Turbo compressor comprising bearing cooling channel
View Patent ↗Provided is a turbo compressor including a compressed gas inlet through which a gas is sucked in, an impeller for compressing the gas introduced through the compressed gas inlet, a compressed gas outlet through which the gas compressed by the impeller is discharged to the outside, a compression unit including a compressed gas channel connected from the compressed gas inlet to the compressed gas outlet, a motor including a rotating shaft having an end coupled to the impeller, to rotate the impeller, a housing including a motor accommodation space for accommodating the motor, a cooling air channel provided to pass through the motor accommodation space and formed to circulate a cooling gas accommodated therein, a cooling water channel formed to circulate a cooling liquid capable of cooling the housing, and thrust bearings disposed at an end of the rotating shaft, wherein the cooling water channel includes bearing cooling water channels disposed within a predetermined distance from the thrust bearings to cool the thrust bearings. According to the present invention, the thrust bearings supporting the rotating shaft and the cooling gas accommodated in front air channels adjacent to the bearing cooling water channels may be very rapidly cooled.
1. A turbo compressor capable of compressing a gas and supplying the compressed gas to outside, the turbo compressor comprising:
a compressed gas inlet through which the gas is sucked in;
an impeller for compressing the gas introduced through the compressed gas inlet;
a compressed gas outlet through which the gas compressed by the impeller is discharged to the outside;
a compression unit comprising a compressed gas channel connected from the compressed gas inlet to the compressed gas outlet;
a motor comprising a rotating shaft having an end coupled to the impeller, to rotate the impeller;
a housing comprising a motor accommodation space for accommodating the motor;
a cooling air channel provided to pass through the motor accommodation space and formed to circulate a cooling gas accommodated therein;
a cooling water channel formed to circulate a cooling liquid capable of cooling the housing; and
thrust bearings disposed at an end of the rotating shaft,
wherein the cooling water channel comprises bearing cooling water channels disposed within a predetermined distance from the thrust bearings to cool the thrust bearings,
wherein the rotating shaft comprises a thrust bearing runner corresponding to the thrust bearings,
wherein the bearing cooling water channels are provided within a predetermined distance from the thrust bearing runner,
wherein the bearing cooling water channels extend by a predetermined length along radial directions of the rotating shaft to allow the cooling liquid to flow along the radial directions of the rotating shaft such that the bearing cooling water channels cover a total area of front air channels of the cooling air channel and the thrust bearings, the front air channels being provided between the bearing cooling water channels and the thrust bearings and configured to allow the cooling gas to flow from an edge of an front end of the housing toward a center of the front end of the housing,
wherein the bearing cooling water channels have a fan shape with an upper width located farther from the rotating shaft greater than a lower width located closer from the rotating shaft and are arranged along a circumferential direction of the rotating shaft.
2. The turbo compressor of claim 1 , further comprising a journal bearing disposed between the impeller and the thrust bearings as a bearing supporting the rotating shaft,
wherein the journal bearing is disposed under the bearing cooling water channels.
3. The turbo compressor of claim 2 , wherein the thrust bearings and the journal bearing are air bearings.
4. The turbo compressor of claim 1 , wherein the cooling air channel comprises air channels penetrating through the housing to cool the housing, and
wherein the cooling water channel comprises water channels penetrating through the housing to cool the housing.
5. The turbo compressor of claim 4 , wherein the cooling water channel is provided to exchange heat with the cooling gas accommodated in the cooling air channel, and
wherein the air channels penetrating through the housing and the water channels penetrating through the housing extend along a longitudinal direction of the rotating shaft and alternately disposed along the circumferential direction of the rotating shaft.
6. The turbo compressor of claim 1 , wherein the rotating shaft comprises a hollow extending along a longitudinal direction, and
wherein the cooling air channel comprises an air channel penetrating through the hollow of the rotating shaft.
7. The turbo compressor of claim 1 , wherein the rotating shaft comprises:
a plurality of members comprising a hollow extending along a longitudinal direction; and
a tie bolt extending along the longitudinal direction of the rotating shaft to sequentially penetrate through the hollow of the plurality of members and to detachably couple the plurality of members to the impeller.
8. The turbo compressor of claim 1 , wherein the compressed gas channel is spatially separate from the cooling air channel to prevent the gas inside the compressed gas channel from penetrating into the cooling air channel, and
wherein the turbo compressor further comprises a cooling fan for forcibly circulating the cooling gas accommodated in the cooling air channel.
9. The turbo compressor of claim 8 , wherein the cooling fan is disposed at a rear end of the rotating shaft and rotated by torque of the rotating shaft.
10. The turbo compressor of claim 6 , wherein the cooling air channel comprises an air channel through which the gas is discharged to a front side of the impeller after penetrating through the hollow of the rotating shaft.