一种中分面空间受限的渐变稳压腔室及进腔方法
By designing a gradually stabilizing chamber with limited space in the split plane, the chamber is divided into four independent areas. Airflow is controlled by inlet isolation and horizontal isolation, which solves the problem of insufficient aerodynamic performance under limited space in the split plane, achieves low loss and uniform flow, and improves the efficiency and stability of the turbine unit.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- DONGFANG TURBINE CO LTD
- Filing Date
- 2023-12-25
- Publication Date
- 2026-07-17
AI Technical Summary
When the space of the split surface is limited, it is difficult to achieve a high-performance air intake chamber with excellent aerodynamic performance in the design of the horizontal tangential air intake chamber, resulting in energy loss and uneven flow.
A gradually stabilizing chamber with a confined central split surface is designed. The chamber is divided into four independent regions by a full-circumference annular chamber and an intake baffle and a horizontal baffle to simulate tangential airflow in the intake chamber. This ensures that the airflow flows in an orderly manner in each region and controls the flow distribution through the intake baffle.
It achieves low aerodynamic pressure loss and uniform chamber outlet airflow, improving the efficiency and stability of the turbine unit and reducing energy loss and flow disturbance.
Smart Images
Figure CN117869019B_ABST