发明名称 |
GAS TURBINE EQUIPMENT AND CASING STRUCTURE OF TRANSITION PIECE OF ITS COMBUSTOR |
摘要 |
PROBLEM TO BE SOLVED: To reliably install a seal member at a transition piece outlet part as rigidity of the transition piece outlet part of the combustor of gas turbine equipment is properly ensured. SOLUTION: A casing 8 of the transition piece 6 to effect intercommunication between the combustor of the gas turbine equipment and the turbine side is formed in the shape of a parallelogram in section in a way that a surface vertically to the direction of a gas turbine rotary shaft is situated in parallel to the compressor side and the turbine side and a surface paralleling the inner surface of the transition piece is formed. Wear resistant coating 23 is applied on the surface, described above, of the casing 8. The casing 8 is mounted with the curved part of a seal member 21 fitted in the casing 8.
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申请公布号 |
JP2001349544(A) |
申请公布日期 |
2001.12.21 |
申请号 |
JP20000174191 |
申请日期 |
2000.06.06 |
申请人 |
HITACHI LTD |
发明人 |
SEKIHARA TAKASHI;SAITO TAKEO |
分类号 |
F23R3/42;F02C7/28;(IPC1-7):F23R3/42 |
主分类号 |
F23R3/42 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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