Experiments have been conducted with two type of gas lubricated foil joumal bearings and a small cryogenic turboexpander. One of these bearings is named as a spirally-wound foil bearing and the another is namedas a multi-leaves foil bearing. Both ofthem have much simpler construction and lower cost as compared with the conventional foil bearings. The rotor ofcryogenic turboexpander, 103 mm long and weighing 0.9 N, has the work.ing speed up to 230,000 rpm. The main purpose ofthe investigation is a preliminary examination of stabilizing characteristics of those foil bearings under several different clearances and foil stiffuess as weil as the durability of the foils. Experimental results indicate the foil bearings presented here offer system stability and high durability, and it confirmed that the application of gas foil bearing to the cryogenic turboexpander is feasible and hopeful.
CITATION STYLE
Xiong, L.-Y., Wu, G., Chen, C.-Z., & Li, Y.-Z. (1998). A Feasibility Study on the Use of New Gas Foil Bearings in Cryogenic Turboexpander. In Advances in Cryogenic Engineering (pp. 661–665). Springer US. https://doi.org/10.1007/978-1-4757-9047-4_81
Mendeley helps you to discover research relevant for your work.