WO2007089081A1 - Axial flow fan - Google Patents

Axial flow fan Download PDF

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Publication number
WO2007089081A1
WO2007089081A1 PCT/KR2007/000234 KR2007000234W WO2007089081A1 WO 2007089081 A1 WO2007089081 A1 WO 2007089081A1 KR 2007000234 W KR2007000234 W KR 2007000234W WO 2007089081 A1 WO2007089081 A1 WO 2007089081A1
Authority
WO
WIPO (PCT)
Prior art keywords
blade
angle
hub
axial flow
tip
Prior art date
Application number
PCT/KR2007/000234
Other languages
English (en)
French (fr)
Inventor
Kyung Seok Cho
Se Young Park
Woo June Kim
Original Assignee
Halla Climate Control Corp.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Halla Climate Control Corp. filed Critical Halla Climate Control Corp.
Priority to JP2008553148A priority Critical patent/JP4895314B2/ja
Priority to EP07700961A priority patent/EP1979624A4/en
Priority to US12/162,895 priority patent/US20120003097A1/en
Priority to CN2007800042572A priority patent/CN101379300B/zh
Publication of WO2007089081A1 publication Critical patent/WO2007089081A1/en

Links

Classifications

    • 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
    • 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
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/328Rotors specially for elastic fluids for axial flow pumps for axial flow fans with unequal distribution of blades around the hub
    • 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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form
    • F04D29/386Skewed blades
    • 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • 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
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes

Definitions

  • the present invention relates to an axial flow fan, and more particularly, to an axial flow fan capable of promoting structural stability so as to decrease deformation and unbalance of a blade and accomplishing low noise level.
  • an axial flow fan 10 which is used for cooling heat exchange medium passing an inside of a heat exchanger such as a radiator, a condenser and so on of a vehicle, is provided with a hub 20 coupled to a shaft 52 of a driving source 50 such as a motor, a plurality of blades 30 arranged radially at an outer circumference of the hub 20, and a fan band 40 for connecting tips of the blades 30 so as to prevent the blades from being deformed.
  • the axial flow fan 10 is therefore rotated by rotational force transferred from the driving source 50 to the hub 20 and blows air in an axial direction by the blades 30.
  • a shroud 60 fixed to the heat exchanger is used to guide efficiently the air blown by the axial flow fan 10.
  • the shroud 60 is formed so as to have a blowhole which is sized so that the axial flow fan 10 can be rotatably inserted therein, and support the motor 50 which is a driving source.
  • a leading edge LE which is an edge at a side of a rotational direction and a trailing edge TE which is an edge at an opposite side of the rotational direction have a backward sweeping angle inclined toward an opposite direction of the rotation as it goes from a root 32 of the blade connecting the blade 30 to the hub 20 to a center portion of the blade 30 and a forward sweeping angle inclined toward the rotational direction as it goes to a tip 34 of the blade connecting the blade to the fan band 40.
  • Such change of the sweep angle is an important factor in performance of the axial flow fan, however it is known to be difficult to obtain satisfactory blowing efficiency and noise reduction effect.
  • the former axial flow fan 10a has a waveform structured blade 30a, in which the sweeping angles of the leading edge LE and the trailing edge TE change alternately from a backward to a forward and from the forward to the backward as it goes from a root 32a of the blade toward a tip 34a of the blade. Further, a chord length CL is gradually increased as it goes from the root 32a of the blade toward the tip 34a of the blade.
  • a reference symbol ⁇ denotes an angle of the blade 30 in relation to a horizontal line H.
  • Reference symbols 20a and 40a denote the hub and the fan bend respectively.
  • the latter axial flow fan 10b has a waveform structured blade 30b as same as the former, and a chord length CL (see Fig. 4) is also gradually increased as it goes from the root 32b of the blade toward the tip 34b of the blade 34b. Further, the root 32b of the blade has maximum backward sweeping angle and the tip 34b of the blade has maximum forward sweeping angle.
  • Reference symbols 20b and 40b denote the hub and the fan band respectively.
  • an area between inflection points Pl and P2 located on a mid- chord line, which runs along middle points between the leading edge LE and the trailing edge TE, works as an area for dispersing air flow and thus prevent the air flow from being concentrated, thereby capable of increasing blowing efficiency and reducing noise compared to the axial flow fan shown in Fig. 1 and Fig. 2.
  • an equiangular distribution angle is defined as a case that the distribution angle becomes 360/n.
  • the distribution angle Al of the blade can be moved by a predetermined angle in a rotational direction (+) or an opposite direction of the rotation (-) of the axial flow fan in the equiangular distribution angle, and at this time a range in which the angle can be increased or decreased is referred as a clearance angle B.
  • a clearance angle B a range in which the angle can be increased or decreased.
  • 5,000,660 discloses an axial flow fan with a blade of an uneven structure in which curvatures from a root of the blade to a tip of the blade are different at least between two blades, and the axial flow fan is suggested for the purpose of increasing rigidity of a portion of the root of the blade and reducing noise in a portion of the tip of the blade.
  • An object of the present invention is to provide an axial flow fan capable of promoting structural stability so as to decrease deformation and unbalance of a blade and accomplishing low noise level by determining a distribution angle of the blade with an optimum clearance angle and thereby determining uneven rate of the blade.
  • an axial flow fan including, a hub (110) ; a plurality of blades (120) arranged radially in a circumference of the hub and having a sweeping angle of which direction changes alternately in an area between a root (122) and a tip (124) of the blade; and a fan band (130) for connecting integrally the tips of the each blade; wherein when assuming that an angle between two lines (Ll, L2) which pass through a center (C) of the hub 110 and middles (Cl, C2) of each root of the blade, respectively, where the adjacent two blades (120) and the hub
  • a hub- side distribution angle of the blade an angle between two lines which pass through a center of the hub and middles of each root of the blade, respectively, where the adjacent two blades and the hub come into contact is, a hub- side distribution angle of the blade, and an angle between two lines which pass through a center of the hub and middles of each tip of the two blades (120), respectively is a tip-side distribution angle of the blade, the hub-side distribution angle of blade and the tip-side distribution angle of blade are same.
  • the blade has the sweeping angle which changes gradually as it goes from the tip of the blade having a forward angle to the root of the blade having a backward angle and connected to the hub and a plurality of flow dispersing areas (D) between the forward angle area of a side of the tip of the blade and the backward angle area of a side of the root of the blade, in which a direction of the sweeping angle is alternately reversed.
  • D flow dispersing areas
  • the blade has a leading edge (LE) extending from the tip of the blade to the root of the blade, and a direction of a sweeping angle of the leading edge changes gradually from a maximum backward angle at the root of the blade to a maximum forward angle at the tip of the blade, wherein the direction of the sweeping angle is reversed from the backward angle at a side of the root of the blade to a forward angle, then reversed to a backward angle and reversed again to a forward angle so as to be connected to a forward angle at a side of the tip of the blade.
  • LE leading edge
  • the blade has a trailing edge (TE) extending from the tip of the blade to the root of the blade, and a changing pattern of a sweeping angle of the trailing edge (TE) is as same as that of the leading edge (LE) .
  • Fig. 1 is an exploded perspective view illustrating an example of a conventional axial flow fan and shroud assembly.
  • Fig. 2 is a partial front view illustrating the conventional axial flow fan.
  • Fig. 3 is a front view illustrating another example of a conventional axial flow fan.
  • Fig. 4 is a sectional view of a blade for defining a chord.
  • Fig. 5 is a perspective view illustrating yet another example of a conventional axial flow fan.
  • Fig. 6 is a partial front view illustrating the axial flow fan shown in Fig. 5.
  • Fig. 7 is a partial front view for explaining distribution angle of a blade in the axial flow fan shown in Fig. 5.
  • Fig. 8 is a front view illustrating an embodiment of an axial flow fan according to the present invention.
  • Fig. 9 is a partial front view for explaining a structure of a blade in the axial flow fan of the present invention shown in
  • Fig. 10 to Fig. 15 are graphs comparatively showing noise levels according to frequency in relation to the axial flow fan according to the present invention and the conventional axial flow fan.
  • Fig. 16 is a graph showing variation pattern in overall noise according to variation of a clearance angle.
  • Fig. 8 illustrates an axial flow fan according to the present invention.
  • the axial flow fan 100 includes a hub 110; a plurality of blades 120 radially arranged at a circumference of the hub 110 and having a sweeping angle of which direction changes alternately in an area between a root 122 of the blade and a tip 124 of the blade; and a fan band 130 for connecting integrally the tips 124 of the each blade 120.
  • the illustrated axial flow fan 100 has 9 blades 120.
  • an angle between two lines Ll and L2 which pass through a center C of the hub 110 and middles Cl and C2 of each root 122 of the blade, respectively, where the adjacent two blades 120 and the hub 110 come into contact is a distribution angle Al of the blade
  • a range of an angle by which the distribution angle Al of the blade is movable in a rotational direction (+) or an opposite direction of rotation (-) of the axial flow fan 100 is a clearance angle
  • a number of the blade is n
  • an equiangular distribution, representing an interval by which the blades are arranged can be defined by 360/n.
  • the blades 120 can be exemplary arranged in interval of 40°, an actual angular distribution of the blade 120 can be moved in the rotational direction (+) or the opposite direction of rotation (-) of the axial flow fan 100 by a predetermined angle in the range of the clearance angle.
  • FIG. 9 is a partial front view for explaining a structure of the blade in the axial flow fan of the present invention shown in Fig. 8.
  • the leading edge LE of the blade 120 has a sweeping angle of which direction is gradually changes from the maximum backward sweeping angle at the root 122 of the blade to the maximum forward sweeping angle at the tip 124 of the blade in a full section between the root 122 of the blade and the tip 124 of the blade.
  • leading edge LE has a flow dispersing area D, which is a small section starting from a first inflection point rii, at which the direction of the sweeping angle is changes from backward to forward, passing through a second inflection point ri 2 , at which the direction of the sweeping angle is changes again from forward to backward, and reaching to a third inflection point ri 3 , at which the direction of the sweeping angle is changes again from backward to forward.
  • a flow dispersing area D which is a small section starting from a first inflection point rii, at which the direction of the sweeping angle is changes from backward to forward, passing through a second inflection point ri 2 , at which the direction of the sweeping angle is changes again from forward to backward, and reaching to a third inflection point ri 3 , at which the direction of the sweeping angle is changes again from backward to forward.
  • the leading edge LE of the blade 120 is formed such that the direction of the sweeping angle gradually changes from backward at a side of root 122 of the blade in an order of forward, backward and forward, and finally to forward at a side of the tip 124 of the blade between a backward area of the side of the root 122 of the blade 120 and a forward area of the side of the tip 124 of the blade 120.
  • the trailing edge TE of the blade 120 is also formed as same pattern as the leading edge LE, that is, such that the direction of the sweeping angle gradually changes from backward at a side of root 122 of the blade in an order of forward, backward and forward, and finally to forward at a side of the tip 124 of the blade between the backward area of the side of the root 122 of the blade 120 and the forward area of the side of the tip 124 of the blade 120.
  • the flow dispersing area D forms two flow concentrating parts Sl and S2 at which flows are concentrated to a side of the trailing edge TE and thus acts to lessen greatly concentration of the flow, thereby increasing a blowing efficiency relative to power consumption and greatly reducing noise generation.
  • Fig. 10 to Fig. 15 are graphs comparatively showing noise levels throughout frequencies in the case that the clearance angle is 4° to 9° according to the present invention.
  • test to the axial flow fans according to the present invention (the first and second embodiments) and the conventional axial flow fan under the condition of same voltage showed that the axial flow fans according to the present are much lower in noise level than the conventional one.
  • the axial flow fans according to the present invention has much air flow rate in a low rpm and test to the axial flow fans according to the present invention and the conventional axial flow fan under the condition of same air flow rate showed that the axial flow fans according to the present are much lower in noise level, rpm and voltage than the conventional one.
  • noise level of even fan is denoted with black solid line and noise levels of each uneven fan are denoted with gray dotted lines.
  • noise levels of each uneven fan are denoted with gray dotted lines.
  • Table 1 lists data of variation in overall noise according to the clearance angle and Fig. 16 graphically shows the data of table 1. [Table l]
  • Fig. 16 shows clearly a tendency, in which the noise is very high in the case that the distribution angle of blade is the equiangular distribution angle, that is, the clearance angle is 0°, and the noise is gradually reduced with increase of the clearance angle while the noise is increased again if the clearance angle passes over a specific value.
  • the noise is clearly reduced in the case that the clearance angle is 4° to 9° than in the case of the even fan, particularly noise reduction effect is maximized in the case that the clearance angle is 6° to 7°.
  • the above described axial flow fan is capable of promoting silence operation of an apparatus which employs an axial flow fan as noise can be greatly reduced compared to the conventional axial flow fan by determining the distribution angle of the blade 120 with an optimum clearance angle. Further, blowing efficiency and noise reduction effect can be much increased by adjusting the clearance angle as well as forming the flow dispersing area on the blade.
  • the axial flow fan according to the present invention can generate much air flow rate even in low rpm compared to the conventional one, it is capable of promoting structural stability and thus increasing durability of the axial fan.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PCT/KR2007/000234 2006-02-03 2007-01-15 Axial flow fan WO2007089081A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2008553148A JP4895314B2 (ja) 2006-02-03 2007-01-15 軸流ファン
EP07700961A EP1979624A4 (en) 2006-02-03 2007-01-15 AXIAL FLOW FAN
US12/162,895 US20120003097A1 (en) 2006-02-03 2007-01-15 Axial flow fan
CN2007800042572A CN101379300B (zh) 2006-02-03 2007-01-15 轴流式风扇

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
KR10-2006-0010535 2006-02-03
KR20060010535 2006-02-03
KR10-2007-0001552 2007-01-05
KR1020070001552A KR101328559B1 (ko) 2006-02-03 2007-01-05 축류팬

Publications (1)

Publication Number Publication Date
WO2007089081A1 true WO2007089081A1 (en) 2007-08-09

Family

ID=38600424

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/KR2007/000234 WO2007089081A1 (en) 2006-02-03 2007-01-15 Axial flow fan

Country Status (6)

Country Link
US (1) US20120003097A1 (ja)
EP (1) EP1979624A4 (ja)
JP (1) JP4895314B2 (ja)
KR (1) KR101328559B1 (ja)
CN (1) CN101379300B (ja)
WO (1) WO2007089081A1 (ja)

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Publication number Priority date Publication date Assignee Title
FR2965315A1 (fr) * 2010-09-29 2012-03-30 Valeo Systemes Thermiques Helice pour ventilateur dont l'angle de calage varie
GB2507493B (en) * 2012-10-30 2015-07-15 Solyvent Flakt Ab Air movement fans
WO2017085134A3 (en) * 2015-11-16 2017-06-29 R.E.M. Holding S.R.L. Low noise and high efficiency blade for axial fans and rotors and axial fan or rotor comprising said blade
US9970453B2 (en) 2010-09-29 2018-05-15 Valeo Systemes Thermiques Propeller for ventilator, with a variable chord length

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KR101470004B1 (ko) * 2008-07-21 2014-12-05 한라비스테온공조 주식회사 축류팬
JP5199849B2 (ja) * 2008-12-05 2013-05-15 三菱重工業株式会社 車両用熱交換モジュールおよびこれを備えた車両
KR101218536B1 (ko) * 2010-01-06 2013-01-07 한라공조주식회사 축류팬
KR101681772B1 (ko) * 2010-02-02 2016-12-01 한온시스템 주식회사 차량용 축류팬
CN102207106A (zh) * 2010-03-31 2011-10-05 鸿富锦精密工业(深圳)有限公司 风扇整流架
CN105221480A (zh) * 2010-11-05 2016-01-06 台达电子工业股份有限公司 风扇结构
JP5108977B1 (ja) * 2012-01-23 2012-12-26 シナノケンシ株式会社 圧縮機又は真空機
KR101408917B1 (ko) * 2012-01-30 2014-06-18 한라비스테온공조 주식회사 축류팬
JP5622777B2 (ja) 2012-03-23 2014-11-12 シナノケンシ株式会社 圧縮機又は真空機
CN102788043B (zh) * 2012-08-03 2015-04-01 南充工塑零部件有限公司 发动机风扇
JP6704232B2 (ja) * 2015-10-05 2020-06-03 マクセルホールディングス株式会社 送風装置
WO2017061236A1 (ja) * 2015-10-05 2017-04-13 日立マクセル株式会社 送風装置
CN105275854A (zh) * 2015-10-26 2016-01-27 日本电产凯宇汽车电器(江苏)有限公司 一种汽车散热器用的电子风扇总成
JP1555680S (ja) * 2016-03-01 2016-08-08
JP6414197B2 (ja) * 2016-12-28 2018-10-31 ダイキン工業株式会社 軸流ファンおよび送風ユニット
KR102548590B1 (ko) * 2016-12-28 2023-06-29 한온시스템 주식회사 축류팬
CN106870013A (zh) * 2017-02-21 2017-06-20 戴劲松 叶片间通道扩张的涡轮机工作叶片
CN110573746B (zh) * 2017-04-28 2021-01-08 三菱电机株式会社 螺旋桨式风扇
US20190063464A1 (en) * 2017-08-31 2019-02-28 Ford Global Technologies, Llc Engine cooling fans with uneven blade spacing
CN109424580B (zh) * 2017-08-31 2020-11-20 佛山市顺德区美的电热电器制造有限公司 叶轮和具有其的风机、烹饪器具
KR102496677B1 (ko) * 2018-05-24 2023-02-07 한온시스템 주식회사 축류팬
CN111043063B (zh) * 2018-10-15 2021-06-18 广东美的白色家电技术创新中心有限公司 对旋风扇
DE202019100367U1 (de) * 2019-01-23 2020-04-24 Brose Fahrzeugteile SE & Co. Kommanditgesellschaft, Würzburg Lüfterrad eines Kraftfahrzeugs

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Publication number Priority date Publication date Assignee Title
US4684324A (en) * 1985-08-02 1987-08-04 Gate S.P.A. Axial fan, particularly for motor vehicles
US5000660A (en) 1989-08-11 1991-03-19 Airflow Research And Manufacturing Corporation Variable skew fan
EP0933534A2 (en) 1998-02-03 1999-08-04 Siemens Canada Limited Axial flow fan
US6558123B1 (en) * 1998-03-23 2003-05-06 Spal S.R.L. Axial flow fan
US6139275A (en) 1998-07-28 2000-10-31 Kabushiki Kaisha Toshiba Impeller for use in cooling dynamoelectric machine
JP2000205190A (ja) * 1998-12-31 2000-07-25 Halla Aircon Co Ltd 軸流ファン
KR20020094183A (ko) 2001-06-12 2002-12-18 한라공조주식회사 축류팬
KR20020094184A (ko) 2001-06-12 2002-12-18 한라공조주식회사 축류팬
US6908287B2 (en) 2001-06-12 2005-06-21 Halla Climate Control Corp. Axial flow fan

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2965315A1 (fr) * 2010-09-29 2012-03-30 Valeo Systemes Thermiques Helice pour ventilateur dont l'angle de calage varie
WO2012041564A1 (fr) * 2010-09-29 2012-04-05 Valeo Systemes Thermiques Hélice pour ventilateur dont l'angle de calage varie
CN103328826A (zh) * 2010-09-29 2013-09-25 法雷奥热***公司 用于风机的具有可变叶片角的推进器
JP2013538975A (ja) * 2010-09-29 2013-10-17 ヴァレオ システム テルミク ピッチ角が変化するブロアホイール
CN103328826B (zh) * 2010-09-29 2016-01-20 法雷奥热***公司 用于风机的具有可变叶片角的推进器
US9841032B2 (en) 2010-09-29 2017-12-12 Valeo Systemes Thermiques Propeller for ventilator, with a variable blade angle
US9970453B2 (en) 2010-09-29 2018-05-15 Valeo Systemes Thermiques Propeller for ventilator, with a variable chord length
GB2507493B (en) * 2012-10-30 2015-07-15 Solyvent Flakt Ab Air movement fans
WO2017085134A3 (en) * 2015-11-16 2017-06-29 R.E.M. Holding S.R.L. Low noise and high efficiency blade for axial fans and rotors and axial fan or rotor comprising said blade
US11795975B2 (en) 2015-11-16 2023-10-24 R.E.M. Holding S.R.L. Low noise and high efficiency blade for axial fans and rotors and axial fan or rotor comprising said blade

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Publication number Publication date
JP2009531578A (ja) 2009-09-03
CN101379300B (zh) 2011-11-23
EP1979624A4 (en) 2012-05-16
JP4895314B2 (ja) 2012-03-14
EP1979624A1 (en) 2008-10-15
US20120003097A1 (en) 2012-01-05
CN101379300A (zh) 2009-03-04
KR20070079905A (ko) 2007-08-08
KR101328559B1 (ko) 2013-11-13

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