发明名称 Rotor shaft, in particular for a gas turbine
摘要 Cooling air channels (14) are formed within the turbine section (12) of a drive shaft (10) and between turbine disks (13) around the turbine section. Each of the cooling air channels radiates outward from a cavity (15) around the cooling air supply channel (16) within the drive shaft and is of an elliptical cross-section. The major and minor axes of each cooling air channel runs perpendicular and parallel to the drive shaft axis, respectively.
申请公布号 EP1705339(A3) 申请公布日期 2013.11.06
申请号 EP20060110741 申请日期 2006.03.07
申请人 ALSTOM TECHNOLOGY LTD 发明人 WIEBE, MARKUS, ROLAND;KRAMER, THOMAS;KIEWEL, HOLGER
分类号 F01D5/08 主分类号 F01D5/08
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