2021
DOI: 10.1016/j.ymssp.2020.106983
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Nonlinear study on a rigid rotor supported by herringbone grooved gas bearings: Theory and validation

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Cited by 37 publications
(18 citation statements)
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“…The forces acting on the rotor are its weight, the total aerodynamic force, and an eventual imbalance force if the axis of inertia of the rotor is shifted from the axis of rotation (static imbalance). Using the non‐dimensional parameters defined in Reference 45, the governing equations of the rotor dynamics in the (fixed) reference frame of the bearing bushing are given by: alignleftalign-1rightmrd2ϵxdτ2align-2=mrg+Fx+Ūimcos(2τ)$$ {\overline{m}}_r\frac{{\mathrm{d}}^2{\epsilon}_x}{\mathrm{d}{\tau}^2}\kern0.5em ={\overline{m}}_r\overline{g}+{\overline{F}}_x+{\bar{U}}_{im}\cos \left(2\tau \right) $$ alignleftalign-1rightmrd2ϵydτ2align-2=Fy+Ūimsin(2τ)$$ {\overline{m}}_r\frac{{\mathrm{d}}^2{\epsilon}_y}{\mathrm{d}{\tau}^2}\kern0.5em ={\overline{F}}_y+{\bar{U}}_{im}\sin \left(2\tau \right) $$ where τ=ωtfalse/2$$ \tau =\omega t/2 $$, with ω$$ \omega $$ the rotation speed of the rotor, and where trueFx$$ {\overline{F}}_x $$ and trueFy$$ {...…”
Section: Parametric Reduced Order Model Of a Gas Bearings Supported T...mentioning
confidence: 99%
“…The forces acting on the rotor are its weight, the total aerodynamic force, and an eventual imbalance force if the axis of inertia of the rotor is shifted from the axis of rotation (static imbalance). Using the non‐dimensional parameters defined in Reference 45, the governing equations of the rotor dynamics in the (fixed) reference frame of the bearing bushing are given by: alignleftalign-1rightmrd2ϵxdτ2align-2=mrg+Fx+Ūimcos(2τ)$$ {\overline{m}}_r\frac{{\mathrm{d}}^2{\epsilon}_x}{\mathrm{d}{\tau}^2}\kern0.5em ={\overline{m}}_r\overline{g}+{\overline{F}}_x+{\bar{U}}_{im}\cos \left(2\tau \right) $$ alignleftalign-1rightmrd2ϵydτ2align-2=Fy+Ūimsin(2τ)$$ {\overline{m}}_r\frac{{\mathrm{d}}^2{\epsilon}_y}{\mathrm{d}{\tau}^2}\kern0.5em ={\overline{F}}_y+{\bar{U}}_{im}\sin \left(2\tau \right) $$ where τ=ωtfalse/2$$ \tau =\omega t/2 $$, with ω$$ \omega $$ the rotation speed of the rotor, and where trueFx$$ {\overline{F}}_x $$ and trueFy$$ {...…”
Section: Parametric Reduced Order Model Of a Gas Bearings Supported T...mentioning
confidence: 99%
“…Then the expression of the partial derivative of pressure with respect to the coordinate axis direction in the Reynolds equation can be obtained: (12) Substitute Formula (12) into the Reynolds equation in the Cartesian coordinate system and organize the static Reynolds equation in the oblique coordinate system as:…”
Section: Static Reynolds Equationmentioning
confidence: 99%
“…The research on herringbone grooved journal bearings mainly focuses on the optimization of the performance of the herringbone grooves and their structural parameters [10][11][12]. Eliott et al used herringbone grooves to improve bearing performance [13][14][15].…”
Section: Introductionmentioning
confidence: 99%
“…The effects of the parameters of the grooves in the bearing pad surfaces on the load performance of the three-pad aerodynamic bearing were investigated. By two-dimensional narrow groove theory, a model of a rigid rotor with herringbone-grooved journal gas bearing support was established by Liu et al 18 The onset speed of the sub-synchronous vibration of the rotor system was predicted by the theoretical model and experimental data. In order to reduce the gas film vortex and oscillation and improve the operation stability of rotor system supported in spherical spiral groove hybrid gas bearing, Jia et al 19 investigated the dynamic change of the gas film stiffness and damping coefficients under different motion conditions.…”
Section: Introductionmentioning
confidence: 99%