Open rotor engine and fan structure therefor
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- AECC COMML AIRCRAFT ENGINE CO LTD
- Filing Date
- 2024-11-22
- Publication Date
- 2026-05-29
AI Technical Summary
The fan structure of open rotor engines presents challenges in noise control, particularly due to interference from tip vortices, root vortices, and nonlinear, multi-scale coupling issues caused by interference between the front and rear rows of blades, making it difficult to meet stringent noise regulations.
A first noise reduction structure is set at the trailing edge of the rotor blades and a second noise reduction structure is set at the leading edge of the stator blades. The structure includes holes and dissipation cavities, a rectifier section, and a resonant cavity and a medium layer in the hub. The rotor wake and rotor-stator interference noise are suppressed by the viscosity and smooth flow of the airflow.
It effectively reduces the fan noise of open rotary engines, meets international airworthiness noise limits, and reduces fuel consumption and CO2 emissions.
Smart Images

Figure CN122106947A_ABST