发明名称 Gas turbine engine
摘要 A rotor disc (15) has an axially enlarged hub portion (18) with a bore (20) through which a turbine shaft (19) extends in a coaxial, radially spaced apart relationship, the annular gap between the hub portion (18) and the shaft (19) receives a flow of temperature regulating fluid. The shaft (19) is provided with axially extending elongate projections (22) to increase the turbulence and relative velocity of the temperature regulating fluid adjacent the projections (22). <IMAGE> <IMAGE>
申请公布号 EP0807743(B1) 申请公布日期 2002.07.03
申请号 EP19970303037 申请日期 1997.05.02
申请人 ROLLS-ROYCE PLC 发明人 ROLT, ANDREW MARTIN
分类号 F01D5/08 主分类号 F01D5/08
代理机构 代理人
主权项
地址