发明名称 AXIAL THREE-STAGED COMPRESSOR
摘要 FIELD: compressor construction, in particular, multiple-staged compressors. SUBSTANCE: compressor has blades composed of parts 4,5,6 directed at different angles to axis of rotation of rotor. Guiding part 4 of blade is directed at an angle of 0-10 deg, compression part 5 at an angle of 15-60 deg and releasing part 6 at an angle of 50-85 deg to rotor axis. Cylindrical surface of rotor is divided into equal sections. Length of guiding part 4 of blades 3 is gradually increasing within each section to define air intake cavity. Compression part 5 of each blade has thickness gradually increasing toward releasing part 6. Releasing part 6 of each blade has constant thickness and its side surfaces define in conjunction with surfaces of adjacent blades slit channels. EFFECT: increased efficiency by creating increased pressure. 3 dwg
申请公布号 RU2136974(C1) 申请公布日期 1999.09.10
申请号 RU19940039948 申请日期 1994.10.25
申请人 POPKOV IVAN IVANOVICH 发明人 POPKOV I.I.
分类号 F04D19/02;(IPC1-7):F04D19/02 主分类号 F04D19/02
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