Benefits of controlled inclination for contactless transport by squeeze-film levitation

Abstract

Developed in this paper is a theoretical description of the fluid flow involved in contactless transport systems that operate using squeeze-film levitation. Regular perturbation methods are employed to solve the appropriate Reynolds equation that governs the viscous, compressible flow of air in the slender film separating the oscillator and the levitated object. The resulting reduced formulation allows efficient computation of the time-averaged levitation force and moment induced by fluid pressure, as well as the accompanying quasistatic thrust force that accounts additionally for shear stresses. Investigated, in particular, is the possibility of combining two distinct methods of thrust generation that have been experimentally demonstrated in previous studies – (i) inclination of the levitated body and (ii) generation of asymmetrical flexural deformations, such as travelling waves, on the oscillator surface – the latter of which is shown to allow a transition from the typically repulsive levitation force to one that is attractive. Computations reveal that systematic control of the inclination angle can provide significant performance benefits for squeeze-film transport systems. In the case of attractive levitation, the amount of improvement that can be obtained appears to correlate closely with the degree of lateral asymmetry exhibited by the flexural oscillations.

Controlling the motion of gas-lubricated adhesive disks using multiple vibration sources

“…A recent theoretical study claims that asymmetrical flexural oscillations of a flat plate can be used to achieve thrust forces with adhesive levitation ( Ramanarayanan and Sánchez, 2023 ), but to the best of our knowledge, there has yet been no experimental proof of this proposition. In this paper, we demonstrate, for the first time, the ability of an oscillated robotic disk to achieve adhesion to a flat surface while generating linear movement and rotation with low air resistance (see in Figures 1A, B ).…”