发明名称 TURBINE COOLING CIRCUIT
摘要 <p>PROBLEM TO BE SOLVED: To provide a turbine cooling circuit 32 including a passage sleeve 34 having the rear end 36 adjacent to a rim 30a of a turbine disc 30. SOLUTION: Seal rotors 38 and 42 are separately arranged from the rear end, and are adjacent to a row of an inlet hole 40. An inducer 46 has an outlet 50 arranged on the radial directional outside of a sleeve inlet hole. Seal stators 52 and 54 surround the seal rotors, and form a rotary seal arranged on the radial directional inside of an inducer outlet.</p>
申请公布号 JP2002349287(A) 申请公布日期 2002.12.04
申请号 JP20020077552 申请日期 2002.03.20
申请人 GENERAL ELECTRIC CO <GE> 发明人 GLYNN CHRISTOPHER CHARLES;WALLACE THOMAS TRACY;DICKMAN RONALD ARTHUR;SHELTON MONTY LEE
分类号 F01D5/08;F01D5/18;F01D11/02;F02C7/12;F02C7/18;(IPC1-7):F02C7/18 主分类号 F01D5/08
代理机构 代理人
主权项
地址