发明名称 TURBINE ASSEMBLY AND TURBINE SHROUD THEREFOR
摘要 A turbine assembly includes a shroud (122) for being mounted around a last stage of the low pressure turbine rotor. The shroud (122) includes an arcuate body having spaced-apart forward and aft ends and spaced-apart circumferential ends. Attachments are provided for securing the shroud body to the surrounding engine case. An arcuate extension member (130) protrudes rearward from the aft end of the shroud body. The extension member (130) has an inner surface (132) which defines a portion of the gas flowpath through the engine. Seals may be provided to prevent leakage between adjacent shroud segments. The shroud (122) is especially useful for protecting a downstream turbine frame from debris and thermal stress.
申请公布号 CA2518525(C) 申请公布日期 2014.08.19
申请号 CA20052518525 申请日期 2005.09.08
申请人 GENERAL ELECTRIC COMPANY 发明人 CZACHOR, ROBERT PAUL;MANTEIGA, JOHN ALAN
分类号 F01D11/08;F01D25/24 主分类号 F01D11/08
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