The modern compressor operation is challenged by the liquid presence in wet gas operating conditions. The liquid phase may affect the compressor stability by partially flooding the internal annular gas seals and inducing subsynchronous vibration (SSV). To improve the annular seal behavior and increase the rotor stability, high-precision results of leakage flow rates and rotordynamic force coefficients are needed for annular gas seals in wet gas conditions. In order to better understand the leakage and rotordynamic characteristics of the annular gas seal in wet gas conditions, a 3D transient CFD-based perturbation method was proposed for computations of leakage flow rates and rotordynamic force coefficients of annular gas seals with liquid phase in main gas phase, based on inhomogeneous Eulerian-Eulerian multiphase flow model, mesh deformation technique, and the multifrequency rotor whirling orbit model. Numerical results of frequency-dependent rotordynamic force coefficients and leakage flow rates were presented and compared for three types of noncontact annular gas seals, which include a smooth plain annular seal (SPAS), a labyrinth (LABY) seal, and a fully partitioned pocket damper seal (FPDS). These three seals were designed to have the identical rotor diameter, sealing clearance, and axial length. The accuracy and the availability of the present transient CFD numerical method were demonstrated with the experiment data of leakage flow rates and frequency-dependent rotordynamic force coefficients of the smooth plain seal with four inlet liquid volume fractions (LVFs) of 0%, 2%, 5%, and 8%. Steady and transient numerical simulations were conducted at inlet air pressure of 62.1 bar, pressure ratio of 0.5, rotational speed of 15,000 rpm, and inlet preswirl ratio of 0.3 for four inlet LVFs varying from 0% to 8% and 14 subsynchronous and synchronous whirling frequencies up to 280 Hz. The numerical results show that the inlet liquid phase has a significant influence on the leakage and rotordynamic coefficients for all three types of annular gas seals. The mixture leakage flow rate increases with the increasing inlet LVF, combining the decreasing gas-phase and linearly increasing liquid-phase leakage flow rates. The smooth plain seal leaks the most gas phase and liquid phase, followed by the pocket damper seal (PDS) and then the labyrinth seal. Increasing inlet LVF significantly decreases the direct stiffness and slightly increases the effective damping of the smooth plain seal. The labyrinth seal possesses evident negative direct stiffness and shows a noticeable decreasing effective damping with the increasing inlet LVF at the subsynchronous frequency range. Increasing inlet LVF obviously increases all the force coefficients of the pocket damper seal including the positive effective damping. From a rotordynamic viewpoint, the FPDS possesses a better liquid tolerant capability and so is a better sealing scheme for the balance piston seals and center seals of the centrifugal compressor in wet gas operating condition.
Skip Nav Destination
Article navigation
March 2019
Research-Article
Numerical Investigation on the Leakage and Rotordynamic Characteristics for Three Types of Annular Gas Seals in Wet Gas Conditions
Zhigang Li,
Zhigang Li
Institute of Turbomachinery,
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
Search for other works by this author on:
Zhi Fang,
Zhi Fang
Institute of Turbomachinery,
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
Search for other works by this author on:
Jun Li
Jun Li
Institute of Turbomachinery,
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China;
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China;
Collaborative Innovation Center of
Advanced Aero-Engine,
Beijing 100191, China
e-mail: junli@mail.xjtu.edu.cn
Advanced Aero-Engine,
Beijing 100191, China
e-mail: junli@mail.xjtu.edu.cn
Search for other works by this author on:
Zhigang Li
Institute of Turbomachinery,
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
Zhi Fang
Institute of Turbomachinery,
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China
Jun Li
Institute of Turbomachinery,
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China;
School of Energy & Power Engineering,
Xi’an Jiaotong University,
Xi’an 710049, China;
Collaborative Innovation Center of
Advanced Aero-Engine,
Beijing 100191, China
e-mail: junli@mail.xjtu.edu.cn
Advanced Aero-Engine,
Beijing 100191, China
e-mail: junli@mail.xjtu.edu.cn
1Corresponding author.
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 31, 2018; final manuscript received August 16, 2018; published online October 4, 2018. Editor: Jerzy T. Sawicki.
J. Eng. Gas Turbines Power. Mar 2019, 141(3): 032504 (16 pages)
Published Online: October 4, 2018
Article history
Received:
July 31, 2018
Revised:
August 16, 2018
Citation
Li, Z., Fang, Z., and Li, J. (October 4, 2018). "Numerical Investigation on the Leakage and Rotordynamic Characteristics for Three Types of Annular Gas Seals in Wet Gas Conditions." ASME. J. Eng. Gas Turbines Power. March 2019; 141(3): 032504. https://doi.org/10.1115/1.4041313
Download citation file:
Get Email Alerts
Image-based flashback detection in a hydrogen-fired gas turbine using a convolutional autoencoder
J. Eng. Gas Turbines Power
Fuel Thermal Management and Injector Part Design for LPBF Manufacturing
J. Eng. Gas Turbines Power
An investigation of a multi-injector, premix/micromix burner burning pure methane to pure hydrogen
J. Eng. Gas Turbines Power
Related Articles
Static and Rotordynamic Characteristics for Two Types of Novel Hole-Pattern Seals Operating in Supercritical CO 2 Turbomachinery
J. Eng. Gas Turbines Power (July,2022)
Leakage and Rotordynamic Characteristics for Three Types of Annular Gas Seals Operating in Supercritical CO 2 Turbomachinery
J. Eng. Gas Turbines Power (October,2021)
Sensitivity Analysis of the Static and Rotordynamic Characteristics on Geometric Parameters for a Supercritical Carbon Dioxide Hole-Pattern Damper Seal
J. Eng. Gas Turbines Power (January,2025)
Swirl Brake Design for Improved Rotordynamic Vibration Stability Based on Computational Fluid Dynamics System Level Modeling
ASME Open J. Engineering (January,2023)
Related Proceedings Papers
Related Chapters
Summary and Conclusions
Bearing Dynamic Coefficients in Rotordynamics: Computation Methods and Practical Applications
Later Single-Cylinder Engines
Air Engines: The History, Science, and Reality of the Perfect Engine
Stability and Range
Design and Analysis of Centrifugal Compressors