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.
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
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