Turbine assembly with detachable struts

A turbine assembly having an outer casing (36), an inner structural ring (38), and an annular gas path (42) defined between outer and inner flow path walls (44, 46) for conducting a gas flow through the turbine assembly. A plurality of structural struts (52) are spaced apart in a circumferential direction, each strut (52) including a strut body (52a) extending in a radial direction for supporting the inner structural ring (38) to the outer casing (36). A first strut end (64) at a radially outer end of the strut body (52a) is detachably attached to the outer casing (36) with a first fastener structure (68) engaging the outer casing (36), and a second strut end (66) at a radially inner end of the strut body (52a) is detachably attached to the inner structural ring (38) with a second fastener structure (70) engaging the inner structural ring (38). 种涡轮机组件，具有外部壳体（36）、内部结构环（38）以及用于引导气流通过所述涡轮机组件的限定在外流路壁和内流路壁（44、46）之间的环形气体路径（42）。多个结构支柱（52）沿周向方向隔开，每个支柱（52）包括沿径向方向延伸、用于将内部结构环（38）支撑到外部壳体（36）的支柱主体（52a）。处于支柱主体（52a）的径向外端处的第