发明名称 タービンシールシステム
摘要 In accordance with one embodiment, a system includes a multi-stage turbine including a first turbine stage including a first wheel having multiple first slots spaced circumferentially about the first wheel, and multiple first blade segments each coupled to at least one of the multiple first slots. The multi-stage turbine also includes a second turbine stage including a second wheel having multiple second slots spaced circumferentially about the second wheel, and multiple second blade segments each coupled to at least one of the multiple second slots. The multi-stage turbine further includes a one-piece interstage seal extending axially between the first and second turbine stages, wherein the one-piece interstage seal comprises a first radial support coupled to the first wheel and a second radial support coupled to the second wheel, and the one-piece interstage seal extends circumferentially across at least two of the multiple first slots or at least two of the multiple second slots.
申请公布号 JP6018367(B2) 申请公布日期 2016.11.02
申请号 JP20110168135 申请日期 2011.08.01
申请人 ゼネラル・エレクトリック・カンパニイ 发明人 ジョセフ・スコット・カミンズ;アイアン・デビッド・ウイルソン
分类号 F01D11/00;F01D5/06;F01D25/00;F02C7/28 主分类号 F01D11/00
代理机构 代理人
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