Startseite Analysis of leakage characteristics and structural optimization of two-stage floating ring seal
Artikel
Lizenziert
Nicht lizenziert Erfordert eine Authentifizierung

Analysis of leakage characteristics and structural optimization of two-stage floating ring seal

  • Tingxun Hu ORCID logo , Wangqun Deng EMAIL logo , Zhenhuan Tang , Dong Mi , Weifeng Zhang und Xiaoyan Wang
Veröffentlicht/Copyright: 19. März 2025
Veröffentlichen auch Sie bei De Gruyter Brill

Abstract

Two-stage floating ring seal is a non-contact circumferential seal with low leakage and high reliability. This paper elaborates on the variation mechanism and calculation method of the working clearance and working conditions of sealing chamber, reveals the corresponding relationship between operating conditions of aircraft engine and leakage characteristics of two-stage floating ring seal, obtains an effective method for analyzing the leakage characteristics of two-stage floating ring seals. The pressure of sealing chamber can be determined by continuously assuming the pressure of sealing chamber and substituting it to continuity equation. Carry out leakage characteristic experiments under specific operating conditions, the minimum deviation between the value of calculation and the experimental results is −11.47 %, the maximum deviation is 7.34 %, and the average of the absolute value of deviation is 5.01 %. The optimization design scheme for the working clearance and the intermediate air flow channel have been proposed, which can provide important support for improving the reliability and sealing performance of the two-stage floating ring seal.


Corresponding author: Wangqun Deng, AECC Hunan Aviation Powerplant Research Institute, Zhuzhou, Hunan 412002, China; and Key Laboratory of Aero-Engine Vibration Technology, Aero Engine Corporation of China, Zhuzhou 412002, China, E-mail:

Nomenclature (SI units)

T f

temperature of the sealing gas (K)

T z

temperature of the bearing cavity (K)

T p

temperature of the rotating ring (K)

K f

convective heat transfer coefficients of the sealing gas (W·m2/K)

K z

convective heat transfer coefficients of the bearing cavity (W·m2/K)

δ p0

thermal expansion of the rotating ring (m)

a

linear expansion coefficient of the rotating rin (/K)

r p

initial size of the outer diameter of rotating ring (m)

T s

room temperature (K)

δ z

actual magnitude of interference (m)

δ c

initial magnitude of interference (m)

α w

linear expansion coefficient of the outer ring (/K)

α s

linear expansion coefficient of the graphite ring (/K)

T

temperature difference (K)

d 1

inner diameter of the graphite ring (m)

d 1

inner diameter of the outer ring (m)

d 3

outer diameter of the outer ring (m)

L 1

width of the graphite ring (m)

L 2

width of the outer ring (m)

L

contact width between the graphite ring and the outer ring (m)

p 0

pressure on the graphite ring and the outer ring (N)

p 1

equivalent pressure on the graphite ring (N)

p 2

equivalent pressure on the outer ring (N)

K 1

diameter ratio of the graphite ring

K 2

diameter ratio of the outer ring

σ r1

equivalent circumferential stress of the graphite ring (Pa)

σ θ1

equivalent radial stress of the graphite ring (Pa)

σ z1

equivalent axial stress of the graphite ring (Pa)

σ r2

equivalent circumferential stress of the outer ring (Pa)

σ θ2

equivalent radial stress of the outer ring (Pa)

σ z2

equivalent axial stress of the outer ring (Pa)

E 1

elastic modulus of the graphite ring (Pa)

μ 1

Poisson’s ratio of the graphite ring

E 2

elastic modulus of the outer ring (Pa)

μ 2

Poisson’s ratio of the outer ring

r 1

radial displacement of the graphite ring (m)

r 2

radial displacement of the outer ring (m)

P 0

pressure in the sealing chamber (Pa)

S 1

leakage from the high-pressure side (g/s)

S 2

leakage from the middle bleed side (g/s)

T 1

temperature on the high-pressure side (K)

T 2

temperature on the middle bleed side (K)

  1. Research ethics: Not applicable.

  2. Informed consent: Informed consent was obtained from all individuals included in this study, or their legal guardians or wards.

  3. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  4. Use of Large Language Models, AI and Machine Learning Tools: None declared.

  5. Conflict of interest: The authors state no conflict of interest.

  6. Research funding: This study is supported by the Technology Innovation Platform Foundation of AECC (No. CXPT-2023-023), and the National Natural Science Foundation of China (No.52375077).

  7. Data availability: Not applicable.

References

1. Duan, W, Chu, F, Kimb, CH, Lee, YB. A bulk-flow analysis of static and dynamic characteristics of floating ring seals. Tribol Int 2007;40:470–8. https://doi.org/10.1016/j.triboint.2006.04.010.Suche in Google Scholar

2. Choi, CH, Noh, JG, Kim, DJ, Hong, SS, Kim, J. Effects of floating ring seal clearance on the pump performance for turbopumps. J Propul Power 2009;25:191–5. https://doi.org/10.2514/1.36806.Suche in Google Scholar

3. Mariot, A, Arghir, M, Helies, P, Dehouve, J. Experimental analysis of floating ring annular seals and comparisons with theoretical predictions. J Eng Gas Turbines Power 2016;138:042503-1–9. https://doi.org/10.1115/1.4031347.Suche in Google Scholar

4. Li, GQ, Zhang, Q, Huang, EL, Lei, Z, Wu, H, Xu, G. Leakage performance of floating ring seal in cold/hot state for aero-engine. Chin J Aeronaut 2019;32:2085–94. https://doi.org/10.1016/j.cja.2019.03.004.Suche in Google Scholar

5. Jiang, J, Sun, D, Zhao, H, Wang, S, Hu, HT, Chang, C. Numerical study on mechanical properties of floating ring seal based on fluid-solid thermal coupling. Lubr Eng 2023;48:30–9.Suche in Google Scholar

6. Sun, D, Wang, P, Wang, XD, Zhao, H, Zhang, GC. Investigation on rotor dynamic characteristics and adaptive concentric performance of a new type of floating convergent pocket seal. J Propuls Technol 2021;42:406–14.Suche in Google Scholar

7. Hu, TX, Zhou, K, Wang, XY, Li, N, Zhou, HY. Numerical calculation and experiment on leakage char-acteristics of floating ring seal. J Aero Power 2020;35:888–96.Suche in Google Scholar

8. Hu, TX, Wang, XY, Zhou, K, Li, QF, Zhou, HY. Effects of temperature on leakage characteristics of floating ring seal. J Propuls Technol 2022;43:200846.Suche in Google Scholar

9. Xia, P, Liu, ZS. Effects of structure elasticity on leakage and rotor dynamic coefficients of floating ring seals. J Propuls Technol 2017;38:2815–21.Suche in Google Scholar

10. Liu, ZS, Xia, P, Zhang, GH. Floating ring seals movement mechanism and its influence on stability of rotor system. J Vib Shock 2016;35:110–16.Suche in Google Scholar

11. Ha, TW, Lee, YB, Kim, CH. Leakage and rotor dynamic analysis of a high pressure floating ring seal in the turbopump unit of a liquid rocket engine. Tribol Int 2002;35:153–61. https://doi.org/10.1016/s0301-679x(01)00110-4.Suche in Google Scholar

12. Arghir, M, Nguyen, MH, Tonon, D, Dehouve, J. Analytic modeling of floating ring annular seals. J Eng Gas Turbines Power 2012;134:052507. https://doi.org/10.1115/1.4004728.Suche in Google Scholar

13. Chen, Z, Gao, CY, Fan, WC, Jie, H. Simu-lation of flow field in a floating ring seal and modification of its leakage rate expression. J Sichuan Univ (Eng Sci Ed) 2016;1:208–14.Suche in Google Scholar

14. Zheng, R, Chen, XZ, Li, SX, Zhao, X, Shi, RJ, Song, ZF. Opening characteristics of inlaid floating ring seal with high-speed gas film. J Beijing Univ Aeronaut Astronaut 2022;48:2111–20.Suche in Google Scholar

15. Lee, YB, Kim, KW, Ryu, SJ, Chung, JT. Leakage performance and rotor dynamic characteristics of bump floating ring seals for turbopump. In: ASME Turbo Expo 2014: Turbine Technical Conference and Exposi-tion. New York: American Society of Mechanical Engineers, Springer; 2014.10.1115/GT2014-26274Suche in Google Scholar

16. Ma, Z, Zhou, K, Wang, XY. Measurement method of small gas leakage flow of sealing devices. Lubr Eng 2018;43:130–3.Suche in Google Scholar

17. Ma, G, Xi, P, Shen, XM, Hu, GY. Analysis of quasi-dynamic characteristics of compliant floating ring gas cylinder seal. J Aero Power 2010;1190–6.Suche in Google Scholar

18. Yang, XQ, Wang, YF, Ma, GF. CFD numerical simulation of the performance of floating ring seals with variable inclination groove. Lubr Eng 2024;49:52–8.Suche in Google Scholar

19. Liu, W, Zhang, SY, Zhai, ZX, Zhu, SH, Li, SX. Classification method for frictional vibration signals of floating ring seal based on QSE-ResNet. J Vib Shock 2024;21:194–201.Suche in Google Scholar

20. Liu, Y, Guo, HD, Zhang, Q, Yan, FC. Simulation research on normal stiffness of floating ring seal end face based on the fractal theory. J Vib Shock 2024;16:102–10.Suche in Google Scholar

Received: 2025-02-23
Accepted: 2025-02-23
Published Online: 2025-03-19
Published in Print: 2025-08-26

© 2025 Walter de Gruyter GmbH, Berlin/Boston

Artikel in diesem Heft

  1. Frontmatter
  2. Simulation and analysis of the over-expanded flow field in asymmetric nozzles with lateral expansion
  3. Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models
  4. Research on vibration damping of integral squeeze film damper based on fan rotor tester of turbofan
  5. Influence of conical shaft stiffness on the dynamic characteristics of flexible rotor
  6. A novel design methodology for preventing dislocation in the Zig-zag shroud
  7. Numerical study of effect of the casing slot on the tip leakage vortex and vortex cavitation of a fuel pump
  8. Multi-parameter study on array-jets impingement with crossflow temperature effect
  9. Exploration of shock-induced flow dynamics and turbulence-driven combustion optimization in advanced cavity configurations of hydrogen fueled scramjet combustors
  10. A part-load performance analysis method for gas turbines based on the stage by stages model of the power turbine
  11. Effect of lip-thickness on rectangular nozzle co-flowing subsonic jet
  12. Numerical analysis of pollutant formation and exhaust emission in a short annular combustor under part load operation
  13. Analysis of leakage characteristics and structural optimization of two-stage floating ring seal
  14. Hypersonic boundary layer flow at an axisymmetric stagnation point on a blunt body
  15. Numerical simulations of a turbulent lifted hydrogen flame in vitiated coflow with flamelet generated manifold approach
  16. Optimization of labyrinth seal leakage with independently varied tooth parameters using efficient global optimization
  17. Investigations of modified cooling hole injection angle configurations for improved trench film cooling performance
  18. Influence of non-axisymmetric endwall profiling under incoming vortex on the corner separation of a diffusion cascade
  19. Impact of annular ribs in sudden expansion flow conditions to control base pressure
  20. Effect of preheated swirling multi-annular jets on mixing and flow characteristics in various expanded confinements
Heruntergeladen am 26.11.2025 von https://www.degruyterbrill.com/document/doi/10.1515/tjj-2025-0021/html
Button zum nach oben scrollen