International Journal of Rotating Machinery / 2017 / Article / Fig 14

Research Article

Development and Application of Integrated Aerodynamic Protuberant Foil Journal and Thrust Bearing in Turboexpander

Figure 14

Rotor orbits and vibrations in and directions: (a) 30000 rpm; (b) 40000 rpm; (c) 50000 rpm.
(a)
(b)
(c)