METHODS AND APPARATUSES FOR COOLING GAS TURBINE ENGINE ROTORASSEMBLIES
摘要
A turbine mid-frame assembly is provided. The turbine mid-frame assembly includes a turbine mid-frame including at least one of a fastener cover plat e and an opening (42) extending through the turbine mid-frame configured to facilitat e cooling a turbine (20) coupled downstream from and adjacent to the turbine mid-frame .
申请公布号
CA2567938(A1)
申请公布日期
2007.05.16
申请号
CA20062567938
申请日期
2006.11.14
申请人
GENERAL ELECTRIC COMPANY
发明人
GLYNN, CHRISTOPHER CHARLES;ROYAL, GLEN WILLIAM;JENDRIX, RICHARD WILLIAM;CORMIER, NATHAN GERARD;PROCTOR, ROBERT;MONTGOMERY, JULIUS JOHN
