The leakage flow characteristics and the influencing factors of the brush seals were studied both theoretically and experimentally. A fluid-structure interaction theoretical model was established to analyze the leakage flow characteristics of brush seals. Experiments were presented to test the leakage quantity of brush seals with different pressure ratios and rotational speeds and compared with the theory solution model to verify. Based on the accuracy of the theory computational model
the effect law of the brush seal leakage quantity in different structural parameters was analyzed
and the formula for predicting the leakage quantity of brush seals was constructed. The results showed that
the leakage quantity of the brush seals increased approximately linearly with the increase of the pressure ratio when the radial clearance was fixed. The rotational speed had little influence on the leakage quantity of the brush seals. Bristles diameter and the clearance of the bristles affected the leakage quantity through affecting the effective flow area of the gas in the brush area
the smaller effective flow area led to the smaller leakage quantity. With the increase of the bristles diameter and the axial rows of the bristles
the leakage quantity of the brush seals decreased gradually. The leakage quantity increased with the increase of the bristles clearances. As the backing plate fence height and the axial clearance between the last row bristles and the backing plate fence increased
the leakage quantity firstly increased rapidly
and finally became stable. The constructed theoretical formula of leakage quantity can accurately predict the leakage quantity of brush seals and provide a theoretical basis for the optimization design of brush seals structure.
Fluid-structure interaction investigation on the flow field and mechanical characteristic in brush seals with bristle deflections
Flow field characteristics of underwater supersonic over⁃expanded gas jet
Numerical and experimental research on influence of brush bristle wear on leakage and flow characteristics of brush seal
Pre-cooling characteristics of high temperature inlet air for turbine power combined with ramjet
Numerical investigation on induced mechanism of blow-down effect of brush seals with fluid-structure interaction
Related Author
SUN Dan
LIU Ning-ning
HU Guang-yang
AI Yan-ting
WANG Ke-ming
Chun ZHANG
Wei YU
Baoshou WANG
Related Institution
Shenyang Engine Research Institute, Aero Engine Corporation of China
Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University
National Key Laboratory on Hydrodynamics,China Ship Scientific Research Center
Key Lab for Power Transmission of Aero Engine,Shenyang Engine Research Institute,Aero Engine Corporation of China
Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System,School of Aero⁃engine,Shenyang Aerospace University