Centrifugal fan inlet orifice and impeller assembly

• US 5,478,201 A
• Filed: 06/13/1994
• Issued: 12/26/1995
• Est. Priority Date: 06/13/1994
• Status: Expired due to Term

• Current Assignee: Carrier Corporation (Carrier Global Corporation)
• Original Assignee: Carrier Corporation (Carrier Global Corporation)
• Inventors: Amr, Yehia M.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US08/258,871
• Time in Patent Office: 561 Days
• Field of Search: 415/206, 415/208.1, 415/208.3, 415/208.2, 415/211.1, 415/220, 415/223, 415/119, 416/185, 416/186 R, 416/189, 416/192, 416/193 R, 416/203, 416/223 B
• US Class Current: 415/206
• CPC Class Codes: F04D 17/16 for displacing without appreciable compression
• CPC Class Codes: F04D 29/282 the leading edge of each vane being substantially parallel to the rotation axis
• CPC Class Codes: F04D 29/4213 suction ports
• CPC Class Codes: F04D 29/666 by means of rotor construction or layout, e.g. unequal distribution of blades or vanes

Abstract

An inlet orifice structure and impeller assembly for a centrifugal flow fan. The inlet orifice has an elliptical cross section in a plane passing through the axis of rotation of the fan. The impeller is shrouded and also has a similarly elliptical cross section. The impeller is sized so that, when assembled together, the shroud overlaps and rotates around the stationary inlet orifice. In a preferred embodiment, there are 13 impeller blades nonuniformly spaced around a hub plate. A particular blade spacing is disclosed and claimed. The inner surface of the hub plate is arcuately curved to guide the air flow through the fan from its entering axial direction to its radial exiting direction. The contour of the hub plate allows for the fan drive motor to be partially recessed into the plate.

Claims

1. An apparatus for moving air comprising:

an inlet orifice structure (10) comprising a surface having an axisymmetric orifice leading edge (101),

an axisymmetric throat (102) in downstream air flow relationship with said orifice leading edge and extending from said leading edge to an orifice trailing edge (103),

said throat being in form like a surface produced by rotating a first planar line (L₁) about a coplanar axis of generation (A_G),

said first planar line being a generally quarter segment of a first ellipse having a major axis (A_SMO) that is substantially parallel to said axis of generation and a semiminor axis (A_SmO); and

a fan impeller (20) of the centrifugal flow type having

an axis of rotation (A_G) that is, when assembled for operation with said inlet orifice structure, coincident with said axis of generation of said orifice structure,

an impeller hub plate (202) having an inner face (2021) and centered on said axis of rotation;

thirteen blades (203),

each having a root (2031) and a tip (2032), and affixed at said root to and extending generally outward from said inner face,

arranged with an angular spacing between similar points on adjacent blades of 31.85°

, 24°

, 30.25°

, 31°

, 24.9°

, 22.75°

, 28.25°

, 32.15°

, 27.25°

, 29.5°

, 26.6°

23.25° and

28.25°

,

backwardly swept with respect to a preferred direction of rotation of said impeller;

an axisymmetric orificed shroud (201) affixed to said blade tips and having

a shroud leading edge (2011) and a shroud trailing edge (2012), with respect to air flow through said shroud orifice,

a diffuser (2013) extending from said shroud leading edge to said shroud trailing edge,

said diffuser being in form like a surface produced by rotating a second planar line (L₂) about a coplanar axis of generation that is coincident with said axis of rotation,

said second planar line being a generally quarter segment of a second ellipse having a semimajor axis (A_SMS) substantially parallel to said axis of generation and a semiminor axis (A_SmS) and

a portion of said diffuser adjacent said leading edge having an inner radius (R_IS) sufficient to allow, when said fan impeller and said inlet orifice structure are assembled for operation, said diffuser portion to overlap and freely rotate about said throat portion of said orifice structure.

2. The apparatus of claim 1 in which said semimajor axis of said first ellipse is at least 1.2 times said semiminor axis of said first ellipse.

3. The apparatus of claim 2 in which said semimajor axis of said first ellipse is 1.4 times said semiminor axis of said first ellipse.

4. The apparatus of claim 1 in which said impeller has a maximum swept radius (R_MAX) and said semiminor axis of said first ellipse is at least 0.14 times said maximum swept radius.

5. The apparatus of claim 4 in which said semiminor axis of said first ellipse is 0.20 times said maximum swept radius.

6. The apparatus of claim 1 in which said semimajor axis of said second ellipse is at least 1.2 times the semiminor axis of said second ellipse.

7. The apparatus of claim 6 in which said semimajor axis of said second ellipse is 1.64 times the semiminor axis of said second ellipse.

8. The apparatus of claim 1 in which said impeller has a maximum swept radius and said maximum swept radius is at least 0.25 times the semiminor axis of said second ellipse.

9. The apparatus of claim 8 in which the semiminor axis of said second ellipse is 0.30 times said maximum swept radius.

10. The apparatus of claim 1 in which said hub plate contains a motor enclosure.

11. The apparatus of claim 1 in which said inner faces of said hub plate has a contoured portion (2021) that in form like a surface produced by rotating a third planar line (L₃) about a coplanar axis of rotation that is coincident with said axis of rotation, said third planar line being an arc of a circle.

12. The apparatus of claim 1 in which said arc extends for 45 to 75 degrees of the circumference of said circle.

13. The apparatus of claim 1 in which said blades have a curved chord.