TY - JOUR
T1 - A novel bio-inspired compound restrictor for high-precision aerostatic bearings
T2 - design and evaluation
AU - Chen, Xiuyuan
AU - Luo, Xichun
AU - Sun, Yazhou
AU - Zhong, Wenbin
AU - Walker, Charles
AU - Tian, Yankang
AU - Wang, Zhengjian
AU - Chang, Wenlong
AU - Wardle, Frank
PY - 2026/1/1
Y1 - 2026/1/1
N2 - Compound restrictors are widely adopted in aerostatic bearings due to their good static performance and ease of fabrication. However, further enhancement of their performance using surfaces with groove structures designed is still rarely researched. Inspired by the unique fluid controllability of the biomimetic hexagonal micro-pattern, this paper proposes a novel bio-inspired aerostatic bearing design to realize high stability without compromising load capacity and static stiffness. Air mass flow rate, another key factor affecting its static performance, is also considered. Computational fluid dynamics (CFD) simulation study reveals that setting suitable divergence angle enables better pressurized airflow controllability. The key structural parameters were calculated using the resistance network method (RNM). The results were further verified through experimental measurements. Performance tests of the prototyped aerostatic linear motion stage verified the theoretical modelling accuracy. A positioning accuracy (perpendicular to the stage feed direction) of less than 15 nm/10 mm was achieved, which was almost half of that of the conventional linear bearing stage under the same conditions (8 μm bearing clearance, 0.2 MPa supply pressure).
AB - Compound restrictors are widely adopted in aerostatic bearings due to their good static performance and ease of fabrication. However, further enhancement of their performance using surfaces with groove structures designed is still rarely researched. Inspired by the unique fluid controllability of the biomimetic hexagonal micro-pattern, this paper proposes a novel bio-inspired aerostatic bearing design to realize high stability without compromising load capacity and static stiffness. Air mass flow rate, another key factor affecting its static performance, is also considered. Computational fluid dynamics (CFD) simulation study reveals that setting suitable divergence angle enables better pressurized airflow controllability. The key structural parameters were calculated using the resistance network method (RNM). The results were further verified through experimental measurements. Performance tests of the prototyped aerostatic linear motion stage verified the theoretical modelling accuracy. A positioning accuracy (perpendicular to the stage feed direction) of less than 15 nm/10 mm was achieved, which was almost half of that of the conventional linear bearing stage under the same conditions (8 μm bearing clearance, 0.2 MPa supply pressure).
KW - aerostatic bearing
KW - positioning accuracy
KW - biomimetic structure
KW - computational fluid dynamics
KW - finite difference method
UR - https://doi.org/10.17868/strath.00094362
U2 - 10.1016/j.precisioneng.2025.09.025
DO - 10.1016/j.precisioneng.2025.09.025
M3 - Article
SN - 0141-6359
VL - 97
SP - 348
EP - 366
JO - Precision Engineering
JF - Precision Engineering
ER -