| 摘要 |
The invention relates to a double-rotor biflow axial compressor which provides two air flows, one of them for external cooling and the other one for the supercharging of internal combustion engines, as well as, in aviation, for double-flow turbo jet engines with the function of turbo fan and axial turbo compressor. According to the invention, the compressor comprises a stator () and a power take-off () supporting two rotors () which rotate in opposite directions, this way generating two air flows, one of them intended for external cooling and transmitted through a discharge conduit () and the other one for supercharging, transmitted through another conduit (). |
