发明名称 Turbine nozzle cooling assembly
摘要 The present application provides an inner nozzle platform. The inner nozzle platform may include a platform cavity 140, an impingement plenum 170 positioned within the platform cavity 140, a retention plate positioned 190 on a first side 235 of the impingement plenum 170, and a compliant seal positioned on a second side of the impingement plenum 170.
申请公布号 EP2613012(A1) 申请公布日期 2013.07.10
申请号 EP20130150161 申请日期 2013.01.03
申请人 GENERAL ELECTRIC COMPANY 发明人 WINN, AARON GREGORY;COIGN, ROBERT WALTER;PHILLIPS, JAMES S.;TIPTON, THOMAS ROBBINS;FOSTER, GREGORY THOMAS;MEENAKSHISUNDARAM, RAVICHANDRAN;PAI, NIRANJAN GOKULDAS
分类号 F01D11/00 主分类号 F01D11/00
代理机构 代理人
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