Abstract
This work proposes a novel hybrid gas-magnetic bearing (HGMB) which has single bearing structure. The gas bearing and the active magnetic bearing (AMB) share the same airgap, and the closed magnetic poles are taken as the bushing of the gas bearing. Controllable electromagnetic forces are applied to adjust system dynamic characteristics. Numerical results demonstrate better rotating accuracy, suppressed sub-synchronous vibration, lower energy consumption compared with rigid gas bearings and AMB, and less air friction losses than conventional HGMBs, indicating the suitability of the proposed bearing for cryogenic turbomachinery.
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Abbreviations
- AMB:
-
Active magnetic bearing
- AMD:
-
Active magnetic damper
- C h :
-
Nominal airgap of the single-structured HGMB (m)
- C g :
-
Nominal airgap of the rigid self-acting gas bearing (m)
- FDM:
-
Finite difference method
- FEM:
-
Finite element modeling
- GFB:
-
Gas foil bearing
- h min :
-
Minimum gas film thickness of the HGMB (m)
- H :
-
Dimensionless gas film thickness (m)
- HFMB:
-
Hybrid foil-magnetic bearing
- HGMB:
-
Hybrid gas-magnetic bearing
- Mode A:
-
Rigid gas bearing
- Mode B:
-
Active magnetic bearing
- Mode C:
-
Single-structured HGMB in aerodynamic mode
- Mode D:
-
Single-structured HGMB in full hybrid mode
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Acknowledgements
The authors are grateful for the supports of the Program of the National Natural Science Foundation of China (No. 51836009) and research fund of State Key Laboratory of Technologies in Space Cryogenic Propellants.
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Liu, Q., Wang, L., Li, Y. et al. Single-structured hybrid gas-magnetic bearing and its rotordynamic performance. Nonlinear Dyn 104, 333–348 (2021). https://doi.org/10.1007/s11071-021-06295-5
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DOI: https://doi.org/10.1007/s11071-021-06295-5