发明名称 A CONDUIT FOR A GAS TURBINE UNIT AND A METHOD OF MANUFACTURING A CONDUIT
摘要 A gas turbine unit (20) has a conduit (10) comprising two halves, a first half (loa) and a second half (lOb) , assembled together. The conduit has an inlet (10') in the tangential direction and an outlet (10") in the radial direction. An inlet (301) of a stator part (30) is received inside the outlet of the conduit, whereby the conduit is securely connected to the stator part by a pressure exerted in the axial direction of the gas turbine unit against the inlet of the stator part when the conduit and the stator part are assembled together.
申请公布号 WO03023192(A1) 申请公布日期 2003.03.20
申请号 WO2002SE01599 申请日期 2002.09.06
申请人 TURBEC AB;REHN, JOHNNY 发明人 REHN, JOHNNY
分类号 F01D9/02;F01D25/24;(IPC1-7):F01D9/02 主分类号 F01D9/02
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