seal performance and its influential factors were analyzed based on its structure feature
and fluid dynamics calculative model of sealing zone was built.The velocity
pressure distribution in sealing clearance and leakage were calculated
and the sealing performance with structure parameters in different working conditions was obtained.The result shows that the leakage increases linearly with the sealing pressure
and decreases slightly with the increase of rotor speed;leakage reduces by about 40% with the leaf width from 3mm to 7mm
while it increases by only about 8% with the leaf length from 12mm to 16mm.With the widening gap of the front/back cover plate to leaf or to rotor
the result is also different;the gap from upper cover plate to rotor has greater impact on leakage compared with lower cover plate
with the leakage up to 16%.Leakage and rotor force are also affected by different dip angles of the leaf end.
Numerical and experimental investigation on interstage pressure drop equalization of differential multi⁃stage brush seals
Temperature field of double helical star gear transmission system in mixed lubrication condition
Accurate prediction method of flow coefficient for 2D curved surface variable inlet
Effect of movable flat baffles plenum volume on pressure distortion flow field of engine
Analysis of flow field characteristics of medium reducer with splash lubrication in a certain helicopter
Related Author
Huan ZHAO
Yelong LI
Dan SUN
Wei MU
Ting MA
Guangyang HU
LIN Tengjiao
HUANG He
Related Institution
Key Laboratory of Advanced Measurement and Test Technique for Aviation;Propulsion System,Liaoning Province,School of Aero⁃engine,Shenyang Aerospace University
Shenyang Engine Research Institute,Aero Engine Corporation of China
Key Laboratory for Power Transmission of Aero Engine, Aero Engine Corporation of China