发明名称 THERMAL INSULATION COATING, ITS CONSTRUCTION METHOD, TURBINE MEMBER, AND GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To provide thermal insulation coating and its construction method for preventing peeling-off of a ceramic layer by a simple configuration and to provide a turbine member on which the thermal insulation coating is applied and a gas turbine provided with the turbine member. SOLUTION: A vertically cracked membrane is provided in a front fringe part 3a of a blade part 3, and the other part is an ordinary porous membrane. To explain concretely, the vertically cracked membrane is applied to a section shown by a diagonal line in Fig. a and shown by a scope A in Fig. b. It is in a scope of, for example, about 15 mm on a belly side from a front fringe and about 15 mm on a back side from a front fringe part root to an upper end. The porous membrane is applied to the other scope. The front fringe uses a line (not shown) on which, for example, a shower head (a cooling hole) of the front fringe part 3a is arranged in the longitudinal direction of the blade part 3 as a reference position. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004169558(A) 申请公布日期 2004.06.17
申请号 JP20020333051 申请日期 2002.11.18
申请人 MITSUBISHI HEAVY IND LTD 发明人 MEGA MASAHIKO;TAKAHASHI KOJI;KANIKAWA MASAYA;OHARA MINORU;IZUTSU DAISUKE;YAMAGUCHI KENGO;NARITA ATSUSHI;MORI KAZUTAKA;TORIGOE TAIJI;SHIGE TAKASHI
分类号 F01D5/28;C23C30/00;F02C7/00;(IPC1-7):F01D5/28 主分类号 F01D5/28
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