In order to obtain the pressure distribution inside the cavity of drum with labyrinth seal
and understand its aerodynamic characteristics
a three-dimensional model of the flow field channel of drum with labyrinth seal was developed
and the static pressure on the surface of drum with and without eccentricity between the drum and the stator was calculated. Then
the mechanics characteristics of drum under aerodynamic loads was analyzed. The simulation results show that different eccentricities complicate the surface static pressure
and change the circumferential static pressure amplitudes obviously. The amplitude of static pressure with the largest eccentricity increases 3 times compared with that without eccentricity. The maximum fluctuation of drum stress amplitude caused by circumferential static pressure considering eccentricity is about 3%.
Design of test system for large⁃scale propeller power simulation in wind tunnel
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications
Aero-engine cycle design approach for multiple operating conditions performance reliability
Relationship between rotor/vanes blade number andnodal diameter number of bladed-disk coupling vibration
Related Author
Hongsheng LEI
Zhengwu CHEN
Zheng WANG
Manfeng DOU
Yu ZHAO
PENG Yunlong
WU Xiong
DING Ting
Related Institution
Key Laboratory of Aerodynamic Noise Control,Low Speed Aerodynamics Institute, China Aerodynamics Research and Development Center
School of Automation, Northwesten Polytechnical University
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics