EP2644898A1 - Impeller and fan - Google Patents

Impeller and fan Download PDF

Info

Publication number
EP2644898A1
EP2644898A1 EP13159732.0A EP13159732A EP2644898A1 EP 2644898 A1 EP2644898 A1 EP 2644898A1 EP 13159732 A EP13159732 A EP 13159732A EP 2644898 A1 EP2644898 A1 EP 2644898A1
Authority
EP
European Patent Office
Prior art keywords
blades
impeller
centrifugal
fan
hub
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.)
Withdrawn
Application number
EP13159732.0A
Other languages
German (de)
French (fr)
Inventor
Yung-Ching Huang
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.)
Asustek Computer Inc
Original Assignee
Asustek Computer Inc
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 Asustek Computer Inc filed Critical Asustek Computer Inc
Publication of EP2644898A1 publication Critical patent/EP2644898A1/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/025Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal comprising axial flow and radial flow stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven

Definitions

  • the invention relates to an impeller and a fan and, more particularly, to an impeller including centrifugal blades connected with axial blades, and a fan applying the impeller.
  • a graphics card As an example, most of the graphics cards use the conventional fan (such as an axial fan or a centrifugal fan) to dissipate heat.
  • the fan is disposed too close to the circuit board of the graphics card and causes problems, such as low efficiency and big noise.
  • An impeller and a fan which have wide air flow directions, low noise, long using life and can improve heat dissipating efficiency are disclosed.
  • the impeller is applied to a fan.
  • the impeller includes a hub, a plurality of centrifugal blades and a plurality of axial blades. One end of each of the centrifugal blades is disposed around circumference of the hub, and the other end of a part of the centrifugal blades is connected to the axial blades, respectively.
  • the impeller is applied to a fan.
  • the impeller includes a hub and a plurality of composite blades disposed around circumference of the hub.
  • Each of the composite blades extends from the hub and includes a centrifugal part and a centrifugal part in sequence.
  • a fan includes an impeller above-mentioned and a motor, wherein the motor is used for driving the impeller.
  • the impeller and the fan are disclosed.
  • the composite blade is disposed in the impeller (one end of the centrifugal blades is connected to the axial blades, or the centrifugal part is connected to the centrifugal part), which makes the air flow of the fan or the heat dissipating device wider, lowers noise, extends the using life of the motor and improves the heat dissipating efficiency of the heat dissipating device.
  • FIG. 1A and FIG. 1B are an explosion diagram and an assembly diagram showing a fan in a first embodiment
  • FIG. 2A and FIG. 2B are an explosion diagram and an assembly diagram showing a fan in a second embodiment
  • FIG. 3 is a schematic diagram showing air flow direction of a fan
  • FIG. 4A and FIG. 4B are an explosion diagram and an assembly diagram showing a heat dissipating device in a third embodiment.
  • FIG. 5A and FIG. 5B are an explosion diagram and an assembly diagram showing a heat dissipating device in a fourth embodiment.
  • FIG. 1A and FIG. 1B are an explosion diagram and an assembly diagram showing a fan 1 in a first embodiment.
  • the fan 1 includes an impeller 11 and a motor 12.
  • the motor 12 drives the impeller 11 to rotate.
  • the impeller 11 includes a hub 111, a plurality of the centrifugal blades 112 and a plurality of the axial blades 113.
  • the fan 1 includes the centrifugal blades 112 and the axial blades 113 to form a composite blade, and thus the fan 1 can also be regarded as a composite fan. Furthermore, since an even number of blades may make the fan unstable in operating, the number of the blades is odd, such as nine axial blades 113 in FIG. 1A and FIG. 1B , which is not limited herein.
  • the centrifugal blades 112 are disposed around the circumference of the hub 111. As shown in FIG. 1A , the axial blades 113 are connected to one end 114 of the centrifugal blades 112 away from the hub 111, respectively.
  • the number of the axial blades 113 can be less than that of the centrifugal blades 112 (the number of the axial blades 113 is half of that of the centrifugal blades 112, which is not limited herein), and the axial blades 113 are smoothly connected to the centrifugal blades 112 to form the composite blade.
  • the number of the axial blades 113 may also equal to that of the centrifugal blades 112, that is, each of the axial blades 113 is connected to one end 114 of one of the centrifugal blades 112.
  • the impeller 11 may be manufactured by injection molding, and may be made of metal (such as aluminium or aluminium magnesium alloy) or plastic, which is not limited herein.
  • the centrifugal blades 112 and the connected axial blades 113 are integrally formed, or the hub 111, the centrifugal blades 112 and the axial blades 113 are integrally formed.
  • the hub 111, the centrifugal blades 112 and the axial blades 113 are integrally formed to improve the strength of the impeller 11.
  • the length of the centrifugal blades 112 may be increased to enhance centrifugal effect (that is increasing the air quantity and the air pressure of the centrifugal blades 112).
  • the motor 12 includes a rotor (such as a magnet ring) 121, a stator 122, a spindle 123 and a base 124.
  • the spindle 123 is connected to the hub 111 and passes through the axle tube 125 at the base 124.
  • the stator 122 is sleeved on the axle tube 125, and the rotor 121 is disposed in inner peripheral of the hub 111 corresponding to the stator 122.
  • a coil of the stator 122 When a coil of the stator 122 is power on, it generates electromagnetic induction with the rotor 121, drives the spindle 123 and the rotor 121 to rotate, and further drives the impeller 11 to rotate. Since the motor 12 is known by persons with ordinary skill in the art, description of the motor 12 is omitted herein.
  • the impeller 11 further includes a connecting element 115.
  • the connecting element 115 is connected to the connecting part (which is the end 114) between the centrifugal blades 112 and the axial blades 113.
  • the connecting element 115 can strengthen the whole structure of the impeller 11 and resist air pressure to prevent the impeller 11 from deforming.
  • the connecting element (not shown) may be only connected to the centrifugal blades 112 to achieve the same functions.
  • FIG. 2A and FIG. 2B are an explosion diagram and an assembly diagram showing a fan 2 in a second embodiment.
  • the fan 2 includes an impeller 21 and a motor 22, and the motor 22 drives the impeller 21 to rotate.
  • the impeller 21 includes a hub 211 and a plurality of composite blades 212 disposed around the circumference of the hub 211.
  • Each of the composite blades 212 extends from the hub 211 and includes a centrifugal part C and an axial part A in sequence.
  • the centrifugal part C means that the composite blades 212 at the part is shaped in the centrifugal blades
  • the axial part A means that the composite blades 212 at the part is shaped in the axial blades.
  • the number of the centrifugal part C equals to that of the axial part A, and the hub 211 and the composite blades 212 are integrally formed to strengthen the impeller 21.
  • the motor 22 includes a rotor (such as a magnet ring) 221, a stator 222, a spindle 223 and a base 224.
  • a rotor such as a magnet ring
  • stator 222 such as a stator
  • spindle 223 such as a spindle
  • base 224 The structure and the operating principle of the motor 22 are illustrated above, which is omitted herein.
  • the impeller 21 further includes a connecting element 215 which is connected to a connecting part 214 between the centrifugal part C and the axial part A.
  • the connecting element 215 can strengthen the whole structure of the impeller 21 and resist air pressure to prevent the impeller 21 from deforming.
  • the connecting element (not shown) may be only connected to the centrifugal part C to achieve the same functions.
  • FIG. 3 is a schematic diagram showing air flow direction of the fan 1 and the fan 2.
  • the direction of arrows in a full line indicates air inflow direction, and the direction of arrows in a dotted line indicates air outflow direction.
  • the composite blades of the fan 1 and 2 are combinations of the centrifugal blades and the axial blades (or the centrifugal part and the centrifugal part). As shown in FIG. 3 , the fan 1 or 2 has six air inflow directions (as shown in arrows in a full line) at the upper side and the bottom side, and the air flows out through the sides and flows downwards, which makes the fan 1 and the fan 2 have wide air flow directions, low noise, long using life of the motor and better heat dissipating efficiency.
  • FIG. 4A and FIG. 4B are an explosion diagram and an assembly diagram showing a heat dissipating device 3 in a third embodiment.
  • the heat dissipating device 3 includes a fan 1 and a heat dissipater 4.
  • the heat dissipater 4 is disposed corresponding to the fan 1.
  • the heat dissipater 4 may be disposed at one side of the fan 1 (not shown).
  • the heat dissipater 4 may also be disposed around the circumference of the fan 1 (as shown in FIG. 4B ).
  • the heat dissipater 4 is a set of heat dissipating fins, which is not limited herein.
  • the heat dissipater 4 is an annular set of heat dissipating fins, and a part of the heat dissipating fins are disposed around the circumference of the fan 1, and the other part of the heat dissipating fins are disposed at the bottom of the fan 1.
  • FIG. 5A and FIG. 5B are an explosion diagram and an assembly diagram showing a heat dissipating device 5 in a fourth embodiment.
  • the heat dissipating device 5 includes a fan 2 and a heat dissipater 4. Comparing to the heat dissipating device 3, the difference is that the heat dissipater 4 cooperates with the fan 2, and other structures and the operating principle are the same as that in the third embodiment, which is omitted herein.
  • the heat dissipating devices 3 and 5 use the fans 1 and 2, respectively, and the composite blades of the fans 1 and 2 are combinations of the centrifugal blades and the axial blades (or combination of the centrifugal part and the centrifugal part).
  • the composite blades of the fans 1 and 2 are combinations of the centrifugal blades and the axial blades (or combination of the centrifugal part and the centrifugal part).
  • FIG. 3 , FIG. 4B and FIG. 5B when the fans 1 and 2 including the composite blades operate, cool air flows in the heat dissipater 4 in six directions (as shown in the full line arrows in FIG. 3 ), and hot air flows out in the directions shown in the dotted line, so as to dissipate heat.
  • the heat dissipating devices 3 and 5 When air flows out of the composite blades, it can flow downwards through the sides.
  • the heat dissipating devices 3 and 5 have six air inflow directions, and the air flows out through the sides and downwards, which increases the air quantity flowing through the heat dissipater 4, and makes the heat dissipating devices 3 and 5 have wide air flow directions, low noise, long using life of the motor and better heat dissipating efficiency.
  • the heat dissipating devices 3 and 5 When the heat dissipating devices 3 and 5 are disposed above a printed circuit board (PCB) of the graphics card, the heat dissipating devices 3 and 5 can reduce the temperature of the graphics card by three degrees comparing to the conventional heat dissipating device.
  • PCB printed circuit board

Abstract

An impeller (11) applied to a fan (1) is disclosed. The impeller (11) includes a hub (111), a plurality of centrifugal blades (112) and a plurality of axial blades (113). One end of each of the centrifugal blades (112) is disposed around the circumference of the hub (111). The axial blades (113) are respectively connected to the other end of a part of the centrifugal blades (112). A fan (1) applying the impeller (11) is also disclosed.

Description

    BACKGROUND OF THE INVENTION 1. Field of the Invention
  • The invention relates to an impeller and a fan and, more particularly, to an impeller including centrifugal blades connected with axial blades, and a fan applying the impeller.
  • 2. Description of Related Art
  • As electronic products develop high performance, high frequency, high speed and become lighter and thinner, they generate more heat, which makes them unstable and affects reliability and use life. Since a fan has a low cost and mature technology, an electronic device usually uses a fan to dissipate heat.
  • Taking a graphics card as an example, most of the graphics cards use the conventional fan (such as an axial fan or a centrifugal fan) to dissipate heat. However, the fan is disposed too close to the circuit board of the graphics card and causes problems, such as low efficiency and big noise. Moreover, it is difficult to consider both air pressure and air quantity of the fan at the same time, and air flow direction from the fan may be not suitable for the graphics card, which affects heat dissipating efficiency.
  • SUMMARY OF THE INVENTION
  • An impeller and a fan which have wide air flow directions, low noise, long using life and can improve heat dissipating efficiency are disclosed.
  • An impeller is applied to a fan. The impeller includes a hub, a plurality of centrifugal blades and a plurality of axial blades. One end of each of the centrifugal blades is disposed around circumference of the hub, and the other end of a part of the centrifugal blades is connected to the axial blades, respectively.
  • An impeller is applied to a fan. The impeller includes a hub and a plurality of composite blades disposed around circumference of the hub. Each of the composite blades extends from the hub and includes a centrifugal part and a centrifugal part in sequence.
  • A fan includes an impeller above-mentioned and a motor, wherein the motor is used for driving the impeller.
  • As stated above, the impeller and the fan are disclosed. The composite blade is disposed in the impeller (one end of the centrifugal blades is connected to the axial blades, or the centrifugal part is connected to the centrifugal part), which makes the air flow of the fan or the heat dissipating device wider, lowers noise, extends the using life of the motor and improves the heat dissipating efficiency of the heat dissipating device.
  • These and other features, aspects and advantages of the present invention will become better understood with regard to the following description, appended claims, and accompanying drawings.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1A and FIG. 1B are an explosion diagram and an assembly diagram showing a fan in a first embodiment;
  • FIG. 2A and FIG. 2B are an explosion diagram and an assembly diagram showing a fan in a second embodiment;
  • FIG. 3 is a schematic diagram showing air flow direction of a fan;
  • FIG. 4A and FIG. 4B are an explosion diagram and an assembly diagram showing a heat dissipating device in a third embodiment; and
  • FIG. 5A and FIG. 5B are an explosion diagram and an assembly diagram showing a heat dissipating device in a fourth embodiment.
  • DESCRIPTION OF THE EMBODIMENTS
  • An impeller, a fan and a heat dissipating device are illustrated with relating figures, and the same symbols denote the same components.
  • FIG. 1A and FIG. 1B are an explosion diagram and an assembly diagram showing a fan 1 in a first embodiment.
  • The fan 1 includes an impeller 11 and a motor 12. The motor 12 drives the impeller 11 to rotate.
  • The impeller 11 includes a hub 111, a plurality of the centrifugal blades 112 and a plurality of the axial blades 113. The fan 1 includes the centrifugal blades 112 and the axial blades 113 to form a composite blade, and thus the fan 1 can also be regarded as a composite fan. Furthermore, since an even number of blades may make the fan unstable in operating, the number of the blades is odd, such as nine axial blades 113 in FIG. 1A and FIG. 1B, which is not limited herein.
  • The centrifugal blades 112 are disposed around the circumference of the hub 111. As shown in FIG. 1A, the axial blades 113 are connected to one end 114 of the centrifugal blades 112 away from the hub 111, respectively. The number of the axial blades 113 can be less than that of the centrifugal blades 112 (the number of the axial blades 113 is half of that of the centrifugal blades 112, which is not limited herein), and the axial blades 113 are smoothly connected to the centrifugal blades 112 to form the composite blade.
  • The number of the axial blades 113 may also equal to that of the centrifugal blades 112, that is, each of the axial blades 113 is connected to one end 114 of one of the centrifugal blades 112. The impeller 11 may be manufactured by injection molding, and may be made of metal (such as aluminium or aluminium magnesium alloy) or plastic, which is not limited herein.
  • The centrifugal blades 112 and the connected axial blades 113 are integrally formed, or the hub 111, the centrifugal blades 112 and the axial blades 113 are integrally formed. In the embodiment, the hub 111, the centrifugal blades 112 and the axial blades 113 are integrally formed to improve the strength of the impeller 11. Moreover, the length of the centrifugal blades 112 may be increased to enhance centrifugal effect (that is increasing the air quantity and the air pressure of the centrifugal blades 112).
  • The motor 12 includes a rotor (such as a magnet ring) 121, a stator 122, a spindle 123 and a base 124. The spindle 123 is connected to the hub 111 and passes through the axle tube 125 at the base 124. The stator 122 is sleeved on the axle tube 125, and the rotor 121 is disposed in inner peripheral of the hub 111 corresponding to the stator 122. When a coil of the stator 122 is power on, it generates electromagnetic induction with the rotor 121, drives the spindle 123 and the rotor 121 to rotate, and further drives the impeller 11 to rotate. Since the motor 12 is known by persons with ordinary skill in the art, description of the motor 12 is omitted herein.
  • The impeller 11 further includes a connecting element 115. The connecting element 115 is connected to the connecting part (which is the end 114) between the centrifugal blades 112 and the axial blades 113. The connecting element 115 can strengthen the whole structure of the impeller 11 and resist air pressure to prevent the impeller 11 from deforming. The connecting element (not shown) may be only connected to the centrifugal blades 112 to achieve the same functions.
  • FIG. 2A and FIG. 2B are an explosion diagram and an assembly diagram showing a fan 2 in a second embodiment.
  • The fan 2 includes an impeller 21 and a motor 22, and the motor 22 drives the impeller 21 to rotate.
  • The impeller 21 includes a hub 211 and a plurality of composite blades 212 disposed around the circumference of the hub 211. Each of the composite blades 212 extends from the hub 211 and includes a centrifugal part C and an axial part A in sequence. The centrifugal part C means that the composite blades 212 at the part is shaped in the centrifugal blades, and the axial part A means that the composite blades 212 at the part is shaped in the axial blades. Moreover, the number of the centrifugal part C equals to that of the axial part A, and the hub 211 and the composite blades 212 are integrally formed to strengthen the impeller 21.
  • The motor 22 includes a rotor (such as a magnet ring) 221, a stator 222, a spindle 223 and a base 224. The structure and the operating principle of the motor 22 are illustrated above, which is omitted herein.
  • The impeller 21 further includes a connecting element 215 which is connected to a connecting part 214 between the centrifugal part C and the axial part A. The connecting element 215 can strengthen the whole structure of the impeller 21 and resist air pressure to prevent the impeller 21 from deforming. The connecting element (not shown) may be only connected to the centrifugal part C to achieve the same functions.
  • FIG. 3 is a schematic diagram showing air flow direction of the fan 1 and the fan 2. The direction of arrows in a full line indicates air inflow direction, and the direction of arrows in a dotted line indicates air outflow direction.
  • The composite blades of the fan 1 and 2 are combinations of the centrifugal blades and the axial blades (or the centrifugal part and the centrifugal part). As shown in FIG. 3, the fan 1 or 2 has six air inflow directions (as shown in arrows in a full line) at the upper side and the bottom side, and the air flows out through the sides and flows downwards, which makes the fan 1 and the fan 2 have wide air flow directions, low noise, long using life of the motor and better heat dissipating efficiency.
  • FIG. 4A and FIG. 4B are an explosion diagram and an assembly diagram showing a heat dissipating device 3 in a third embodiment.
  • The heat dissipating device 3 includes a fan 1 and a heat dissipater 4. The heat dissipater 4 is disposed corresponding to the fan 1. The heat dissipater 4 may be disposed at one side of the fan 1 (not shown). The heat dissipater 4 may also be disposed around the circumference of the fan 1 (as shown in FIG. 4B). The heat dissipater 4 is a set of heat dissipating fins, which is not limited herein. In the embodiment, the heat dissipater 4 is an annular set of heat dissipating fins, and a part of the heat dissipating fins are disposed around the circumference of the fan 1, and the other part of the heat dissipating fins are disposed at the bottom of the fan 1.
  • The structure and the operating principle of the fan 1 are illustrated above, which is omitted herein.
  • FIG. 5A and FIG. 5B are an explosion diagram and an assembly diagram showing a heat dissipating device 5 in a fourth embodiment.
  • The heat dissipating device 5 includes a fan 2 and a heat dissipater 4. Comparing to the heat dissipating device 3, the difference is that the heat dissipater 4 cooperates with the fan 2, and other structures and the operating principle are the same as that in the third embodiment, which is omitted herein.
  • The heat dissipating devices 3 and 5 use the fans 1 and 2, respectively, and the composite blades of the fans 1 and 2 are combinations of the centrifugal blades and the axial blades (or combination of the centrifugal part and the centrifugal part). Please refer to FIG. 3, FIG. 4B and FIG. 5B, when the fans 1 and 2 including the composite blades operate, cool air flows in the heat dissipater 4 in six directions (as shown in the full line arrows in FIG. 3), and hot air flows out in the directions shown in the dotted line, so as to dissipate heat.
  • When air flows out of the composite blades, it can flow downwards through the sides. Thus, the heat dissipating devices 3 and 5 have six air inflow directions, and the air flows out through the sides and downwards, which increases the air quantity flowing through the heat dissipater 4, and makes the heat dissipating devices 3 and 5 have wide air flow directions, low noise, long using life of the motor and better heat dissipating efficiency.
  • When the heat dissipating devices 3 and 5 are disposed above a printed circuit board (PCB) of the graphics card, the heat dissipating devices 3 and 5 can reduce the temperature of the graphics card by three degrees comparing to the conventional heat dissipating device.
  • Since the air flows downwards through the sides of the composite blades, heat from peripheral electronic elements near the heat dissipating devices 3 and 5 can also be dissipated.
  • Moreover, as persons with ordinary skills in the art know, when the motors 12 and 22 reverse operating, the six air inflow directions become six air outflow directions, and the air flows in through the sides, which broadens the air flow directions, lowers the noise, extends the using life and improves the heat dissipating efficiency.
  • Although the present invention has been described in considerable detail with reference to certain preferred embodiments thereof, the disclosure is not for limiting the scope of the invention. Persons having ordinary skill in the art may make various modifications and changes without departing from the scope of the invention. Therefore, the scope of the appended claims should not be limited to the description of the preferred embodiments described above.

Claims (10)

  1. An impeller (11) applied to a fan (1), characterized by comprising:
    a hub (111);
    a plurality of centrifugal blades (112), wherein one end of each of the centrifugal blades (112) is disposed around circumference of the hub (111); and
    a plurality of axial blades (113), wherein the other end of a part of the centrifugal blades (112) is connected to the axial blades (113), respectively.
  2. The impeller (11) according to claim 1, characterized in that the number of the axial blades (113) is less than or equals to the number of the centrifugal blades (112).
  3. The impeller (11) according to claim 1, characterized in that each of the centrifugal blades (112) and the connected axial blades (113) are integrally formed.
  4. The impeller (11) according to claim 1, characterized in that the hub (111), the centrifugal blades (112) and the axial blades (113) are integrally formed.
  5. The impeller (11) according to claim 1, characterized in that the other end of the centrifugal blades (112) is respectively connected to a connecting element (115).
  6. An impeller (11) applied to a fan (1), characterized by comprising:
    a hub (111); and
    a plurality of composite blades (212) disposed around circumference of the hub (111), wherein each of the composite blades (212) extends from the hub (111) and includes a centrifugal part (C) and an axial part (A) in sequence.
  7. The impeller (11) according to claim 6, characterized in that the impeller (11) further includes:
    a plurality of centrifugal blades (112) staggerly disposed with the composite blades (212).
  8. The impeller (11) according to claim 6, characterized in that the hub (111) and the composite blades (212) are integrally formed.
  9. The impeller (11) according to claim 6, characterized in that the impeller (11) further includes:
    a connecting element (115) connected to the centrifugal part (C) or a connecting part between the centrifugal part (C) and the centrifugal part (C).
  10. A fan (1), characterized by comprising:
    the impeller (11) according to claim 1 or 6; and
    a motor (12);
    wherein the impeller (11) is driven by the motor (12).
EP13159732.0A 2012-03-30 2013-03-18 Impeller and fan Withdrawn EP2644898A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US201261617875P 2012-03-30 2012-03-30

Publications (1)

Publication Number Publication Date
EP2644898A1 true EP2644898A1 (en) 2013-10-02

Family

ID=47913077

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13159732.0A Withdrawn EP2644898A1 (en) 2012-03-30 2013-03-18 Impeller and fan

Country Status (4)

Country Link
US (1) US20130259667A1 (en)
EP (1) EP2644898A1 (en)
CN (1) CN103362857A (en)
TW (1) TW201339432A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11905973B2 (en) * 2022-05-04 2024-02-20 Micro-Star Int'l Co., Ltd. Fan assembly

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203453120U (en) * 2013-09-03 2014-02-26 讯凯国际股份有限公司 Fan and fan impeller thereof
US10230290B2 (en) * 2014-09-08 2019-03-12 Regal Beloit America, Inc. Electrical machine and methods of assembling the same
USD765188S1 (en) * 2015-04-20 2016-08-30 Calogero A. LaRussa Flying propeller
TWM510981U (en) * 2015-07-03 2015-10-21 Cooler Master Co Ltd Assembled fan
AU2016385149B2 (en) * 2016-01-07 2019-08-29 Ningbo Hongdu Electrical Appliance Co., Ltd. Axial fan assembly and motor home air-conditioner using same
UA112277C2 (en) * 2016-03-09 2016-08-10 Вадим Володимирович Бурукін METHOD OF IMPELLER GAS EXHAUST IN AERODYNAMIC SEPARATORS, AERODYNAMIC SEPARATOR AND AIR BREEDING UNIT OF THE AERODYNAMIC SEPARATOR
DE102016224245A1 (en) * 2016-12-06 2018-06-07 Robert Bosch Gmbh Hand tool with a spring detent mechanism
WO2018198799A1 (en) * 2017-04-27 2018-11-01 日本電産株式会社 Blower device
US10859091B2 (en) * 2018-05-31 2020-12-08 Abb Schweiz Ag System having machine and fan with an axial flow inducer
CN109209993B (en) * 2018-11-09 2020-08-11 嵊州市法帝电器有限公司 Wind wheel for integrated cooker and manufacturing method thereof
JP2021160046A (en) * 2020-03-31 2021-10-11 株式会社マキタ Impact tool
CN114233679A (en) * 2020-09-09 2022-03-25 英业达科技有限公司 Fan with cooling device
TWM618603U (en) * 2021-06-15 2021-10-21 華碩電腦股份有限公司 Fan module
TWI792698B (en) * 2021-11-19 2023-02-11 圓方應用材料有限公司 Airflow multiplier blade structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1738210A (en) * 1928-09-21 1929-12-03 Frederick G Sargent Device for increasing buoyancy
US3650633A (en) * 1970-11-30 1972-03-21 Remi A Benoit In-line centrifugal fan
CN1445462A (en) * 2003-04-29 2003-10-01 上海交通大学 Pipe double axial-flow impeller
US20060034694A1 (en) * 2004-08-11 2006-02-16 Datech Technology Co., Ltd. Radial fan having axial fan blade configuration
WO2010139030A2 (en) * 2009-06-02 2010-12-09 Peter Devriese Diagonal ventilator

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2414234Y (en) * 2000-03-22 2001-01-10 台达电子工业股份有限公司 Composite blade for electric fan
US6733241B2 (en) * 2002-07-11 2004-05-11 Hunter Fan Company High efficiency ceiling fan
CN101008397A (en) * 2006-01-26 2007-08-01 赵汉高 Axial and lateral combination type fan blade

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1738210A (en) * 1928-09-21 1929-12-03 Frederick G Sargent Device for increasing buoyancy
US3650633A (en) * 1970-11-30 1972-03-21 Remi A Benoit In-line centrifugal fan
CN1445462A (en) * 2003-04-29 2003-10-01 上海交通大学 Pipe double axial-flow impeller
US20060034694A1 (en) * 2004-08-11 2006-02-16 Datech Technology Co., Ltd. Radial fan having axial fan blade configuration
WO2010139030A2 (en) * 2009-06-02 2010-12-09 Peter Devriese Diagonal ventilator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11905973B2 (en) * 2022-05-04 2024-02-20 Micro-Star Int'l Co., Ltd. Fan assembly

Also Published As

Publication number Publication date
US20130259667A1 (en) 2013-10-03
TW201339432A (en) 2013-10-01
CN103362857A (en) 2013-10-23

Similar Documents

Publication Publication Date Title
EP2644898A1 (en) Impeller and fan
US7381027B2 (en) Fan motor
US20090180901A1 (en) Fan and inner rotor motor thereof
JPWO2008062835A1 (en) Series axial fan
US20080101966A1 (en) High efficient compact radial blower
CN101517865A (en) Electrical machine with an internally cooled rotor
US20190120243A1 (en) Fan impeller structure and cooling fan thereof
TWI493113B (en) Thin dissipating fan with an axial air gap motor and selecting method for motor size thereof
KR20200018614A (en) compressor
CN209590756U (en) Cooling device
US9065320B2 (en) Passive drive motors and passive fans for use therewith
CN101044324B (en) Fan stator
JP2016102469A (en) Centrifugal fan
US11162498B2 (en) Fan
CN101201057A (en) Thermal fan for electronic chips
US7443671B2 (en) Axial duct cooling fan
CN105736419A (en) Fan
CN211692878U (en) Circulation cooling type heat radiation fan
CN201068873Y (en) Electronic chip heat radiating fan
CN101487478A (en) Fan and its inner rotor motor
EP3879680A1 (en) Motor arrangement
CN102536858A (en) Fan
JP5392330B2 (en) Centrifugal fan
JP6276169B2 (en) Centrifugal fan
CN101498320B (en) Fan and impeller thereof

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

17P Request for examination filed

Effective date: 20140227

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

17Q First examination report despatched

Effective date: 20190125

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20190605