Centrifugal compressor
A centrifugal compressor is provided. The centrifugal compressor includes a housing and a rotatable assembly mounted for rotation about an axis within the housing. The rotatable assembly includes an impeller forming part of a compressor stage. A first air intake is located at a first end of the apparatus, the first air intake providing an air source for the compressor stage and a second air intake is located at a second end of the apparatus. A thrust plate is attached to the rotatable assembly, the thrust plate including at least one interior channel so that air entering the second air inlet passes through the at least one interior channel.
1. An apparatus, comprising:
a housing;
a volute coupled to the housing;
a rotatable assembly mounted within the housing, the rotatable assembly comprising a shaft with an impeller coupled to the shaft;
a first air inlet located at a first end of the apparatus, the first air inlet providing a first air source;
a second air inlet located at a second end of the apparatus, the second air inlet providing a second air source; and
a thrust plate coupled to the rotatable assembly, the thrust plate comprising a disk-shaped center element having two sides and a plurality of grooves located on at least one of the two sides, and two disk-shaped outer elements, with one outer element positioned on each side of the center element, with all three elements coupled to the rotatable assembly so that the three elements rotate with the rotatable assembly.
2. The apparatus of claim 1 , where the at least one interior channel comprises a groove extending in a substantially radial direction inside the thrust plate with an inlet located adjacent to a rotational axis of the shaft and an outlet located at a perimeter of the thrust plate.
3. The apparatus of claim 1 , where air enters the second air inlet, passes though the at least one interior channel in the thrust plate, and then exits the apparatus though an aperture located in the second end of the apparatus.
4. The apparatus of claim 1 , further comprising a motor rotor coupled to the shaft, the motor rotor forming an armature of a motor for driving the rotating assembly about a rotational axis.
5. The apparatus of claim 1 , where both the first air source and the second air source are structured to receive air at an ambient pressure.
6. The apparatus of claim 1 , further comprising a third air inlet, the third air inlet comprising a plurality of apertures located on the compressor housing.
7. The apparatus of claim 6 , where air enters the plurality of apertures located on the compressor housing and flows substantially parallel to a rotational axis of the shaft toward the volute, and then turns back and again flows substantially parallel to the rotational axis of the shaft, but away from the volute.
8. The apparatus of claim 7 , where the air flowing away from the volute exits the apparatus though an aperture located in the second end of the apparatus.
9. An apparatus, comprising:
a housing;
a volute coupled to the housing;
a rotatable assembly mounted within the housing, the rotatable assembly comprising a shaft with an impeller coupled to the shaft;
a first air inlet located at a first end of the apparatus, the first air inlet providing a first air source;
a second air inlet located at a second end of the apparatus, the second air inlet providing a second air source;
a third air inlet comprising a plurality of apertures located on the housing and providing a third air source; and
a plurality of air outlets located on a rear housing cover, and positioned radially outward from the second air inlet.
10. The apparatus of claim 9 , where air enters the plurality of apertures located on the housing and flows substantially parallel to a rotational axis of the shaft toward the volute, and then turns back and again flows substantially parallel to the rotational axis of the shaft, but away from the volute.
11. The apparatus of claim 9 , further comprising a thrust plate coupled to the rotatable assembly, the thrust plate including at least one interior channel so that air entering the second air inlet passes through the at least one interior channel.
12. The apparatus of claim 11 , where the at least one interior channel comprises a groove extending in a substantially radial direction inside the thrust plate with an inlet located adjacent to a rotational axis of the shaft and an outlet located at a perimeter of the thrust plate.