Multi-stage centrifugal compressor driven by integral high speed motor

• US 6,579,078 B2
• Filed: 04/23/2002
• Issued: 06/17/2003
• Est. Priority Date: 04/23/2001
• Status: Expired due to Term

• Current Assignee: Earnest Pacific Limited
• Original Assignee: Elliot Turbomachinery Company Incorporated
• Inventors: Hill, M. Raymond, Grbic, Milovan R.
• Primary Examiner(s): Freay, Charles G.
• Assistant Examiner(s): Rodriguez, William H.
• Application Number:
  US10/128,136
• Publication Number:
  US 20020192089A1
• Time in Patent Office: 420 Days
• Field of Search: 417/423.7, 417/372, 417/423.8, 417/423.12, 417/423.13, 417/423.11, 417/228, 417/423.5, 310/58, 310/60.R, 310/62, 310/63, 310/60.A, 310/64
• US Class Current: 417/423.7
• CPC Class Codes: F04D 17/122 the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
• CPC Class Codes: F04D 25/06 the pump being electrically driven F04D25/08 takes precedence
• CPC Class Codes: F04D 29/057 hydrostatic; hydrodynamic
• CPC Class Codes: F04D 29/063 specially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/5806 Cooling the drive system
• CPC Class Codes: F04D 29/584 cooling or heating the machine F04D29/5846, F04D29/5853 take precedence
• CPC Class Codes: F05D 2260/85 Starting
• CPC Class Codes: F16C 2360/44 Centrifugal pumps in general F04D
• CPC Class Codes: F16C 2380/26 Dynamo-electric machines or combinations therewith, e.g. electro-motors and generators in general H02K
• CPC Class Codes: F16C 33/10 Construction relative to lubrication lubrication in general F16N
• CPC Class Codes: H02K 1/278 Surface mounted magnets; Inset magnets
• CPC Class Codes: H02K 2205/12 Machines characterised by means for reducing windage losses or windage noise
• CPC Class Codes: H02K 5/1672 radially supporting the rotary shaft at both ends of the rotor H02K5/1677 takes precedence
• CPC Class Codes: H02K 9/19 for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil

Abstract

A multi-stage centrifugal compressor with an integral high-speed motor for compressing air has a variable speed permanent magnet motor having electronically commutated stator coils surrounding a rotor carrying permanent magnets, wherein there is a gap between the coils and the rotor. The rotor has a magnetic steel rotor shaft rotatably supported at each end by pressurized oil lubricated hydrodynamic bearings. The stator coils have a plurality of stator wires extending longitudinally along the stator and continuing around the ends of the stator to define end turns. The compressor also has a plurality of compressor impellers mounted to turn with the rotor shaft and cooler for cooling the bearings, rotor and stator coils comprising a pump for introducing cooled oil into the bearings, said bearing configured so that oil exiting from the bearings splashes over the supported ends of the shaft and splashes over the end turns of the stator coils. There is a passageway through the stator for introducing pressurized air within a gap between the stator and the rotor during start up to maintain a positive pressure within the gap thereby displacing oil from the gap.

Claims

1. A multi-stage centrifugal compressor with an integral high-speed motor for compressing air comprising:

a) a variable speed permanent magnet motor having electronically commutated stator coils surrounding a rotor carrying permanent magnets, wherein there is a gap between the coils and the rotor, said rotor having a magnetic steel rotor shaft rotatably supported at each end by pressurized oil lubricated hydrodynamic bearings, wherein the stator coils are comprised of a plurality of stator wires extending longitudinally along the stator and continuing around the ends of the stator to define end turns;

b) a plurality of compressor impellers mounted to turn with the rotor shaft,

c) a pump for introducing cooled oil into the bearings for lubricating the bearings and for cooling the bearings, rotor and stator coils, said bearing configured so that oil exiting from the bearings splashes over the supported ends of the shaft and splashes over the end turns of the stator coils, and

d) passageway through the stator for introducing pressurized air during start up to maintain a positive pressure within the gap thereby displacing oil from the gap.

2. The compressor according to claim 1 further comprising means for terminating the introduction of pressurized air to the gap when the motor has reached a predetermined speed.

3. The compressor according to claim 1, wherein compressed air from an external source is introduced into the gap during start up.

4. The compressor according to claim 1, wherein the stator coil is supported by laminations and wherein the passageway extends through the stator coil laminations midway between the axial ends of the rotor shaft.

5. The compressor according to claim 1, wherein the rotor shaft has an axial hole extending therethrough to accept oil for cooling.

6. A multi-stage centrifuigal compressor with integral high-speed motor comprising

a) variable speed permanent magnet motor having electronically commutated stator coils surrounding a rotor carrying permanent magnets, said rotor having a magnetic steel shaft rotatably supported by bearings,

b) a plurality of compressor impellers mounted to turn with the rotor shaft,

c) said rotor comprising:

1) said steel shaft having a square cross-section defined by four faces parallel to the rotating axis of the shaft,

2) said permanent magnets defined by a cylindrical surface and a flat surface and having a circular segment shaped cross-section secured to each of the four faces of the square steel shaft, said magnets arranged with alternating polarity, and

3) prestressed carbon graphite fiber reinforced plastic binding for holding the permanent magnets onto the shaft.

7. The compressor according to claim 6 further comprising a hall effect magnetic sensor proximate to the rotor for detecting a change in polarity of the magnetic field of the rotor as a corner of the square cross-sectioned shaft rotates past the sensor.

8. The compressor according to claim 6 wherein the magnets are positioned on the shaft to define a continuous cylindrical surface.

9. The compressor according to claim 8 wherein edges of each magnet are positioned adjacent to the edges of magnets having opposite polarity.

10. The compressor according to claim 8 wherein edges of the magnets defined by the cylindrical surface thereof and the flat surface thereof abut the edges of magnets of opposite polarity.

11. A method of starting a multi-stage centrifugal compressor with an integral high-speed motor, wherein the motor has a stator and a rotor rotationally supported therein defining a gap therebetween and wherein the rotor is supported at each end by hydrodynamic oil bearings, wherein the method is comprised of the steps of:

a) injecting pressurized air within the gap at a position between the ends of the rotor as the rotor begins to rotate to minimize the entry of oil from the bearings into the gap and

b) when the rotor reaches a rotational speed sufficient to centrifugally expel oil outwardly from the rotor ends and away from the gap, discontinuing the injection of air.