发明名称 TWO-AXLE TYPE GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To provide a two-axle type gas turbine capable of suppressing the unbalance of rotors by disposing a bearing between a high-pressure turbine rotor and a low-pressure turbine rotor and securely sealing the bearing. SOLUTION: This two-axle type gas turbine comprises a compressor 20 compressing sucked air and discharging compressed air, a high-pressure turbine 50 having the high-pressure turbine rotor 51 connected to a compressor rotor 21 and forming a gas generator 10 together with the compressor 20, a low-pressure turbine 70 installed on the downstream side of the high-pressure turbine 50 and having the low-pressure turbine rotor 71 rotating independently of the high-pressure turbine rotor 51, an air supply system 76 leading the compressed air from the compressor 20 to a low-pressure turbine initial stage stationary blade 74, and a flexible pipe 90 with flexibility connecting an air supply system 76 to the front bearing 81 of the low-pressure turbine rotor 71 disposed on the upstream side of a low-pressure turbine initial stage moving blade 72a and leading a part of the compressed air flowing in the air supply system 76 to the front bearing 81. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2005344680(A) 申请公布日期 2005.12.15
申请号 JP20040168440 申请日期 2004.06.07
申请人 HITACHI LTD 发明人 ITO TORU;TAKEHARA ISAO;MURATA EITARO;KUROKI HIDETOSHI
分类号 F01D11/04;F01D25/16;F01D25/18;F02C3/10;F02C7/06;F02C7/28;(IPC1-7):F01D11/04 主分类号 F01D11/04
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