发明名称 AXIAL TURBO COMPRESSOR
摘要 <P>PROBLEM TO BE SOLVED: To provide an axial turbo compressor having an annular compressor flow path arranged concentrically around a rotational axis. <P>SOLUTION: In the axial turbo compressor with the compressor flow path 25 delimited on the outside by a flow path wall 42, and with rotor blades assemblable to form a ring arranged in a rotatably mounted state about the rotational axis, free-end side tips of the rotor blades face the flow path wall 42 with a space formed in between, the flow path wall at least partially has an in-wall structure 44 in an axial-direction section of the tips, and bleed openings 52 of bleed flow paths 50 are provided to let a medium flowing in the compressor flow path 25 flow out. The bleed openings are placed in the in-wall structure so as to allow remarkably effective extracting of the medium flowing in the compressor flow path 25. <P>COPYRIGHT: (C)2013,JPO&INPIT
申请公布号 JP2012255440(A) 申请公布日期 2012.12.27
申请号 JP20120129623 申请日期 2012.06.07
申请人 SIEMENS AG 发明人 MERTENS DIRK
分类号 F04D29/54;F02C9/18;F04D29/66 主分类号 F04D29/54
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