Numerical Analysis of Dynamic Coefficients for Gas Film Face Seals

Author:

Liu Yuchuan1,Shen Xinmin2,Xu Wanfu3

Affiliation:

1. State Key Laboratory of Tribology, Tsinghua University, Beijing 100084, China

2. School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

3. Lubrication Technology Research Center, Shenyang Institute of Technology, Shenyang 110015, China

Abstract

A numerical analysis of stiffness and damping coefficients for gas film face seals in three degrees of freedom is presented in this paper. By applying small perturbation approximation, the steady and perturbed Reynolds equations, taking account of both hydrodynamic and hydrostatic effects, are obtained and solved by finite element method. Several numerical samples, including externally pressurized annular thrust gas bearings and spiral groove thrust gas bearings, validate the model and numerical algorithm. The results show that the interactions between axial and angular perturbation are negligible. Hence, in the dynamic analysis of gas film face seals, the perturbation in three degrees of freedom can be simplified as two independent ones, an axial movement and an angular wobble around two orthogonal axes perpendicular to axial direction.

Publisher

ASME International

Subject

Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials

Reference21 articles.

1. Manaloski, S. B., and Pan, C. H. T., 1965, “The Static and Dynamic Characteristic of the Spiral-Grooved Thrust Bearing,” ASME J. Basic Eng., 87, pp. 547–558.

2. Lund, L. , 1968, “Calculation of Stiffness and Damping Properties of Gas Bearings,” ASME J. Lubr. Technol., 90, pp. 793–803.

3. Zhou, H., 1981, “A High Order, Isoparametric, Finite Element Method for the Calculation of Static and Perturbed Frequency Characteristics of Spiral-Grooved Self Acting Gas Bearings,” Proc. 8th International Gas Bearing Symposium, BHRA Fluid Engineering, Cranfield, England, pp. 229–236.

4. Wang, Y., 1988, “Stability Study of High Speed Gas Lubricated Floating Ring Combined With Aerostatic/Areodynamic Hybrid Bearing,” Ph.D. thesis, Beijing University of Aeronautics and Astronautics, Beijing, China.

5. Mao, Q., Chen, Z., and Li, Z., 1993, “Study on An Aerodynamic Thrust Bearing with Elastically Supported Swing Pads,” Journal of Beijing Institute of Technology, 13(S1), pp. 25–28.

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