发明名称 Axial turbocompressor
摘要 An axial turbocompressor having an annular compressor passage which is arranged concentrically around a rotational axis, is delimited radially on the outside by a passage wall, and in which rotor blades, which may be assembled to form a ring, are arranged in a rotatably mounted manner around the rotational axis, is provided. The free-ending tips of the rotor blades lie opposite the passage wall in each case, forming a gap, and the passage wall, in the axial section of the tips, at least partially has a wall structuring and wherein a bleed opening of a bleed passage is provided in the passage wall for the tapping of medium flowing in the compressor passage. In order to enable an exceptionally efficient bleed of medium flowing in the compressor passage, the bleed opening is located in the wall structuring.
申请公布号 US2012315131(A1) 申请公布日期 2012.12.13
申请号 US201213488540 申请日期 2012.06.05
申请人 MERTENS DIRK 发明人 MERTENS DIRK
分类号 F01D1/04;F01D25/24 主分类号 F01D1/04
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