发明名称 DAMPING DEVICE AND GAS TURBINE COMBUSTOR
摘要 <p>A damping device (63) is provided in a bypass pipe (61) for supplying high-pressure air to a combustor tail pipe. The damping device (63) has a fluid introduction portion (71) covering the outer periphery of the bypath pipe (61) to form a fluid introduction space (B), acoustic boxes (73a, 73b) having base ends connected to the fluid introduction portion (71) and also having head ends circumferentially extending on the outer periphery of the bypass pipe (61) to form resonance spaces (Da, Db), and partition plates (74a, 74b) forming resonance ducts (Ea, Eb), having a predetermined length, by partitioning the resonance spaces (Da, Db).</p>
申请公布号 KR20100074292(A) 申请公布日期 2010.07.01
申请号 KR20107010980 申请日期 2008.11.19
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 ITO TAKANORI;MATSUYAMA KEISUKE;IKEDA KAZUFUMI;TANIMURA SATOSHI;AKAMATSU SHINJI
分类号 F02C7/24;F01D25/00;F23R3/26;G10K11/16 主分类号 F02C7/24
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