Abstract
The gas-film-lubricated mechanical face seal is a combined hydrodynamic and hydrostatic seal with positive leakage. Up to now, it has been widely accepted by end, users and builders of high-speed turbo compressors. The groove technology on the sealing face of the seat is one of the core technologies of dry gas seals. This article presents a patented herringbone spiral-grooved gas seal. Its one-dimensional analytical solution and two-dimensional numerical solution methods for the gas-film pressure distribution on the sealing face are presented. Up to now, more than 200 gas seals adopting this groove technology have been applied successfully in high-speed turbo compressors that deal with dangerous process gas in the oil refinery and petrochemical industries. The theoretical analyses and field applications show that gas seals with herringbone spiral grooves are advanced and practicable.
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