Claims
- 1. A turbo-compressor air supply system which supplies air to a paint spray system at an elevated pressure, the turbo-compressor includes a housing, a rotatable vertically-disposed drive shaft centrally disposed within the housing, a bearing housing which houses a concentrically disposed bearing, the drive shaft including a series of flanges disposed below the housing, the system comprising:
- (a) a rotatable section centrally disposed about the shaft, the section including a first rotor and a second rotor, each rotor having a central passage for mounting about the shaft, each rotor having an air-inlet side and an air-outlet side, each rotor comprising a first series of blades spirally arrayed about the central passage, the first series of blades being sandwiched between a first pair of plates, the rotors being rotatably driven in the same direction as the shaft as the air is directed onto the blades, and the rotors being coaxial with the shaft, and the rotatable section also including a tubular sleeve which mounted about the shaft, the tubular sleeve separating the rotor, and the tubular sleeve being rotatable with the rotors and the shaft in the same direction as the rotors and the shaft, the air being expelled from the second rotor and circulated through the paint spray gun; and
- (b) a stationary section centrally disposed about the shaft, the stationary section including a first stator, the stator having a central passage for mounting about the shaft, the stator comprising a series of vanes spirally arrayed around the stator central passage, the stator vanes being sandwiched between a pair of stator plates, the stator being coaxial with the shaft, the vanes of the stationary section guiding the air leaving the air-outlet side of the first rotor to the air-inlet side of the second rotor;
- whereby, some of the circulated air being expelled from the turbo-compressor is diverted through the flanges on the drive shaft and across the plane bearing.
- 2. The turbo-compressor of claim 1, wherein the stationary section includes a second stator, the second stator being similar to the first stator, the stationary section including a ring which is mounted between and separating the first stator and the second stator.
- 3. The turbo-compressor of claim 1, wherein air enters through the top of the turbo-compressor and exits through the bottom thereof.
- 4. The turbo-compressor of claim 1, further comprising a noise suppressor disposed beneath the plane bearing to reduce the noise generated by the flow of air through the turbo-compressor.
- 5. A method of supplying air through a turbo-compressor at an elevated pressure, the turbo-compressor including a housing, a rotatable vertically-disposed drive shaft centrally disposed within the housing, a bearing housing which houses a concentrically disposed bearing, the drive shaft including a series of flanges disposed below the housing, the method comprising:
- (a) rotating a centrally disposed drive shaft within the housing of a turbo-compressor, the drive shaft having a first rotor disposed thereabout, the rotor being rotatable about the shaft, the rotor having a series of blades sandwiched between two plates, the blades being spirally arrayed from the center of the rotor, the rotor having an air-inlet side and an air-outlet side:
- (b) providing air to the top of a turbo-compressor and into fluid communication with the air-inlet side of the first rotor:
- (c) guiding the air into the air-inlet side of a second rotor by a stator which is centrally disposed about the shaft, the stator having a series of blades sandwiched between two plates, the air circulating through the blades which are spirally arrayed about the shaft;
- (d) driving a second rotor about the shaft with the circulated air, the second rotor being separated from the first rotor by a tubular sleeve which is centrally disposed about the shaft, the air being increasingly pressurized and accelerated as it leaves the second rotor;
- (e) withdrawing the pressurized air from the turbo-compressor, and supplying some of the air to a paint spray system which is in fluid communication with the base of the turbo-compressor and supplying the rest of the air being discharged from the turbo-compressor through the flanges on the drive shaft and across the plane bearing.
- 6. The method of claim 5, further comprising redirecting the pressurized air leaving the second rotor by a second stator, the first stator and the second stator being separated by a ring which is centrally disposed about the drive shaft, and the stators and the ring being stationary relative to the shaft and the rotors.
- 7. The method of claim 5, wherein each rotor and each stator are alternately disposed about the shaft.
- 8. The method of claim 7, wherein the air fills the housing and is flung outward by the centrifugal force of the rotor, and is forced between the blades of the rotor where it drives the rotor around at an increasing speed.
- 9. The method of claim 6, wherein the guided air impinges upon the blades of each rotor, and thereby driving each rotor around the shaft at an increasing speed.
- 10. A portable paint spray unit comprising:
- (a) a drive motor having a drive shaft, the drive motor being disposed within a motor casing;
- (b) a turbo-compressor including a housing mounted on the base, the turbo-compressor including a housing, and a rotatable vertically-disposed drive shaft centrally disposed within the housing, the turbo-compressor having a bearing housing which houses a concentrically disposed bearing, the drive shaft including a series of flanges disposed below the housing, the turbo-compressor having a drive shaft projecting from the housing into the chamber, the turbo-compressor having an air intake disposed at the top of the drive shaft, the turbo-compressor having an air outlet disposed at the bottom of the drive shaft, the air outlet being attachable to a paint spray system, the air outlet being in fluid communication with the chamber, some of the circulated air being discharged from the turbo-compressor being diverted through the flanges on the drive shaft and across the plane bearing;
- (c) drive train means which couple the shaft of the drive motor to the drive shaft of the turbo-compressor;
- (d) a noise suppressor being disposed beneath the turbo-compressor and the drive motor, the noise suppressor reducing the noise generated by the flow of air through the turbo-compressor.
CROSS REFERENCE TO RELATED APPLICATIONS
This is a Continuation-In-Part of patent application Ser. No. #067,305 entitled by Denis W. Toth, which was filed on June 27, 1987, in the United States Patent Office.
US Referenced Citations (6)
Foreign Referenced Citations (2)
Number |
Date |
Country |
165198 |
Oct 1958 |
SEX |
1492644 |
Nov 1977 |
GBX |
Continuation in Parts (1)
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Number |
Date |
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Parent |
67305 |
Jun 1987 |
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