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This invention provides a blower design capable of high temperature operation due to use of a self-sustaining cooling scheme through a sealed motor housing in which a cooling circuit can be created, and the use of a thermal barrier across which a temperature gradient may be formed. The thermal barri

This invention provides a blower design capable of high temperature operation due to use of a self-sustaining cooling scheme through a sealed motor housing in which a cooling circuit can be created, and the use of a thermal barrier across which a temperature gradient may be formed. The thermal barrier may be formed by a thermal choke plate assembly positioned between a hot side and a cold side of the blower to dissipate heat conducted from the hot side. Alternatively, the thermal barrier may be formed by an internal fan ring provided with the blower's rotating assembly to dissipate heat conducted from the blower's impeller. The thermal choke plate assembly and the fan ring may further be used in combination to block heat transfer by all modes between a hot side and a cold side of the blower.

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1. A blower for processing a gas, comprising: (a) a blower hot side, including: a volute with a process gas inlet and a process gas outlet,a diffuser attached to the volute for directing the flow of the process gas through the volute, andan impeller mounted for rotation about a central longitudinal

1. A blower for processing a gas, comprising: (a) a blower hot side, including: a volute with a process gas inlet and a process gas outlet,a diffuser attached to the volute for directing the flow of the process gas through the volute, andan impeller mounted for rotation about a central longitudinal axis within the volute for processing the gas as it flows through the volute;(b) a blower cold side, including: a sealed motor housing defining an interior cavity,a rotating assembly disposed within the interior cavity of the motor housing, comprising: a rotating shaft mounted for rotation about the central longitudinal axis, anda motor rotor mounted on the rotating assembly for rotation with the rotating shaft,wherein the impeller is mounted at an end of the rotating assembly for rotation therewith; anda motor stator assembly mounted in stationary relationship within the motor housing relative to the rotor;(c) a thermal barrier positioned between the blower hot side and the blower cold side for reducing heat transfer from the blower hot side to the blower cold side; anda radiation heat shield positioned against the exterior surface of the volute adjacent to the thermal barrier for reflecting heat radiated from the blower hot side. 2. The blower of claim 1, wherein the thermal barrier is formed by a thermal choke plate assembly, comprising: an outer choke plate disposed adjacent to the blower hot side;an inner choke plate disposed adjacent to the blower cold side; anda transition between the outer choke plate and the inner choke plate;wherein heat transferred from the blower hot side is directed, in part, to the outer choke plate through the transition and to the inner choke plate, andfurther wherein heat is dissipated from the thermal choke plate assembly as it passes from the outer choke plate to the inner choke plate to form a temperature gradient across the hot and cold sides of the blower. 3. The blower of claim 2, wherein the inner choke plate has a greater surface area than the outer choke plate. 4. The blower of claim 2 wherein the thermal choke plate assembly further comprises a plurality of spacers between the outer choke plate and the inner choke plate, wherein heat may be directed from the outer choke plate to the inner choke plate through said spacers. 5. The blower of claim 2 wherein the transition of the thermal choke plate assembly is a neck portion located at the respective interior diameters of the outer and inner choke plates, said neck portion being disposed adjacent to the rotating assembly where heat from the rotating assembly may be conducted to the thermal choke plate assembly via the neck portion. 6. The blower of claim 2 wherein the radiation heat shield is positioned against the exterior surface of the volute adjacent to the outer choke plate for reflecting heat radiated from the blower hot side. 7. A blower for processing a gas, comprising: (a) a blower hot side, including: a volute with a process gas inlet and a process gas outlet,a diffuser attached to the volute for directing the flow of the process gas through the volute, andan impeller mounted for rotation about a central longitudinal axis within the volute for processing the gas as it flows through the volute;(b) a blower cold side, including: a sealed motor housing defining an interior cavity,a rotating assembly disposed within the interior cavity of the motor housing, comprising: a rotating shaft mounted for rotation about the central longitudinal axis, anda motor rotor mounted on the rotating assembly for rotation with the rotating shaft,wherein the impeller is mounted at an end of the rotating assembly for rotation therewith; anda motor stator assembly mounted in stationary relationship within the motor housing relative to the rotor, and;(c) a thermal barrier positioned between the blower hot side and the blower cold side for reducing heat transfer from the blower hot side to the blower cold side; wherein the thermal barrier comprises at least one of:a thermal choke plate assembly, comprising: an outer choke plate disposed adjacent to the blower hot side;an inner choke plate disposed adjacent to the blower cold side; anda transition between the outer choke plate and the inner choke plate;wherein said outer choke plate and said inner choke plate are axially spaced apart from one another and connected together by said transition such that heat transferred from the blower hot side to the outer choke plate is directed to the inner choke plate via the transition, andfurther wherein heat is dissipated from the thermal choke plate assembly as it passes from the outer choke plate to the inner choke plate to form a temperature gradient across the hot and cold sides of the blower; anda fan ring mounted on the rotating assembly between the impeller and the motor rotor, said fan ring comprising: a generally longitudinal hub portion having a first end and a second end and being mounted on the rotating assembly for rotation therewith;a radial cooling fan at the second end and having a plurality of fan blades facing the blower cold side; anda bellows feature positioned intermediate the first and second ends and including a plurality of heat fins extending radially from the hub portion,wherein heat conducted from the impeller is dissipated by the fan ring. 8. The blower of claim 7 wherein the bellows feature of the fan ring defines a seal within the blower to block the leakage of process gas from the blower hot side to the blower cold side. 9. The blower of claim 7 wherein the fan ring forms a part of the rotating shaft. 10. The blower of claim 7 wherein the impeller is attached to the first end of the fan ring. 11. A blower for processing a gas, comprising: (a) a blower hot side, including: a volute with a process gas inlet and a process gas outlet,a diffuser attached to the volute for directing the flow of the process gas through the volute, andan impeller mounted for rotation about a central longitudinal axis within the volute for processing the gas as it flows through the volute;(b) a blower cold side, including: a sealed motor housing defining an interior cavity,a rotating assembly disposed within the interior cavity of the motor housing, comprising: a rotating shaft mounted for rotation about the central longitudinal axis, anda motor rotor mounted on the rotating assembly for rotation with the rotating shaft,wherein the impeller is mounted at an end of the rotating assembly for rotation therewith; anda motor stator assembly mounted in stationary relationship within the motor housing relative to the rotor, and;(c) a thermal barrier positioned between the blower hot side and the blower cold side for reducing heat transfer from the blower hot side to the blower cold side; wherein the thermal barrier comprises: (i) a thermal choke plate assembly, comprising: an outer choke plate disposed adjacent to the blower hot side;an inner choke plate disposed adjacent to the blower cold side; anda transition between the outer choke plate and the inner choke plate;wherein heat transferred from the blower hot side is directed, in part, to the outer choke plate through the transition and to the inner choke plate, andfurther wherein heat is dissipated from the thermal choke plate assembly as it passes from the outer choke plate to the inner choke plate to form a temperature gradient across the hot and cold sides of the blower; and(ii) a fan ring mounted on the rotating assembly between the impeller and the motor rotor, said fan ring comprising: a generally longitudinal hub portion having a first end and a second end and being mounted on the rotating assembly for rotation therewith;a radial cooling fan at the second end and having a plurality of fan blades facing the blower cold side; anda bellows feature positioned intermediate the first and second ends and including a plurality of heat fins extending radially from the hub portion,wherein heat conducted from the impeller is dissipated by the fan ring. 12. The blower of claim 11 wherein the transition of the thermal choke plate assembly is a neck portion located at the respective interior diameters of the outer and inner choke plates, said neck portion being disposed adjacent to the fan ring where heat from the rotating assembly may be dissipated from the heat fins of the fan ring and conducted to the thermal choke plate assembly via the neck portion. 13. The blower of claim 11 wherein the bellows feature of the fan ring defines a seal within the blower to block the leakage of process gas from the blower hot side to the blower cold side with the tips of the heat fins being generally adjacent to the neck portion of the thermal choke plate assembly. 14. The blower of claim 11 further comprising a radiation heat shield positioned against the exterior surface of the volute adjacent to the outer choke plate for reflecting heat radiated from the blower hot side. 15. A rotating assembly for use in a centrifugal blower, comprising: a rotating shaft mounted for rotation about an axis;an impeller mounted at a first end of the rotating shaft;at least two hydrodynamic foil bearing assemblies mounted in association with the blower for supporting the rotating shaft;a motor rotor forming an armature of the blower, said rotor being mounted for rotation with the rotating shaft;a fan ring comprising: a generally longitudinal hub portion having a first end and a second end and being mounted for rotation with the rotating shaft;a radial cooling fan at the second end and having a plurality of fan blades facing the motor rotor; anda bellows feature positioned intermediate the first and second ends and including a plurality of heat fins extending radially from the hub portion,wherein heat conducted from the impeller may be dissipated by the fan ring; anda tie rod extending along the axis of rotation and holding the impeller, the rotating shaft, the motor rotor and the fan ring under preload. 16. The rotating assembly of claim 15 further comprising at least one hydrodynamic foil thrust bearing assembly having a thrust runner mounted for rotation with the rotating shaft adjacent a second end thereof opposing the impeller. 17. The rotating assembly of claim 15 wherein at least one of the hydrodynamic foil bearing assemblies comprises a foil gas conical bearing including: a conical sleeve mounted in the blower and having a conical opening adapted to receive the rotating shaft;a conical-shaped foil assembly comprising a conical inner foil and at least one corrugated elastic spring foil; anda retaining ring attached to the conical sleeve to prevent axial movement of the conical-shaped foil assembly. 18. The rotating assembly of claim 17 wherein the foil gas conical bearing is provided between the motor rotor and the impeller. 19. The rotating assembly of claim 17 wherein the foil gas conical bearing is provided between the motor rotor and the second end of the rotating shaft. 20. The rotating assembly of claim 17 comprising two foil gas conical bearings, one of which is provided between the motor rotor and the impeller and the other of which is provided between the motor rotor and the second end of the rotating shaft. 21. The rotating assembly of claim 15 wherein the fan ring forms a part of the rotating shaft. 22. The rotating assembly of claim 15 wherein the impeller is attached to the first end of the fan ring. 23. The rotating assembly of claim 15 further comprising a secondary axial fan mounted at a second end of the rotating shaft opposing the impeller. 24. A method of cooling a centrifugal blower comprising: providing a sealed blower housing having a front end and a rear end and defining an axial interior cavity, radially disposed cooling channels, a front end cavity and a rear end cavity;providing a plurality of cooling fins about the outer surface of the blower housing, said cooling fins being generally adjacent the radially disposed cooling channels inside the blower housing;providing a rotating assembly within the axial interior cavity, said rotating assembly being mounted for rotation about an axis and comprising a rotating shaft, an impeller mounted at a first end of the rotating shaft and being disposed within a volute, and a fan ring adjacent to the impeller, said fan ring having a radial cooling fan facing the rear end of the blower housing and including a plurality of fan blades;drawing gas through the axial interior cavity of the blower housing along the rotating assembly by rotating the radial cooling fan, said gas taking up heat from components of the rotating assembly;distributing the hot gas into the front end cavity;directing the hot gas to and through the radially disposed cooling channels;cooling the hot gas as it passes through the radially disposed cooling channels by conducting heat from the hot gas from the radially disposed cooling channels to the cooling fins where the heat may be released therefrom to the ambient air around the blower housing; anddistributing the cooled gas to the rear end cavity where it may be drawn into and through the axial interior cavity by rotation of the radial cooling fan. 25. The method of claim 24 further comprising reducing heat transfer from the impeller, wherein said reducing step includes providing a thermal choke plate assembly between the blower housing and the volute to dissipate heat generated by operation of the impeller, said thermal choke plate assembly comprising: an outer choke plate disposed adjacent to the volute;an inner choke plate disposed adjacent to the blower housing; anda transition between the outer choke plate and the inner choke plate;wherein heat transferred from the impeller and volute is directed, in part, to the outer choke plate through the transition and to the inner choke plate, andfurther wherein heat is dissipated from the thermal choke plate assembly as it passes from the outer choke plate to the inner choke plate to form a temperature gradient across the blower. 26. The method of claim 24 further comprising reducing heat transfer from the impeller, wherein said reducing step includes providing a radiation heat shield positioned against the exterior surface of the volute for reflecting heat radiated from the impeller and the volute. 27. The method of claim 24 further comprising reducing heat transfer from the impeller, wherein said reducing step includes providing a bellows feature having a plurality of radially extending heat fins on the fan ring, wherein heat conducted from the impeller is dissipated from the heat fins. 28. The method of claim 27 wherein said reducing step includes providing a thermal choke plate assembly between the blower housing and the volute to dissipate heat generated by operation of the impeller, said thermal choke plate assembly comprising: an outer choke plate disposed adjacent to the volute;an inner choke plate disposed adjacent to the blower housing; anda transition between the outer choke plate and the inner choke plate;wherein heat transferred from the impeller and volute is directed, in part, to the outer choke plate through the transition and to the inner choke plate, andfurther wherein heat is dissipated from the thermal choke plate assembly as it passes from the outer choke plate to the inner choke plate to form a temperature gradient across the blower. 29. The method of claim 27 wherein said reducing step further includes forming a seal with the heat fins of the fan ring to block flows of hot gas from the impeller into the blower housing. 30. A method of cooling a blower comprising: providing a blower hot side comprising a volute, a diffuser and an impeller, wherein the impeller is mounted for rotation with respect to the volute and the diffuser to process a gas as it flows through the blower hot side;providing a blower cold side comprising a sealed blower housing defining an axial interior cavity, radially disposed cooling channels, a front end cavity and a rear end cavity;providing a rotating assembly within the axial interior cavity, said rotating assembly being mounted for rotation about an axis and comprising a rotating shaft;mounting the impeller at a first end of the rotating shaft so that the impeller and the rotating shaft rotate together;forming a thermal barrier in the blower to separate the blower hot side from the blower cold side and to reduce heat transfer therebetween; andreflecting heat radiated from the blower hot side. 31. A method of cooling a blower comprising: providing a blower hot side comprising a volute, a diffuser and an impeller, wherein the impeller is mounted for rotation with respect to the volute and the diffuser to process a gas as it flows through the blower hot side;providing a blower cold side comprising a sealed blower housing defining an axial interior cavity, radially disposed cooling channels, a front end cavity and a rear end cavity;providing a rotating assembly within the axial interior cavity, said rotating assembly being mounted for rotation about an axis and comprising a rotating shaft;mounting the impeller at a first end of the rotating shaft so that the impeller and the rotating shaft rotate together; andforming a thermal barrier in the blower to separate the blower hot side from the blower cold side and to reduce heat transfer therebetween,wherein the thermal barrier is formed by at least one of:providing a thermal choke plate assembly between the blower hot side and the blower cold side to dissipate heat generated by operation of the impeller, said thermal choke plate assembly comprising: an outer choke plate disposed adjacent to the blower hot side;an inner choke plate disposed adjacent to the blower cold side; anda transition between the outer choke plate and the inner choke plate,wherein said outer choke plate and said inner choke plate are axially spaced apart from one another and connected together by said transition; andmounting a fan ring on the rotating assembly between the blower hot side and the blower cold side, said fan ring comprising: a generally longitudinal hub portion having a first end and a second end and being mounted on the rotating assembly for rotation therewith;a bellows feature positioned intermediate the first and second end and including a plurality of heat fins extending radially from the hub portion, anddissipating heat conducted from the impeller though said plurality of heat fins. 32. The method of claim 31 further comprising dissipating heat from the blower hot side to the ambient air by directing said heat to the outer choke plate, directing said heat from the outer choke plate through the transition,directing said heat from the transition to the inner choke plate, andtransferring said heat to ambient air as it is directed along the components of the thermal choke plate assembly. 33. The method of claim 31, a wherein said fan ring further comprises a radial cooling fan at the second end and having a plurality of fan blades facing the blower cold side, further wherein said method comprises cooling the blower cold side by drawing and distributing gas through the blower housing upon rotation of the radial cooling fan. 34. The method of claim 30 wherein the thermal barrier is formed by: (a) providing a thermal choke plate assembly between the blower hot side and the blower cold side to dissipate heat generated by operation of the impeller, said thermal choke plate assembly comprising: an outer choke plate disposed adjacent to the blower hot side,an inner choke plate disposed adjacent to the blower cold side, anda transition between the outer choke plate and the inner choke plate; and(b) mounting a fan ring on the rotating assembly between the blower hot side and the blower cold side, said fan ring comprising: a generally longitudinal hub portion having a first end and a second end and being mounted on the rotating assembly for rotation therewith, anda bellows feature positioned intermediate the first and second end and including a plurality of heat fins extending radially from the hub portion. 35. The method of claim 30 further comprising providing a radiation heat shield positioned against the exterior surface of the volute for reflecting heat radiated from the blower hot side.