发明名称 SISTEMA DI UTILIZZAZIONE DELLA PERDITA DI ARIA DI RAFFREDDAMENTO IN UN TURBOMOTORE A GAS
摘要 <p>The fluid cooling arrangement is intended for a turbine blade comprising the blade profile itself (12), a platform (13) and a blade root (17) part of which is held in the rotor (10) whilst another portion partially bounds a void (44) which receive fluid leaking from a chamber upstream of the blades. A wall element (16) is provided, extending radially inwards from the platform and partially bounding the void. A bore (52) is provided in this wall, whose centre line is at an acute angle relative to the rotor axis, which bore serves as outlet for the fluid from the void. The bore centre line may be parallel to the downstream portion of the blade profile.</p>
申请公布号 IT1063518(B) 申请公布日期 1985.02.11
申请号 IT19760026732 申请日期 1976.09.01
申请人 GENERAL ELECTRIC COMPANY 发明人
分类号 F01D5/18;(IPC1-7):F02C/ 主分类号 F01D5/18
代理机构 代理人
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