Influence of inlet preswirl on discharge and heat transfer characteristics of honeycomb and smooth labyrinth seals
|更新时间:2026-07-07
|
Influence of inlet preswirl on discharge and heat transfer characteristics of honeycomb and smooth labyrinth seals
Vol. 24, Issue 4, (2009)
作者机构:
西安交通大学 能源与动力工程学院,西安,710049
作者简介:
基金信息:
DOI:
CLC:
Published:2009
稿件说明:
移动端阅览
YAN Xin, LI Jun, FENG Zhen-ping. Influence of inlet preswirl on discharge and heat transfer characteristics of honeycomb and smooth labyrinth seals[J]. 2009, 24(4).
DOI:
YAN Xin, LI Jun, FENG Zhen-ping. Influence of inlet preswirl on discharge and heat transfer characteristics of honeycomb and smooth labyrinth seals[J]. 2009, 24(4).DOI:
Influence of inlet preswirl on discharge and heat transfer characteristics of honeycomb and smooth labyrinth seals
Three-dimensional Reynolds-averaged Navier-Stokes(RANS) equations were numerically solved to investigate the influence of the inlet preswirl on discharge and heat transfer characteristics in honeycomb and smooth labyrinth seals.The discharge and total temperature increase characteristics
as well as the leakage flow field of these two different seals
were also obtained under five different pressureratios at inlet preswirl ratios of-0.3
0
+0.3.The results show that the influence of the inlet preswirl on the leakage flow rate and meridian flow structure is nearly negligible for both honeycomb and smooth labyrinth seals.Positive inlet preswirl can decrease the total temperature difference between the seal inlet and outlet
while the negative preswirl will cause the opposite effect.The damping effect of the honeycomb can reduce the influence of the inlet preswirl on the total temperature difference.The computed windage heating power of the honeycomb seal is larger than that of smooth labyrinth seal with positive or without inlet preswirl
while it's smaller for the negative inlet preswirl condition.
Numerical and experimental investigation on interstage pressure drop equalization of differential multi⁃stage brush seals
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Numerical simulation of internal flow field in gas generator of fire extinguishing bomb
Research on one-dimensional/three-dimensional coupled modeling for seal and cavity flow of centrifugal compressor
Numerical simulation of light-craft effects onlaser supported donation wave with gas-liquid two phase propellant
Related Author
Huan ZHAO
Yelong LI
Dan SUN
Wei MU
Ting MA
Guangyang HU
Ping ZHANG
Shan LU
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
School of Power and Energy,Northwestern Polytechnical University
Nondestructive Testing and Evaluation Laboratory, Dalian University of Technology