An adjustable centrifugal compressor radial diffuser structure
By designing an adjustable radial diffuser structure and using guide rings and eccentric wheel mechanisms to adjust the blade inlet angle, the efficiency loss problem of centrifugal compressors under non-design conditions was solved, achieving more efficient energy conversion and flow channel consistency, optimizing rotor-stator clearance, and improving compressor performance.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
- Filing Date
- 2023-03-02
- Publication Date
- 2026-06-09
AI Technical Summary
The radial diffuser of existing centrifugal compressors suffers severe efficiency loss under non-design conditions, and the regulating mechanism has defects that affect efficiency, such as changing the radial clearance between the rotor and stator, flow channel obstruction, or leakage.
An adjustable radial diffuser structure was designed. The radial diffuser blades and eccentric wheel mechanism are driven by a guide ring to adjust the blade inlet angle, reduce airflow leakage and maintain flow channel consistency. A double eccentric wheel mechanism is used to prevent airflow leakage and optimize the radial clearance.
It improves the efficiency of centrifugal compressors under different operating conditions, reduces airflow leakage, maintains the smoothness and efficiency of diffuser channels, optimizes the radial clearance between rotor and stator, and enhances overall performance.
Smart Images

Figure CN116292414B_ABST