an exhaust stream; and a shroud housing the turbine element, the shroud comprising: a mounting region distal to the turbine element,a containment region,a transition region between the mounting region and the containment region, the containment region having a containment thickness proximal to the turbine element, the containment thickness at least as thick as a thickness of the transition region, anda bell-mouthed exhaust diffuser coupled to the containment region, where a thickness of the shroud decreases in a direction from the containment region to an end of the exhaust diffuser, the shroud further comprising an outer surface that includes an upper flat segment within the containment region and further includes curvature within the exhaust diffuser, an end of the exhaust diffuser level with the upper flat segment.
地址 Schenectady NY US