Compact fan and impeller

• US 5,188,508 A
• Filed: 05/09/1991
• Issued: 02/23/1993
• Est. Priority Date: 05/09/1991
• Status: Expired due to Term

• Current Assignee: Motion Holdings, LLC (Gentherm Incorporated)
• Original Assignee: Comair Rotron Incorporated (Gentherm Incorporated)
• Inventors: Scott, Peter D., Bushnell, Peter
• Primary Examiner(s): Kwon, John T.
• Assistant Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US07/698,000
• Time in Patent Office: 656 Days
• Field of Search: 415/182.1, 415/203, 415/209, 415/206, 415/207, 415/913, 416/180, 416/197 C, 416/223 R, 416/223 B, 416/235, 416/237, 416/238, 416/242
• US Class Current: 415/206
• CPC Class Codes: F04D 17/165 Axial entry and discharge
• CPC Class Codes: F04D 25/0613 the electric motor being of the inside-out type, i.e. the rotor is arranged radially outside a central stator
• CPC Class Codes: F04D 29/281 for fans or blowers
• CPC Class Codes: F04D 29/30 Vanes
• CPC Class Codes: Y10S 415/913 Inlet and outlet with concentric portions

Abstract

A compact centrifugal fan that draws air in past the impeller hub, which encloses a motor and which spins about a central axis, and then urges the air through a bend in the fluid passageway. As the air passes through the annular inlet channel about the impeller hub, it flows in a forward axial direction. The air passes through the bend in the fluid passageway, as the air is being swept around the hub by the blades of the impeller. After the air passes through the bend, it has a reverse axial flow component, in addition to a circumferential flow component. Air having a forward axial flow component passes by the portion of an impeller blade that is closest to the impeller hub, and air having a reverse axial flow component passes the portion of a blade that is furthest from the impeller hub.

Claims

1. An impeller comprising:

a cylindrical hub having a central axis; and

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub and a tip region disposed distally from the hub, each blade having a curved edge extending from the root region to the tip region, the root region having, distal from the curved edge, a generally straight edge that is configured so that the distance from the central axis to the root region'"'"'s straight edge increases approximately linearly in the direction towards the curved edge, and the tip region having, distal from the curved edge, a substantially straight edge that is disposed at an angle with respect to the root region'"'"'s straight edge so that the tip region'"'"'s straight edge is substantially more perpendicular to the central axis than the root region'"'"'straight edge.

2. An impeller according to claim 1, wherein the tip region of each blade is axially displaced, from the root region, in the direction of the curved edge.

3. An impeller according to claim 2, wherein the tip region of each blade extends axially beyond the hub, in the direction of the curved edge.

4. An impeller according to claim 1, wherein the tip region is disposed in approximately the same plane as is the root region.

5. An impeller according to claim 1, wherein each blade is disposed at an angle with respect to a normal to the surface of the hub where the blade is disposed, such that the tip region trails the root region.

6. An impeller for use in a centrifugal fan, the flow through which initially has a forward axial flow component and becomes flow with a reverse axial flow component, comprising:

a cylindrical hub;

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, wherein the surface of the tip region is disposed in approximately the same plane as in the root region, wherein the tip region has leading and trailing faces and the blade is curved in such a way that the leading face is slightly concave.

7. An impeller according to claim 6, wherein the tip region has a section, taken through a plane approximately perpendicular to the faces and parallel to the axis, that smoothly decreases in thickness in the direction of forward axial flow, so that the edge of the blade region where forward axial flow terminates and reverse axial flow begins is relatively slim.

8. An impeller according to claim 6, wherein each blade has a curved edge where the flow having a forward axial flow component terminates and flow having a reverse axial flow component begins, and the tip region, along the edge distal from the curved edge, is substantially a straight line segment transverse to the axis.

9. An impeller for use in a centrifugal fan, the flow through which initially has a forward axial flow component and becomes flow with a reverse axial flow component, comprising:

a cylindrical hub;

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, each blade having a curved edge where forward axial flow terminates and flow having a reverse axial flow component begins, wherein the tip region, along the edge distal from the curved edge, is substantially a straight line segment transverse to the axis.

10. An impeller for use in a centrifugal fan, the flow through which initially has a forward axial flow component and becomes flow with a reverse axial flow component, comprising:

a cylindrical hub;

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, each blade having a curved edge where forward axial flow terminates and flow having a reverse axial flow component begins, wherein the tip region has a section, taken through a plane approximately perpendicular to the blades and parallel to the axis, the smoothly decreases in thickness in the direction of forward axial flow, so that the curved edge of the blade is relatively slim, wherein the tip region, along the edge distal from the curved edge, is substantially a straight line segment transverse to the axis.

11. A centrifugal fan providing a fluid flow path, the fan comprising:

an open annular channel, having a central axis, for axial flow entry of fluid into the fan;

a conduit, disposed concentrically outside of the channel, providing a circumferential flow path, having an inlet coupled to the channel and an a outlet providing exit flow of fluid transverse to the central axis directly from the conduit, and having an axial dimension that increases along the circumferential flow path and an outer radial dimension that is substantially constant along the flow path;

a motor disposed concentrically inside the channel;

a cylindrical hub attached to the motor and rotatable about the central axis, the hub forming a boundary to the annular channel; and

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, such that the root region passes through a portion of the channel, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, such that the tip region passes through a portion of the conduit, the outer edge of the tip region shaped to conform to the outer radial dimension of the conduit.

12. A fan according to claim 11, wherein the tip region of each blade is also axially displaced from the root region, so that the tip region extends axially beyond the hub, in the direction of forward axial flow.

13. A fan according to claim 12, wherein the root region of each blade includes a generally triangular portion configured so that the distance from the central axis to the outer edge of such portion increases approximately linearly in the direction of forward axial flow.

14. A fan according to claim 13, wherein the conduit has an inner surface that, at the extreme limit of forward axial flow, has a curved cross section and wherein the edge of the tip region of the blade proximal thereto is shaped to conform with such surface.

15. A fan according to claim 14, wherein each blade is disposed at an angle with respect to a normal to the surface of the hub where the blade is disposed such that the tip region trials the root region, and wherein the tip region is disposed in approximately the same plane as is the root region.

16. A centrifugal fan providing a fluid flow path, the fan comprising:

an open annular channel, having a central axis, for axial flow entry of fluid into the fan;

a conduit, disposed concentrically outside of the channel, providing a circumferential flow path, having an inlet coupled to the channel and an a outlet providing exit flow of fluid transverse to the axis, and having an axial dimension that increases along the circumferential flow path and an outer radial dimension that is substantially constant along the flow path;

a motor disposed concentrically inside the channel;

a cylindrical impeller hub attached to the motor and rotatable about the central axis, such that the hub forms a boundary to the annular channel; and

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, such that the tip region passes through a portion of the conduit, the outer edge of the tip region shaped to conform to the outer radial dimension of the conduit,

wherein the tip region of each blade is also axially displaced from the root region, so that the tip region extends axially beyond the hub, in the direction of forward axial flow,

wherein the root region of each blade includes a generally triangular portion configured so that the distance from the central axis to the outer edge of such portion increases approximately linearly in the direction of forward axial flow,

wherein the channel has a surface that has a curved cross section where forward axial flow ends and reverse axial flow begins and wherein the edge of the tip region of the blade proximal thereto is shaped to conform with such surface,

wherein the each blade is disposed at an angle with respect to a normal to the surface of the hub where the blade is disposed such that the tip region trails the root region, and wherein the tip region is disposed in approximately the same plane as is the root region, and

wherein the tip region has leading and trailing faces and the blade is curved in such a way that the leading face is slightly concave.

17. A fan according to claim 16, wherein the tip region has a section, taken through a plane approximately perpendicular to the faces and parallel to the axis, that smoothly decreases in thickness in the direction of forward axial flow, so that the edge of the blade region proximal to the curved inner surface of the conduit is relatively slim.

18. A fan comprising:

a housing;

an impeller having a plurality of blades mounted on a hub;

a motor having a stator fixedly mounted to the housing and a rotor fixedly attached inside the hub, such that the motor, when energized, causes the impeller to spin; and

a fluid passageway, defined by the housing and the hub, such that fluid is drawn in a forward axial direction through an annular inlet between the hub and the housing and swept in a circumferential direction by the blades of the impeller,

the fluid passageway having a bend such that the fluid is urged from a forward axial direction to a reverse axial direction, as the fluid is being swept in a circumferential direction by the blades.

19. A fan according to claim 18, wherein the fluid passageway after the bend, where fluid has a reverse axial flow components, is adjacent to and concentrically outside of the annular inlet.

20. A fan according to claim 19, wherein the fluid passageway has an outlet providing fluid exiting the fan to flow in a direction transverse to the central axis.

21. A fan according to claim 19, wherein each blade has a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, the outer edge of the tip region shaped to conform to the outer radial dimension of the passageway.

22. A fan according to claim 21, wherein the root region of each blade includes a generally triangular portion configured so that the distance from the central axis to the outer edge of such portion increases approximately linearly in the direction of forward axial flow.

23. A fan according to claim 22, wherein the passageway has a wall with a curved cross section at the bend, and wherein the edge of the blade proximal thereto is shaped to conform with such curved cross section.

24. A fan according to claim 23, wherein each blade is disposed at an angle with respect to a normal to the surface of the hub where the blade is disposed such that the tip region trails the root region.

25. A fan according to claim 24, wherein the tip region of each blade is also axially displaced from the root region, so that the tip region extends axially beyond the hub, in the direction of forward axial flow.

26. An impeller for use in a centrifugal fan, the flow through which initially has a forward axial flow component and becomes flow with a reverse axial flow component, the impeller comprising:

a cylindrical hub having a central axis; and

a plurality of blades disposed around the hub, each blade having a root region disposed proximally to the hub, where the flow has a forward axial flow component and a circumferential flow component, and a tip region disposed distally from the hub, where the flow has a reverse axial flow component and a circumferential flow component, each blade having a curved edge where flow with a forward axial flow component terminates and flow having a reverse axial flow component begins, and the root region including a generally triangular portion configured so that the distance from the central axis to the outer edge of the triangular portion increases approximately linearly in the direction of forward axial flow.

27. An impeller according to claim 26, wherein the tip region of each blade is axially displaced, from the root region, in the direction of forward axial flow.

28. An impeller according to claim 27, wherein the tip region of each blade extends axially beyond the hub, in the direction of forward axial flow.