Inlet for axial fan

Information

  • Patent Grant
  • 11226114
  • Patent Number
    11,226,114
  • Date Filed
    Wednesday, May 3, 2017
    7 years ago
  • Date Issued
    Tuesday, January 18, 2022
    3 years ago
Abstract
A fan assembly (10) includes a shrouded fan rotor (18) having a plurality of fan blades (22) extending from a rotor hub (24) and rotatable about a central axis (20) of the fan assembly, and a fan shroud (26) extending circumferentially around the fan rotor (18) and secured to an outer tip diameter of the plurality of fan blades (22). A fan casing (16) encloses the shrouded fan rotor (18). The fan casing (16) defines a fan inlet (30) of the fan assembly and includes an inlet extension (54) at an outer diameter of the fan casing, extending axially upstream of a conventional bell mouth inlet (58), relative to a direction of airflow through the shrouded fan rotor (18).
Description
BACKGROUND

The subject matter disclosed herein relates to vane axial flow fans. More specifically, the subject matter disclosed herein relates to structures to improve fan stall performance and/or improve stall recovery hysteresis performance of vane axial flow fans.


Axial flow fans are widely used in many industries ranging from automotive to aerospace to HVAC but are typically limited in their application by operating range restrictions and noise considerations. While vane-axial fans can achieve high static efficiencies, their limited operating range due to blade stall typically makes the vane-axial fan impractical for use in many systems that have extended operating range requirements. Furthermore, the stall and stall recovery performance of an axial fan can be degraded due to sensitivity to non-optimal or off-design inflow conditions. For example, when an axial fan is subjected to inflow that is substantially at a right angle to the axis of rotation of the fan, the fan may experience reduced stall performance and/or increased stall recovery hysteresis. In certain HVAC applications, such as an indoor fan system for a residential or commercial packaged product or split system, the reduction in operating range driven by this deficient stall/recovery hysteresis performance can hinder the application of vane-axial fan technology.


SUMMARY

In one embodiment, a fan assembly includes a shrouded fan rotor having a plurality of fan blades extending from a rotor hub and rotatable about a central axis of the fan assembly, and a fan shroud extending circumferentially around the fan rotor and secured to an outer tip diameter of the plurality of fan blades. A fan casing encloses the shrouded fan rotor. The fan casing defines a fan inlet of the fan assembly and includes an inlet extension at an outer diameter of the fan casing, extending axially upstream of a conventional bell mouth inlet, relative to a direction of airflow through the shrouded fan rotor.


Additionally or alternatively, in this or other embodiments the inlet extension extends between 5% and 20% of the fan rotor tip diameter axially upstream of the conventional bell mouth inlet.


Additionally or alternatively, in this or other embodiments the conventional bell mouth inlet transitions to the inlet extension, the inlet extension including a convex portion and a concave portion.


Additionally or alternatively, in this or other embodiments the concave portion extends from an inlet extension leading edge axially to a transition point and the convex portion extends from the transition point to a rotor leading edge.


Additionally or alternatively, in this or other embodiments the convex portion axially overlaps the fan shroud.


Additionally or alternatively, in this or other embodiments the inlet extension tapers radially from the conventional bell mouth inlet to an inlet extension leading edge at a taper angle.


Additionally or alternatively, in this or other embodiments the taper angle is between 0.5 degrees and 45 degrees.


Additionally or alternatively, in this or other embodiments a primary direction of airflow approaching the fan inlet is transverse relative to the central axis.


In another embodiment, a casing assembly for an axial fan includes a fan casing extending circumferentially about a central axis, the fan casing defining a fan inlet of the axial fan, and an inlet extension at an outer diameter of the casing, extending axially upstream of a conventional bell mouth inlet, relative to a direction of airflow through the shrouded fan rotor.


Additionally or alternatively, in this or other embodiments the inlet extension includes a concave surface extending from an inlet extension leading edge axially to a transition point and a convex portion extending axially rearwardly from the transition point.


Additionally or alternatively, in this or other embodiments the inlet extension is configured to extend axially upstream of a conventional bell mouth inlet, relative to a direction of airflow through the fan assembly.


Additionally or alternatively, in this or other embodiments the inlet extension is configured to extend between 5% and 20% of the fan rotor tip diameter axially upstream of the conventional bell mouth inlet.


Additionally or alternatively, in this or other embodiments the inlet extension tapers radially from the conventional bell mouth inlet to an inlet extension leading edge at a taper angle.


Additionally or alternatively, in this or other embodiments the taper angle is between 0.5 degrees and 45 degrees.


Additionally or alternatively, in this or other embodiments the inlet extension is configured to axially overlap a fan shroud of the fan assembly.


Additionally or alternatively, in this or other embodiments a primary direction of airflow approaching the fan inlet is transverse relative to the central axis.





BRIEF DESCRIPTION OF THE DRAWINGS

The subject matter is particularly pointed out and distinctly claimed at the conclusion of the specification. The foregoing and other features, and advantages of the present disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:



FIG. 1 is a perspective view of an embodiment of a fan assembly;



FIG. 2 is another cross-sectional view of an embodiment of a fan assembly; and



FIG. 3 is another partial cross-sectional view of an embodiment of a fan assembly.





The detailed description explains embodiments of the invention, together with advantages and features, by way of example with reference to the drawing.


DETAILED DESCRIPTION

Shown in FIG. 1 is a partially exploded perspective view of an embodiment of an axial-flow fan 10 utilized, for example in a heating, ventilation and air conditioning (HVAC) system as an air handling fan. The fan 10 may be driven by an electric motor 12 connected to the fan 10 by a shaft (not shown), or alternatively a belt or other arrangement. In operation, the motor 12 drives rotation of the fan 10 to urge airflow 14 across the fan 10 and along a flowpath, for example, to or from a heat exchanger (not shown). The fan 10 includes a casing 16 with a fan rotor 18, or impeller rotably located in the casing 16. Operation of the motor 12 drives rotation of the fan rotor 18 about a fan axis 20. The fan rotor 18 includes a plurality of fan blades 22 extending from a hub 24 and terminating at a fan shroud 26. The fan shroud 26 is connected to one or more fan blades 22 of the plurality of fan blades 22 and rotates about the fan axis 20 therewith. The fan 10 further includes a stator assembly 28 including a plurality of stator vanes 30, located downstream of the fan rotor 18. The plurality of stator vanes 30 extend substantially radially from a stator hub 32 to a stator shroud 34.


Referring now to FIG. 2, in some applications, such as a rooftop or other packaged product heating, ventilation, air conditioning and refrigeration (HVAC&R) system, the fan 10 is oriented such that the airflow 14 directed at a fan inlet 50 of the fan 10 is from a direction predominantly perpendicular to the fan axis 20. Thus, to flow along the fan axis 20, the airflow 14 must be turned 90 degrees before flowing through the fan 10 and, for example, across a downstream heat exchange surface 52 of the HVAC&R system. This side-flow condition at the fan inlet 50 can result in poor stall and stall recovery hysteresis performance of the fan 10, and may limit an operating range of the fan 10, and thus its use in such applications.


Referring now to FIG. 3, the fan inlet 50 includes a casing extension 54 extending axially forward of a conventional bell mouth inlet 58, in some embodiments the casing extension 54 extends in the range of about 5% to about 20% of the fan rotor tip diameter axially forward of a conventional bell mouth inlet 58. The casing extension 54 provides axial distance for turning of the airflow 14 toward the axial direction along the fan axis 20 prior to entering the fan rotor 18. With a casing extension 54 length of about one inch, a reduction in stall recovery hysteresis of about 70% has been achieved, when compared with a comparable fan without the casing extension 54 that is applied in an installation with predominantly perpendicular inflow as shown in FIG. 2.


The casing extension 54 extends axially upstream of a conventional bell mouth inlet 58 to condition the airflow 14 prior to the airflow entering the fan rotor 18. A casing extension leading edge 60 defines an axially forward-most portion of the casing extension 54. In some embodiments, the casing extension 54 is formed integral with the conventional bell mouth inlet 58, while in other embodiments the casing extension 54 is a separate component from and discontinuous with the conventional bell mouth inlet 58.


In some embodiments, the casing extension 54 is an axial ring extending upstream of the conventional bell mouth inlet 58. In other embodiments, the casing extension 58 transitions from the conventional bell mouth inlet 58 at an inlet angle 80 (shown in FIG. 2). In some embodiments, the inlet angle 80 is in the range of 0.5 degrees to 45 degrees, with in other embodiments, the inlet angle 80 is between 10 and 40 degrees, while in still other embodiments the inlet angle 80 is between 15 and 30 degrees.


In some embodiments, as shown in FIG. 3, the casing extension leading edge 60 transitions to the conventional bell mouth inlet 58 via a concave portion 62 extending from the casing extension leading edge 60 axially to a transition point 64, and a convex portion 66 extending from the transition point 64 to a rotor leading edge 68. In some embodiments, the convex portion 68 axially overlaps the fan shroud 26.


While ideally an axially longer casing extension 54 improves the condition of airflow 14 entering the fan rotor 18, the performance improvement of the fan 10 must be balanced with packaging constraints on the fan 10.


The utilization of casing extension 54 in the fan 10 improves stall performance of the fan 10 and further reduces stall recovery hysteresis in comparison to prior fans. These improvements allow for expansion of the operating envelope of shrouded axial fans, thus increasing their applicability to a wide range of conditions, such as rooftop HVAC&R systems, allowing such systems to take advantage of the performance advantages of shrouded axial fans.


While the present disclosure has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the present disclosure is not limited to such disclosed embodiments. Rather, the present disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate in spirit and/or scope. Additionally, while various embodiments have been described, it is to be understood that aspects of the present disclosure may include only some of the described embodiments. Accordingly, the present disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.

Claims
  • 1. A fan assembly, comprising a shrouded fan rotor:a plurality of fan blades extending from a rotor hub and rotatable about a central axis of the fan assembly; anda fan shroud extending circumferentially around the shrouded fan rotor and secured to an outer tip diameter of the plurality of fan blades; anda fan casing enclosing the shrouded fan rotor, the fan casing defining a fan inlet of the fan assembly and including an inlet extension at an outer diameter of the fan casing, extending axially upstream of a bell mouth inlet, relative to a direction of airflow through the shrouded fan rotor;wherein the inlet extension axially overlaps the fan shroud radially inboard of the fan shroud;wherein the bell mouth inlet transitions to the inlet extension, the inlet extension including a convex portion and a concave portion; andwherein the concave portion extends from an inlet extension leading edge axially to a transition point and the convex portion extends from the transition point to a rotor leading edge.
  • 2. The fan assembly of claim 1, wherein the convex portion axially overlaps the fan shroud.
  • 3. The fan assembly of claim 1, wherein the inlet extension tapers radially from the bell mouth inlet to an inlet extension leading edge at a taper angle.
  • 4. The fan assembly of claim 3, wherein the taper angle is between 0.5 degrees and 45 degrees.
  • 5. The fan assembly of claim 1, wherein a primary direction of airflow upstream of the inlet extension leading edge is transverse relative to the central axis.
  • 6. A casing assembly for an axial fan, comprising a fan casing extending circumferentially about a central axis, the fan casing defining a fan inlet of the axial fan; andan inlet extension at an outer diameter of the fan casing, extending axially upstream of a bell mouth inlet, relative to a direction of airflow through a shrouded fan rotor disposed in the casing assembly;wherein the inlet extension axially overlaps a fan shroud of the shrouded fan rotor radially inboard of the fan shroud;wherein the bell mouth inlet transitions to the inlet extension, the inlet extension including a convex portion and a concave portion; andwherein the concave portion extends from an inlet extension leading edge axially to a transition point and the convex portion extends from the transition point to a rotor leading edge of the shrouded fan rotor.
  • 7. The casing assembly of claim 6, wherein the inlet extension tapers radially from the bell mouth inlet to the inlet extension leading edge at a taper angle.
  • 8. The casing assembly of claim 7, wherein the taper angle is between 0.5 degrees and 45 degrees.
  • 9. The casing assembly of claim 6, wherein a primary direction of airflow upstream of the inlet extension leading edge is transverse relative to the central axis.
CROSS REFERENCE TO RELATED APPLICATIONS

This application is a National Stage application of PCT/US2017/030728, filed May 3, 2017, which claims the benefit of U.S. Provisional Application No. 62/330,975, filed May 3, 2016, U.S. Provisional Application No. 62/330,963, filed May 3, 2016, and U.S. Provisional Application No. 62/369,349, filed Aug. 1, 2016, all of which are incorporated by reference in their entirety herein.

PCT Information
Filing Document Filing Date Country Kind
PCT/US2017/030728 5/3/2017 WO 00
Publishing Document Publishing Date Country Kind
WO2017/192647 11/9/2017 WO A
US Referenced Citations (85)
Number Name Date Kind
2189767 Vose Feb 1940 A
2287822 Odor et al. Jun 1942 A
2293718 Eberhart Aug 1942 A
3229896 Levy Jan 1966 A
3415074 Metcalfe Dec 1968 A
3702220 Medawar et al. Nov 1972 A
3846039 Stalker Nov 1974 A
3883264 Rao May 1975 A
3995970 Nobuyuki Dec 1976 A
4018266 Kay Apr 1977 A
4182596 Wellman Jan 1980 A
4566852 Hauser Jan 1986 A
4971603 Prinsloo et al. Nov 1990 A
5489186 Yapp Feb 1996 A
5525036 Park Jun 1996 A
5551838 Hugbart Sep 1996 A
5884589 Sakamoto Mar 1999 A
5938527 Oshima et al. Aug 1999 A
6017191 Harmsen Jan 2000 A
6038879 Turcotte et al. Mar 2000 A
6101829 Robinson Aug 2000 A
6139265 Alizadeh Oct 2000 A
6195983 Wadia et al. Mar 2001 B1
6398492 Cho et al. Jun 2002 B1
6540479 Liao et al. Apr 2003 B2
6663342 Huang et al. Dec 2003 B2
6910862 Horng et al. Jun 2005 B2
6997678 Sun Feb 2006 B2
7220102 Cho et al. May 2007 B2
7334988 Horng et al. Feb 2008 B2
7377751 Foster, Sr. et al. May 2008 B2
7416386 Ho et al. Aug 2008 B2
7481615 Park Jan 2009 B2
7618233 Parker et al. Nov 2009 B2
7789622 Acre Sep 2010 B2
7824154 Yabuuchi Nov 2010 B2
7942627 Jin May 2011 B2
8056352 Kang et al. Nov 2011 B2
8087878 Chen Jan 2012 B2
8157513 Takeshita et al. Apr 2012 B2
8197198 Miyabara et al. Jun 2012 B2
8333559 Bushnell Dec 2012 B2
8393158 Conners Mar 2013 B2
8491270 Eguchi et al. Jul 2013 B2
8573343 Komatsu et al. Nov 2013 B2
8622695 Decker et al. Jan 2014 B2
8696305 Farlow et al. Apr 2014 B2
8740562 Takemoto et al. Jun 2014 B2
8821123 Camci et al. Sep 2014 B2
8887486 Rosen et al. Nov 2014 B2
9033656 Mizumi et al. May 2015 B2
9334877 Nicholls May 2016 B2
9850914 Dreesen Dec 2017 B2
9945391 Hausmann Apr 2018 B2
10094394 Heli Oct 2018 B2
10190601 Dygert et al. Jan 2019 B2
10227988 Gao et al. Mar 2019 B2
10428829 Gebert et al. Oct 2019 B2
20020159883 Simon et al. Oct 2002 A1
20050042089 Horng et al. Feb 2005 A1
20050186070 Zeng et al. Aug 2005 A1
20050191955 Horng et al. Sep 2005 A1
20060067816 Chang et al. Mar 2006 A1
20060147304 Cho et al. Jul 2006 A1
20060216147 Park Sep 2006 A1
20070031248 Hsu et al. Feb 2007 A1
20070154308 Yang Jul 2007 A1
20110064571 Lind et al. Mar 2011 A1
20130017081 Andrews Jan 2013 A1
20130051997 Uchiyama et al. Feb 2013 A1
20130315737 Dygert et al. Nov 2013 A1
20140019970 Okamoto Jan 2014 A1
20150030445 Gonidec et al. Jan 2015 A1
20150065029 Leckelt et al. Mar 2015 A1
20150098817 Innocenti Apr 2015 A1
20150104303 Velthuis Apr 2015 A1
20150275918 Hausmann Oct 2015 A1
20150330411 Heli Nov 2015 A1
20150354598 Dygert et al. Dec 2015 A1
20150354841 Amr et al. Dec 2015 A1
20170260985 Gao et al. Sep 2017 A1
20180087513 Hoffman Mar 2018 A1
20180106267 Gebert et al. Apr 2018 A1
20190211843 Dygert Jul 2019 A1
20190226688 Dygert et al. Jul 2019 A1
Foreign Referenced Citations (12)
Number Date Country
202004005026 Sep 2004 DE
1895166 Mar 2008 EP
2565467 Jun 2013 EP
2904277 Aug 2015 EP
2433772 Apr 2007 GB
2001182692 Jul 2001 JP
2011185166 Sep 2011 JP
2014020235 Feb 2014 JP
2014056657 Apr 2014 WO
2014109850 Jul 2014 WO
2017192644 Nov 2017 WO
2017192651 Nov 2017 WO
Non-Patent Literature Citations (8)
Entry
ArchiExpo; CFM; “The Online Architecture and Design Exhibition”, BIU Continental Fan Manufacturing Inc., 2019 VirtualExpo; Accessed Online: Dec. 7, 2018; 5 Pages. URL: www.archiexpo.com/prod/continental-fan-manufacturing-inc/product-10072-492474.html.
Ohanian, O., “Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control”, Virginia Tech Electronic Theses and Dissertations, May 4, 2011, 203 Pages, Virginia Tech. URI: http://hdl.handle.net/10919/27687.
International Search Report for International Application No. PCT/US2017/030722; International Filing Date May 3, 2017; dated Jul. 14, 2017; 5 Pages.
International Search Report for International Application No. PCT/US2017/030728; International Filing Date May 3, 2017; dated Sep. 14, 2017; 7 Pages.
International Search Report for International Application No. PCT/US2017/030732; International Filing Date May 3, 2017; dated Sep. 14, 2017; 7 Pages.
Written Opinion for International Application No. PCT/US2017/030722; International Filing Date May 3, 2017; dated Jul. 14, 2017; 6 Pages.
Written Opinion for International Application No. PCT/US2017/030728; International Filing Date May 3, 2017; dated Sep. 14, 2017; 7 Pages.
Written Opinion for International Application No. PCT/US2017/030732; International Filing Date May 3, 2017; dated Sep. 14, 2017; 9 Pages.
Related Publications (1)
Number Date Country
20190178252 A1 Jun 2019 US
Provisional Applications (3)
Number Date Country
62330975 May 2016 US
62330963 May 2016 US
62369349 Aug 2016 US