发明名称 A mounting arrangement for turbine blades
摘要 A mounting arrangement 31 incorporates a blade pocket cavity 35, 135, 235 between a blade platform 34, 134, 234 and a rotor disc post 53. Coolant air is presented within the cavity 35, 135, 235 in order to provide cooling of the platform 34, 134, 234. In order to inhibit ingress of hot air from adjacent wheel spaces 36, an air curtain is created across an open end 45, 145 whereby coolant air is contained within the cavity 35, 135, 235. Air flow from the air curtain itself may pass along a surface 48, 148 to provide more direct cooling for the platform 34, 134, 234. Apertures 49, 50 may be provided in order to bleed coolant air from the cavity 35 and also draw an air flow 51 across the surface 48 for greater cooling efficiency.
申请公布号 EP1574670(A3) 申请公布日期 2009.02.25
申请号 EP20050251229 申请日期 2005.03.01
申请人 ROLLS-ROYCE PLC 发明人 FERRA, PAUL WILLIAM;MYLEMANS, JOHN ANDREW
分类号 F01D5/18;F01D5/08;F01D5/14;F02C7/18 主分类号 F01D5/18
代理机构 代理人
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