发明名称 COMPRESSOR
摘要 PROBLEM TO BE SOLVED: To provide a relatively highly efficient compressor having a pressure ratio equal to that of a centrifugal compressor and reduced in the weight and dimension thereof. SOLUTION: A rotor 2 is structured of a first rotor 21 and a second rotor 22, first recessed parts 7 are symmetrically formed in relation to a rotary shaft 6 in a rear end of the first rotor 21 crossing the rotary shaft 6, second recessed parts 8 are symmetrically formed in relation to the rotary shaft 6 in a front part of the second rotor 22 crossing the rotary shaft 6, and the first rotor 21 and the second rotor 22 are connected to each other to form the rotor 2 of hollow structure. A rotor blade cascade 1 is structured of a first rotor blade cascade 11 corresponding to the first rotor 21 and a second rotor blade cascade 12 corresponding to the second rotor 22, and shape and position of blade are selected in response to each of the rotor blade cascades 11 and 12 to efficiently give rotation energy to a fluid. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006242130(A) 申请公布日期 2006.09.14
申请号 JP20050061362 申请日期 2005.03.04
申请人 JAPAN AEROSPACE EXPLORATION AGENCY 发明人 IWASE SATORU;SAITO YOSHIO
分类号 F04D29/28 主分类号 F04D29/28
代理机构 代理人
主权项
地址