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Author:

Li, Kangdi (Li, Kangdi.) | Zhou, Qianqian (Zhou, Qianqian.) | Xu, Zili (Xu, Zili.) | Wang, Xin (Wang, Xin.) | Jin, Yafeng (Jin, Yafeng.)

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Abstract:

A method for calculating dynamic characteristics of stepped labyrinth seals with consideration of inlet preswirl is proposed to solve the problem that the dynamic characteristics of stepped labyrinth seals are affected by inlet preswirl. Governing equations of air excitation force-rotor displacement-rotor velocity are established based on Murphy's small displacement vorticity principle. CFD numerical simulation method is used to calculate the flow passage of full-ring seals with different prswirl ratios. Dynamic characteristic parameters such as stiffness and damping are obtained by solving the governing equations in the frequency domain. The dynamic characteristics of stepped labyrinth seals with different preswirl ratios are studied. The flow field characteristics of stepped labyrinth seal are studied by drawing the pressure distribution and velocity vector diagrams in the flow passage. Numerical simulation results show that with the increase of preswirl ratio, the direct stiffness increases at low frequency and decreases at high frequency, the cross stiffness is almost constant, and the cross damping decreases with the increase of preswirl. Air flow preswirl significantly reduces the direct damping, and the estimated direct damping in preswirl ratio λ=0.255 and λ=0.516 conditions decreases by 16.9% and 21.4% on average compared with the case of λ=0 condition. With the increase of throttling times, the pressure drop of airflow passing through the sealing tooth increases gradually, which are 0.25 MPa, 0.374 MPa and 0.499 MPa, respectively. The velocity of sealing tooth tip also increases gradually, which are 79.5 m/s, 88.36 m/s and 106.0 m/s, respectively. The step arrangement of sealing teeth increases the complexity of the main flow passage, and the step sealing flow passage is divided into throttling region, jet region and eddy region. The eddy region has two vortexes with opposite direction, which increase the dissipation of airflow kinetic energy in the flow passage. © 2022, Editorial Office of Journal of Xi'an Jiaotong University. All right reserved.

Keyword:

Air Computational fluid dynamics Damping Frequency domain analysis Kinetic energy Kinetics Numerical methods Numerical models Seals Stiffness

Author Community:

  • [ 1 ] [Li, Kangdi]State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an JiaoTong University, Xi'an; 710049, China
  • [ 2 ] [Zhou, Qianqian]State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an JiaoTong University, Xi'an; 710049, China
  • [ 3 ] [Xu, Zili]State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an JiaoTong University, Xi'an; 710049, China
  • [ 4 ] [Wang, Xin]Product Development Center, Dongfang Electric Corporation, Deyang; 618000, China
  • [ 5 ] [Jin, Yafeng]Product Development Center, Dongfang Electric Corporation, Deyang; 618000, China

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Source :

Journal of Xi'an Jiaotong University

ISSN: 0253-987X

Year: 2022

Issue: 3

Volume: 56

Page: 117-123

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 16

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