发明名称 SHROUD HANGER ASSEMBLY AND GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To solve problems wherein the service life of a shroud is shortened, the operating performance of a turbine is affected, and/or an engine maintenance cycle time is shortened. SOLUTION: This shroud hanger assembly comprises a shroud hanger 226 and an impingement baffle 306 joined to the shroud hanger. The shroud hanger comprises a cavity 302 and cooling paths 304 formed in the cavity. Each cooling path extends from the upstream side surface 234 of the shroud hanger through the shroud hanger, and guides cooling air to the impingement baffle. At least two cooling paths are so bound to each other as to communicate with each other through the cavity. COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2008032014(A) 申请公布日期 2008.02.14
申请号 JP20070195871 申请日期 2007.07.27
申请人 GENERAL ELECTRIC CO <GE> 发明人 BOSLEY BLAINE CHARLES;KEITH SEAN ROBERT;KRESS JEFFREY ALLEN;ALBRECHT RICHARD W JR
分类号 F02C7/18;F01D11/08;F02C7/28 主分类号 F02C7/18
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