发明名称 TURBINE ALIGNMENT CONTROL SYSTEM AND METHOD
摘要 A turbine that includes a rotor, an inner turbine shell, an outer turbine shell, and a sliding engagement between the inner turbine shell and the outer turbine shell. The inner turbine shell is a single piece construction that completely surrounds at least a portion of the rotor, and the outer turbine shell surrounds the inner turbine shell. A method for aligning turbine components that includes aligning a single-piece inner turbine shell substantially concentric with a rotor and surrounding the single-piece inner turbine shell with an outer turbine shell. The method further includes supporting the single-piece inner turbine shell with respect to the outer turbine shell using a bearing assembly between the single-piece inner turbine shell and the outer turbine shell.
申请公布号 US2011255959(A1) 申请公布日期 2011.10.20
申请号 US20100760804 申请日期 2010.04.15
申请人 GENERAL ELECTRIC COMPANY 发明人 KLINGLER BRETT DARRICK
分类号 F01D25/26;B23P11/00 主分类号 F01D25/26
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