Thermo-Hydrodynamic Effect of Gas Split Floating Ring Seal with Rayleigh Step Grooves

Author:

Bai Shaoxian1,Chu Dongdong1,Ma Chunhong2,Yang Jing1,Bao Shiyi1

Affiliation:

1. College of Mechanical Engineering, Zhejiang University of Technology, Hangzhou 310032, China

2. School of Mechanical and Energy Engineering, Zhejiang University of Science and Technology, Hangzhou 310023, China

Abstract

The force equilibrium and moment equilibrium play a significant role on the sealing performance of gas split floating ring seals. A small deflection angle may generate seriously wear on sealing surface and cause seal failure. Therefore, the thermo-hydrodynamic lubrication analysis of gas split floating ring seal with Rayleigh grooves is investigated considering the deflection angle and frictional heat of surface contact, which is beneficial to grasp the hydrodynamic characteristics and rules under high-temperature and high-speed conditions. Pressure and temperature distributions of sealing rings are numerically calculated for the cases with different deflection angle, rational speed, seal pressure and ambient temperature. Then, the hydrodynamic effect and sealing performance are analyzed. The obtained results show that, the surface Rayleigh step grooves do not present obvious hydrodynamic effect when split seal ring has no deflection. While, a significant hydrodynamic effect can be obtained when the split seal ring presents a deflection angle about dozens of micro radians. Here, a 10% increase of opening force is achieved when the deflection angle reaches 80 μrad in the case of speed 30,000 r/min and seal pressure 0.2 MPa. Moreover, the hydrodynamic effect becomes obvious with increasing deflection angle as well as rotational speed. Meanwhile, the growth of rotational speed results in an obvious increase of film temperature. The increase of ambient temperature has a significant influence on the decrease of leakage rate. When the ambient temperature increases from 340 K to 540 K, the leakage rate reduces exceeding 50%, however, it does not present obvious effect on the opening force. The proposed model has the potential to provide the theoretical basis and design guidance for surface grooves of gas split floating ring seal in the future.

Funder

National Natural Science Foundation of China

Basic Public Welfare Research Program of Zhejiang Province of China

Publisher

MDPI AG

Subject

General Materials Science

Reference26 articles.

1. Ludwig, L.P., and Strom, T.N. (1973). Improved Circumferential Shaft Seal for Aircraft Gear Transmissions, NASA. NASA-TN-D-7130.

2. Analytic modeling of floating ring annular seals;Arghir;J. Eng. Gas Turbines Power,2012

3. Experimental study on high-pressure gas seals for a liquid oxygen turbopump;Oike;Tribol. Trans.,1988

4. Gas hydrodynamic lubrication performance of split floating ring seals with Rayleigh step grooves;Yang;J. Propuls. Technol.,2022

5. Burcham, R.E., and Diamond, W.A. (1980). High-Pressure Hot-Gas Self-Acting Floating Ring Shaft Seal for Liquid Rocket Turbopumps, NASA. NASA-CR-165392.

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