发明名称 Gas turbine blade cooling structure
摘要 A blade cooling construction comprising a cylindrical hollow and a nozzle, both of which are defined in and by the blade. The hollow and nozzle create a vortex of cooling gas introduced into the blade, which gas whirls about the axis of the hollow by tangentially injecting the cooling gas into the hollow through the nozzle. A portion of the cooling gas is lowered in temperature, and the other portion is raised in temperature. The lower temperature cooling gas is introduced first to a central portion of the blade height which is higher in temperature than the remaining portions of the blade. The higher temperature cooling gas is introduced to a lower temperature portion of the blade.
申请公布号 US4293275(A) 申请公布日期 1981.10.06
申请号 US19790075584 申请日期 1979.09.14
申请人 HITACHI, LTD. 发明人 KOBAYASHI, NARIYOSHI;SAKAMOTO, TAKESHI;ANZAI, SHUNICHI;MATSUMOTO, MANABU
分类号 F01D5/18;F02C7/18;(IPC1-7):F01D5/18 主分类号 F01D5/18
代理机构 代理人
主权项
地址