Turbo-machine having bellows unit for automatic axial thrust control
AssigneeKorea Aerospace Research Institute
InventorsDae-Jin Kim, Jinhan Kim
Life of this patent
Estimating the term…
Loading patent…
AssigneeKorea Aerospace Research Institute
InventorsDae-Jin Kim, Jinhan Kim
Estimating the term…
A turbo-machine including a volute casing, a rotating shaft, an impeller, seals, an axial thrust control member and a bellows unit. The volute casing defines therein a fluid passage. The rotating shaft is rotatably provided in the volute casing. The impeller is coupled to the rotating shaft to draw fluid using centrifugal force. The seals are provided around the front and rear ends of the impeller to prevent leakage of fluid. The axial thrust control member is installed in the volute casing behind the impeller. The bellows unit includes the piston installed in the volute casing in a shape surrounding a circumferential outer surface of the axial thrust control member; and a bellows connected with one surface of the piston, the bellows having the predetermined elasticity; and an internal space, between the piston and the volute casing, isolated from the fluid drawn behind the impeller.
A turbo-machine, comprising:
Dependencies are inferred from the claim text.