| 摘要 |
Supersonic radial compressor with pressure recovery by means of compression shocks which appear outside the blading of the rotor where one or several shunted radial supersonic ring orifices (7, 9) are provided, in the flow direction of the medium, behind the rotor blading and in front of diffusor (3). Specifically one or more radial supersonic ring orifices (7) with separator elements (2) are fixed in the diffuser chamber or at the rotor outlet. |
