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An application of the boundary element method (BEM)ris presented to calculate the behaviors of a spiral grooved thrust bearing (SGTrrnB). The basic reason is that the SGTB has very complex boundary conditions that rrncan hinder the effective or sufficient applications of the finite difference metrrnhod (FDM) and the finite element method (FEM), despite some existing work based rrnon the FDM and the FEM. In order to apply the BEM, the pressure control equationrrn, ie, Reynolds equation, is first transformed into Laplaces and Poissonrrns form of the equations. Discretization of the SGTB with a set of boundary elerrnments is thus explained in detail, which also includes the handling of boundary rrnconditions. The Archimedean SGTB is chosen as an example of the application of BrrnEM, and the relationship between the behaviors and structure parameters of the brrnearing are found and discussed through this calculation. The obtained results larrny a solid foundation for a further work of the design of the SGTB.rnrn is presented to calculate the behaviors of a spiral grooved thrust bearing (SGTrrnB). The basic reason is that the SGTB has very complex boundary conditions that rrncan hinder the effective or sufficient applications of the finite difference metrrnhod (FDM) and the finite element method (FEM), despite some existing work based rrnon the FDM and the FEM. In order to apply the BEM, the pressure control equationrrn, ie, Reynolds equation, is first transformed into Laplaces and Poissonrrns form of the equations. Discretization of the SGTB with a set of boundary elerrnments is thus explained in detail, which also includes the handling of boundary rrnconditions. The Archimedean SGTB is chosen as an example of the application of BrrnEM, and the relationship between the behaviors and structure parameters of the brrnearing are found and discussed through this calculation. The obtained results larr
y a solid foundation for a further work of the design of the SGTB.