EP2242932B1 - A meridional fan - Google Patents

A meridional fan Download PDF

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Publication number
EP2242932B1
EP2242932B1 EP09701751.1A EP09701751A EP2242932B1 EP 2242932 B1 EP2242932 B1 EP 2242932B1 EP 09701751 A EP09701751 A EP 09701751A EP 2242932 B1 EP2242932 B1 EP 2242932B1
Authority
EP
European Patent Office
Prior art keywords
fan
tip
blade
fan according
flange
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP09701751.1A
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German (de)
French (fr)
Other versions
EP2242932A1 (en
Inventor
Anthony Geoffrey Sheard
Allessandro Corsini
Franco Rispoli
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Howden Axial Fans AB
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Howden Axial Fans AB
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Publication date
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Publication of EP2242932A1 publication Critical patent/EP2242932A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps

Definitions

  • the present invention relates to meridional fans, particularly but not exclusively, to axial flow fans for large scale air ventilation and/or heating purposes in industrial buildings, industrial air conditioning units, underground railway systems and similar large infrastructures.
  • Such fans are typically located in a duct system and it is desirable for efficiency purposes for the area swept by the fan blades to be located in a cylindrical ring part of the duct system with a minimal clearance between the tips of the fan blades and the surface of the cylindrical ring.
  • the outer surface of the tips of the fan blades have a contour in the form of an arc corresponding to the circle swept by the fan blades.
  • the fan aerodynamic work input establishes a higher pressure downstream of the fan than upstream.
  • the pressure rise is obtained by means of aerodynamic forces at play when the air flows about the rotor blades.
  • Owing to the design of the blade a pressure difference is established between the blade pressure surface or side and its suction surface or side. The result of this pressure difference means that air tends to spill back over the tip of the fan from the high pressure to the low-pressure side. This air movement reduces the efficiency of the fan and also increases the noise generated by the fan.
  • a known method for reducing the amount of flow back air is to keep the gap between the fan tips and the cylindrical ring to a minimum and also to extend the length of the gap by incorporating on the tip of each blade an extending flange which increases the length of the gap in the direction of the leakage flow and thereby increases the resistance to flow back through the gap.
  • the present invention seeks to provide an improved form of a fan blade tip which increases the efficiency of the fan and at the same time reduces the noise generated by the fan.
  • the fan tips have, in the past, been made as a uniform as possible, but it has now, surprisingly, been discovered that a non uniform profile for certain sections of the blade tip can be advantageous in increasing the efficiency of the fan, reducing the power required to drive the fan at a given speed and pressure, and at the same time reducing the noise generated by the fan.
  • the uniform profile of the known conventional blade tips lead to the generation of tight vortices at the blade tip and it is believed that these vortices, when they reach a critical state suddenly expand very rapidly, to the extent of provoking vortex bursting or collapse, which generates a great deal of turbulence. This adverse effect is amplified if the vortices impinge on an adjacent fan blade at which point they burst on impact.
  • GB 2050530 (Papst) (D3) discloses an axial fan for impelling air through a duct and has a plurality of fan blades with peripheral blade tips having a leading edge, a trailing edge and a tip outer surface defining a leakage path between the tip and the duct ring.
  • the tip has a flange extending in the axial direction, but the whole tenor of the specification is that this is on the upstream side and it is entirely fortuitous that, for manufacturing reasons, certain embodiments have the tip extending onto the downstream high-pressure side as well. However there is no disclosure or teaching in the specification that it is important that the tip flange and hence the leakage path should extend into the high-pressure side.
  • FR 2753495 (Valeo) (D2) discloses a fan rotatable in a duct and in the leakage path between the outer tips of the fan blades and the duct provides means in the form of protuberances to minimise the width of the leakage path. There is no teaching of the desirability of having the leakage path on the high-pressure side nor the advantages of having a non-uniform leading edge.
  • a meridional fan adapted to be rotatably mounted in a duct ring of circular cross section for impelling air through the duct, and having a plurality of fan blades with peripheral blade tips having a width defining an arc with a circumferential extent describing, in operation, a circular path adjacent the duct ring, the blade tips each having a leading edge, a trailing edge and a tip outer surface, a leakage path being formed between the tip outer surface and the duct ring, at least one of the edges and/or the outer surface having a non-uniform profile for influencing the flow of air through the flow leakage path, characterised in that the or each tip has a flange extending in the axial direction on the downstream, high pressure side of the fan, which increases the length of the leakage flow path and wherein the leading edge of the flange has a non-uniform profile so that the circumferential axial extent of the leading edge of the flange varies along the width of the blade
  • the leading edge of the flange has an undulating profile.
  • the trailing edge of the blade tip includes a stepped shoulder extending at least partially across the width of the blade tip.
  • the stepped shoulder consists of a plurality of stepped recesses spaced across the width of the blade tip. These stepped recesses preferably are regularly spaced, but may be irregularly spaced.
  • Figure 3 illustrates a schematic cross-section through the axis of the fan and cylindrical ring 3 illustrating the peripheral flange 5 with its non-uniform leading edge 6.
  • the flange extends axially downstream on the high pressure side of the fan blade.
  • the effect of the high pressure on the blade pressure side means that air tends to spill backwards at the periphery of the fan tips through the gap between the fan tip 4 and the cylindrical ring 3 as illustrated by the arrow 7.
  • the gap thus forms a leakage flow path for air to flow from the high pressure, downstream side of the blade back to the upstream low pressure side and it is desirable to reduce this flow to a minimum.
  • the maximum pressure on the downside of the fan occurs in the boundary layer adjacent the fan face.
  • Figure 4 illustrates a scrap view of a fan blade 2 and its tip 4 in the direction of the arrow B in which the outer surface 8 of the tip has a non uniform profile in the circumferential direction formed by undulations. These undulations may be regular or irregular in size.
  • Figure 6 illustrates an alternative embodiment of a rear view of the blade tip in which a continuous stepped shoulder 9 is provided across the full width of the fan blade.
  • the peripherally extending flange 5 has a non-uniform dimension in the circumferential direction formed by a gradual curving of the leading edge 6.
  • the variation in the circumferential extent of the flange may be formed in a stepped manner with regular or irregularly spaced steps.

Description

  • The present invention relates to meridional fans, particularly but not exclusively, to axial flow fans for large scale air ventilation and/or heating purposes in industrial buildings, industrial air conditioning units, underground railway systems and similar large infrastructures.
  • Such fans are typically located in a duct system and it is desirable for efficiency purposes for the area swept by the fan blades to be located in a cylindrical ring part of the duct system with a minimal clearance between the tips of the fan blades and the surface of the cylindrical ring. To achieve this, the outer surface of the tips of the fan blades have a contour in the form of an arc corresponding to the circle swept by the fan blades.
  • In operation, the fan aerodynamic work input establishes a higher pressure downstream of the fan than upstream. The pressure rise is obtained by means of aerodynamic forces at play when the air flows about the rotor blades. Owing to the design of the blade a pressure difference is established between the blade pressure surface or side and its suction surface or side. The result of this pressure difference means that air tends to spill back over the tip of the fan from the high pressure to the low-pressure side. This air movement reduces the efficiency of the fan and also increases the noise generated by the fan. A known method for reducing the amount of flow back air is to keep the gap between the fan tips and the cylindrical ring to a minimum and also to extend the length of the gap by incorporating on the tip of each blade an extending flange which increases the length of the gap in the direction of the leakage flow and thereby increases the resistance to flow back through the gap.
  • The present invention seeks to provide an improved form of a fan blade tip which increases the efficiency of the fan and at the same time reduces the noise generated by the fan.
  • Intuitively, the fan tips have, in the past, been made as a uniform as possible, but it has now, surprisingly, been discovered that a non uniform profile for certain sections of the blade tip can be advantageous in increasing the efficiency of the fan, reducing the power required to drive the fan at a given speed and pressure, and at the same time reducing the noise generated by the fan. The uniform profile of the known conventional blade tips lead to the generation of tight vortices at the blade tip and it is believed that these vortices, when they reach a critical state suddenly expand very rapidly, to the extent of provoking vortex bursting or collapse, which generates a great deal of turbulence. This adverse effect is amplified if the vortices impinge on an adjacent fan blade at which point they burst on impact.
  • GB 2050530 (Papst) (D3) discloses an axial fan for impelling air through a duct and has a plurality of fan blades with peripheral blade tips having a leading edge, a trailing edge and a tip outer surface defining a leakage path between the tip and the duct ring. The tip has a flange extending in the axial direction, but the whole tenor of the specification is that this is on the upstream side and it is entirely fortuitous that, for manufacturing reasons, certain embodiments have the tip extending onto the downstream high-pressure side as well. However there is no disclosure or teaching in the specification that it is important that the tip flange and hence the leakage path should extend into the high-pressure side.
  • FR 2753495 (Valeo) (D2) discloses a fan rotatable in a duct and in the leakage path between the outer tips of the fan blades and the duct provides means in the form of protuberances to minimise the width of the leakage path. There is no teaching of the desirability of having the leakage path on the high-pressure side nor the advantages of having a non-uniform leading edge.
  • DE 3234011 (D4) and US 4089618 (D5) disclose fans in which trailing radial edges of the fan blades have a non-uniform profile to generate turbulence to reduce noise. However both patents are silent on the feature of leakage paths between the tips of the fan blades and the casing.. US 2003/095864 (D6) discloses a fan in which the outer tips of the fan blades have an end piece which extends axially in both directions of the fan blade to break up blade end vortex. There is no discussion or teaching of the leakage path or the problems associated with such an arrangement. There is also no discussion of the advantages of using non-uniform profiles for the edges of the end faces.
  • According to the present invention there is provided a meridional fan adapted to be rotatably mounted in a duct ring of circular cross section for impelling air through the duct, and having a plurality of fan blades with peripheral blade tips having a width defining an arc with a circumferential extent describing, in operation, a circular path adjacent the duct ring, the blade tips each having a leading edge, a trailing edge and a tip outer surface, a leakage path being formed between the tip outer surface and the duct ring, at least one of the edges and/or the outer surface having a non-uniform profile for influencing the flow of air through the flow leakage path, characterised in that the or each tip has a flange extending in the axial direction on the downstream, high pressure side of the fan, which increases the length of the leakage flow path and wherein the leading edge of the flange has a non-uniform profile so that the circumferential axial extent of the leading edge of the flange varies along the width of the blade tip..
  • Preferably, the leading edge of the flange has an undulating profile. In a further embodiment, the trailing edge of the blade tip includes a stepped shoulder extending at least partially across the width of the blade tip. In one form, the stepped shoulder consists of a plurality of stepped recesses spaced across the width of the blade tip. These stepped recesses preferably are regularly spaced, but may be irregularly spaced.
  • In a preferred embodiment, the outer tip surface has a non-uniform profile in the circumferential direction. Preferably the non-uniform profile may be formed by undulations or by grooves or a mixture thereof in the outer surface. The undulations and grooves may extend partially or completely along the axial extent of the outer surface. In a further embodiment (not shown) the fan tip includes a plurality of holes or perforations.
  • Preferred embodiments of the present invention will now be described by way of example, with reference to the accompanying drawings in which:-
    • Figure 1 shows an axial view of an axial fan having four blades located in a cylindrical casing,
    • Figure 2 shows a radially inward view of a fan blade,
    • Figure 3 shows an axial section of a fan blade and the cylindrical casing,
    • Figure 4 shows a scrap of view of a fan blade in the direction of the Arrow B shown in Figure 3,
    • Figure 5 shows a scrap view of the trailing edge of a fan blade,
    • Figure 6 shows a corresponding view of the trailing edge of a further embodiment, and
    • Figure 7 shows a scrap view of the outer surface of a further embodiment of blade tip.
  • Referring now to Figure 1, there is shown an axial view of an axial flow fan having four fan blades 2 mounted for rotation about an axis 1 of a cylindrical ring part 3 of a duct system of an air ventilation system. The area swept by the fan is such that the blade tips 4 are very close to the cylindrical ring 3 with only a minimal gap there between. To minimise this gap, the outer surfaces of the blade tips 4 have an arcuate contour defined by the circle swept by the blades 2.
  • Referring now to Figure 2 also, it can be seen that the fan blade has on its tip a flange 5 serving to increase the circumferential extent of the gap between the outer surface of the tip and the cylindrical ring 3 to increase the resistance of airflow through the gap. In this embodiment it can be seen that the edge 6 of the flange 5 has a undulating, non-uniform profile in the circumferential direction and at one end of the tip the outer surface is cut away to provide a non-uniform outer surface for the tip.
  • Figure 3 illustrates a schematic cross-section through the axis of the fan and cylindrical ring 3 illustrating the peripheral flange 5 with its non-uniform leading edge 6. The flange extends axially downstream on the high pressure side of the fan blade. The effect of the high pressure on the blade pressure side means that air tends to spill backwards at the periphery of the fan tips through the gap between the fan tip 4 and the cylindrical ring 3 as illustrated by the arrow 7. The gap thus forms a leakage flow path for air to flow from the high pressure, downstream side of the blade back to the upstream low pressure side and it is desirable to reduce this flow to a minimum. The maximum pressure on the downside of the fan occurs in the boundary layer adjacent the fan face. Centrifugal force tends to drive the boundary layer up towards the fan tip and it has been found is that with the flange the boundary layer is deflected and dissipated with the effect that the pressure at the entrance to the leakage path is lower than it otherwise would be.
  • Figure 4 illustrates a scrap view of a fan blade 2 and its tip 4 in the direction of the arrow B in which the outer surface 8 of the tip has a non uniform profile in the circumferential direction formed by undulations. These undulations may be regular or irregular in size.
  • Figure 5 illustrates a schematic view of the fan blade tip 4 having on the low-pressure side a series of cutaway stepped shoulders 9 or recesses which serve to decelerate abruptly the airflow as it exits the gap between the blade tip 4 and the cylindrical ring 3. These recesses may be regularly spaced, of a regular size or may be irregularly spaced and irregularly sized.
  • Figure 6 illustrates an alternative embodiment of a rear view of the blade tip in which a continuous stepped shoulder 9 is provided across the full width of the fan blade. In this embodiment, the peripherally extending flange 5 has a non-uniform dimension in the circumferential direction formed by a gradual curving of the leading edge 6. In another embodiment, not shown, the variation in the circumferential extent of the flange may be formed in a stepped manner with regular or irregularly spaced steps.
  • Figure 7 shows a further embodiment in which the outer surface of the forwardly extending flange has a plurality of spaced recesses or grooves which may or may not extend through to the leading edge or trailing edge of the outer surface.
  • It will be appreciated that the different methods of providing a non-uniform profile for the outer surface, leading and trailing edges of the blade tip may be used individually or in any combination depending upon the particular size, design speed, number of blades etc of a particular fan. In this connection, although the specific embodiment shows a fan with four blades, it will be understood that the number of blades may vary depending upon the design parameters of the particular installation. Other forms of non-uniformity, such as a circumferential channel in the outer surface of the tip, may be provided. Although the described embodiment is an axial flow fan, the invention is also applicable to mixed flow fans. In such applications, the duct ring is not necessarily cylindrical but could be conical or have a diameter that increases exponentially.

Claims (9)

  1. A meridional fan adapted to be rotatably mounted in a duct ring (3) of circular cross section for impelling air through the duct, and having a plurality of fan blades (2) with peripheral blade tips (4) having a width defining an arc with a circumferential extent describing, in operation, a circular path adjacent the duct ring (3), the blade tips (4) each having a leading edge (6), a trailing edge (9) and a tip outer surface (8), a leakage path being formed between the tip outer surface (8) and the duct ring (3), at least one of the edges (6) and/or the outer surface (8) having a non-uniform profile for influencing the flow of air through the flow leakage path, characterised in that:
    the or each tip (4) has a flange (5) extending in the axial direction on the downstream, high pressure side of the fan, which increases the length of the leakage flow path, and wherein the leading edge (6) of the flange (5) has a non-uniform profile so that the circumferential axial extent of the leading edge (6} of the flange (5) varies along the width of the blade tip..
  2. A fan according to claim 1, wherein the leading edge (6) of the flange has an undulating profile.
  3. A fan according to claim 1, or 2, wherein the trailing edge of the fan tip includes a stepped shoulder (9) extending at least partially across the width of the blade tip (3).
  4. A fan according to claim 3, wherein the stepped shoulder (9) comprises a plurality of stepped recesses spaced across the width of the blade tip.
  5. A fan according to claim 5, wherein the stepped recesses (9) are regularly spaced across the width of the blade tip.
  6. A fan according to any one of the preceding claims, wherein the outer tip surface (8) has a non-uniform profile in the circumferential direction.
  7. A fan according to any one of the preceding claims wherein the outer tip surface (8) has a non-uniform profile in the axial direction.
  8. A fan according to claim 6 or 7, wherein the non-uniform profile is formed by undulations or by grooves (10) or a mixture thereof.
  9. A fan according to claim 9, wherein the undulations and/or grooves (10) extend partially or completely along the axial extent of the outer surface.
EP09701751.1A 2008-01-14 2009-01-13 A meridional fan Active EP2242932B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0800582A GB2452104B (en) 2008-01-14 2008-01-14 A meridional fan
PCT/GB2009/000088 WO2009090376A1 (en) 2008-01-14 2009-01-13 A meridional fan

Publications (2)

Publication Number Publication Date
EP2242932A1 EP2242932A1 (en) 2010-10-27
EP2242932B1 true EP2242932B1 (en) 2017-07-12

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EP09701751.1A Active EP2242932B1 (en) 2008-01-14 2009-01-13 A meridional fan

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EP (1) EP2242932B1 (en)
ES (1) ES2636989T3 (en)
GB (1) GB2452104B (en)
WO (1) WO2009090376A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI443262B (en) * 2010-12-29 2014-07-01 Delta Electronics Inc Fan and impeller thereof
EP2530330B1 (en) * 2011-06-01 2016-05-25 MTU Aero Engines AG Rotor blade for the compressor of a turbo engine, compressor and turbo machine
US10422349B2 (en) 2014-07-08 2019-09-24 Daikin Industries, Ltd. Propeller fan and blower unit
CN108087330A (en) * 2017-11-27 2018-05-29 珠海格力电器股份有限公司 Blade construction and with its air conditioner

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030095864A1 (en) * 2001-11-19 2003-05-22 Borislav Ivanovic Fan with reduced noise

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JPS5115210A (en) * 1974-07-02 1976-02-06 Rotoron Inc Zatsuongenshono fuan
DE3017226A1 (en) * 1979-05-12 1980-11-20 Papst Motoren Kg FAN BLADE
DE3234011A1 (en) * 1982-09-14 1984-03-15 Braun Ag, 6000 Frankfurt Axial fan
JPS59185898A (en) * 1983-04-08 1984-10-22 Aisin Seiki Co Ltd Fan blade
SU1339308A1 (en) * 1986-04-14 1987-09-23 Всесоюзный Научно-Исследовательский И Проектно-Конструкторский Институт По Оборудованию Для Кондиционирования Воздуха И Вентиляции Axial-flow fan blade
JPH01106998A (en) * 1987-10-20 1989-04-24 Seiko Electronic Components Ltd Shape of fan of axial flow blower
FR2753495B1 (en) * 1996-09-19 1998-11-13 Valeo Thermique Moteur Sa FAN, IN PARTICULAR FOR A COOLING AND / OR HEATING AND / OR AIR CONDITIONING APPARATUS OF A MOTOR VEHICLE
JPH10148199A (en) * 1996-11-18 1998-06-02 Mitsubishi Heavy Ind Ltd Axial flow fan device
DE10352253A1 (en) * 2003-11-08 2005-06-09 Alstom Technology Ltd Compressor blade
US20060034697A1 (en) * 2004-08-12 2006-02-16 Cheng-Kang Chen Propeller structure of a fan

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Publication number Priority date Publication date Assignee Title
US20030095864A1 (en) * 2001-11-19 2003-05-22 Borislav Ivanovic Fan with reduced noise

Also Published As

Publication number Publication date
EP2242932A1 (en) 2010-10-27
ES2636989T3 (en) 2017-10-10
WO2009090376A1 (en) 2009-07-23
GB2452104B (en) 2009-07-22
GB0800582D0 (en) 2008-02-20
GB2452104A (en) 2009-02-25

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