US20120100001A1 - Fan structure - Google Patents

Fan structure Download PDF

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Publication number
US20120100001A1
US20120100001A1 US12/908,059 US90805910A US2012100001A1 US 20120100001 A1 US20120100001 A1 US 20120100001A1 US 90805910 A US90805910 A US 90805910A US 2012100001 A1 US2012100001 A1 US 2012100001A1
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US
United States
Prior art keywords
polygonal
blades
fan
fan structure
blade
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.)
Abandoned
Application number
US12/908,059
Inventor
Cheng-Kang Chen
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.)
Zaward Corp
Original Assignee
Zaward 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 Zaward Corp filed Critical Zaward Corp
Priority to US12/908,059 priority Critical patent/US20120100001A1/en
Assigned to ZAWARD CORPORATION reassignment ZAWARD CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CHEN, CHENG-KANG
Publication of US20120100001A1 publication Critical patent/US20120100001A1/en
Abandoned legal-status Critical Current

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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
    • 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
    • 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
    • F04D25/0606Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
    • F04D25/0613Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump the electric motor being of the inside-out type, i.e. the rotor is arranged radially outside a central stator
    • 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 a fan, in particular to a fan structure which is capable of reducing an aerodynamic drag.
  • a conventional heat-dissipating system applied to a computer host or other electronic apparatus includes a heat-dissipating fan for generating compulsive airflow for dissipating the heat to the outside. Since the heat-dissipating fan operates for a long period of time, the heat-dissipating effect thereof is much relevant to its operating efficiency. On the other hand, if the noise generated by the heat-dissipating fan is too large, the user will feel very uncomfortable.
  • airflow is generated when a fan rotates.
  • the airflow forms a thin layer, referred to as a boundary layer, when it passes through the surface of blades of the fan.
  • the boundary layer of airflow may generate turbulent flows beyond separating points where the airflow separates from the blades.
  • the turbulent flows may cause the blades to vibrate and thus generate undesirable noise.
  • a frictional force may generate between the surface of the blade and the airflow, which deteriorates the rotating efficiency of the fan.
  • controlling a flow field is one method for reducing the frictional force and extending the distance of the separating points from the boundary layer.
  • the present Inventor proposes a reasonable and novel structure based on his research and expert knowledge.
  • the present invention is to provide a fan structure, which is capable of reducing a frictional force and noise generated by the fan.
  • the present invention is to provide a fan structure, whereby the rotation of blades is smoother, labor-saving and power-saving, and the heat-dissipating efficiency of the fan is increased.
  • the present invention is to provide a fan structure including a hub and a plurality of blades extending from the periphery of the hub, the airflow generated by the fan forming a boundary layer on the surface of each blade, characterized in that: each of the blades is provided with a plurality of polygonal dents, a turbulent flow is generated in each dent when the airflow passes through the dent, and a plurality of the turbulent flows collect together to form an air film between the surface of blade and the boundary layer.
  • the present invention is to provide a fan structure, in which the periphery of a casing is formed with recessed portions recessed toward an accommodating space in the fan. With this arrangement, more external air can be introduced into an intake side and the exhaust resistance generated on an exhaust side can be lowered.
  • the present invention is to provide a fan structure, in which the polygonal dents provided on the surface of each blade is formed into a shape selected from a group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon. With this arrangement, the fan can generate turbulent flows in each polygonal dent at different rotating speeds.
  • the fan structure of the present invention is provided on the blade with a plurality of polygonal dents.
  • the airflow passes through the surface of each blade, the airflow is brought into contact with the periphery of each polygonal dent to generate a turbulent flow.
  • the turbulent flow stays in the polygonal dent.
  • a plurality of the turbulent flows collect together to form an air film for separating the surface of the blade from the boundary layer. Since the air film can extend the distance of the separating points from the boundary layer to thereby prevent the generation of the turbulent flows near the blades, the noise and the frictional force generated by the turbulent flows can be reduced. Therefore, the rotation of the blades is smoother, labor-saving and power-saving, and the heat-dissipating efficiency of the fan is increased.
  • FIG. 1 is an assembled perspective view showing the external appearance of the fan according to the present invention
  • FIG. 2 is a perspective view showing the external appearance of the hub and the blades according to the present invention.
  • FIG. 3 is an assembled cross-sectional view showing the hub and the blades according to the present invention.
  • FIG. 4 is a schematic view showing the airflow generated by the fan according to the present invention.
  • FIG. 5 is a schematic view showing the relationship between the blade and the airflow generated by the fan according to the present invention.
  • FIG. 6 is a schematic view showing the blade according to a second embodiment of the present invention.
  • the present invention provides a fan 1 , which includes a casing 10 , a hub 20 and a plurality of blades 30 extending from the periphery of the hub 20 .
  • the casing 10 is formed into a square frame and has an accommodating space 100 therein.
  • the hub 20 and the plurality of blades 30 are combined in the accommodating space 100 .
  • the casing 10 comprises an intake side 11 and an exhaust side 12 opposite to the intake side 11 .
  • the peripheries of the intake side 11 and the exhaust side 12 are formed with a recessed portion 13 respectively which is recessed toward the accommodating space 100 .
  • four recessed portions 13 are provided, and each recessed portion 13 is provided in the center of each side of the casing 10 .
  • the hub 20 and the blades 30 extending from the periphery of the hub 20 are combined in the accommodating space 100 .
  • the interior of the hub 20 has a shaft 21 and a motor (not shown).
  • the motor drives the shaft 21 of the hub 20 to rotate, which causes the blades 30 provided at the periphery of the hub 20 to rotate accordingly to thereby generate airflow.
  • Each of the blades 30 comprises a first surface 31 and a second surface 32 opposite to the first surface 31 .
  • Each of the blades 30 is provided on its surfaces with a plurality of polygonal dents 33 .
  • These polygonal dents 33 may be formed into any one shape selected from the group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon. Thus, two adjacent sides of the polygonal dent 33 form an angle.
  • the first surface 31 and the second surface 32 of the blade 30 are provided with the polygonal dents 33 .
  • the polygonal dents 33 may be only provided on the first surface 31 or the second surface 32 .
  • FIG. 4 is a schematic view showing the airflow generated by the fan according to the present invention
  • FIG. 5 is a schematic view showing the relationship between the blade and the airflow generated by the fan according to the present invention.
  • the airflow A generated by the fan 1 forms a boundary layer B on the surface of each blade 30 .
  • the airflow A passes through the periphery of each polygonal dent 31 , the airflow A generates a turbulent flow T in the polygonal dent 33 .
  • Many turbulent flows T collect together to form an air film between the surface of the blade 30 and the boundary layer B.
  • the air film can extend the distance of separating points S from the boundary layer B, so that the separating points S are formed outside the blade 30 .
  • each of the polygonal dents 33 may be formed into a shape of fewer sides such as a triangle or quadrangle shape. Contrarily, when the speed of the airflow A is smaller, each of the polygonal dents 33 may be formed into a shape of more sides such as a hexagon or heptagon shape.
  • FIG. 6 shows the second embodiment of the present invention.
  • the difference between the second embodiment and the first embodiment lies in that: the polygonal dents 33 a on the blade 30 a may be formed into at least two shapes selected from the group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon.

Abstract

A fan structure includes a hub and a plurality of blades extending from the periphery of the hub. The airflow generated by the fan forms a boundary layer on the surface of each blade. The present invention is characterized in that: each of the blades is provided with a plurality of polygonal dents, a turbulent flow is generated in each dent when the airflow passes through the dent, a plurality of the turbulent flows collect together to form an air film between the surface of blade and the boundary layer. By this structure, the distance of separating points from the boundary layer is extended, and the frictional force and noise caused by the rotation of the blades are reduced.

Description

    BACKGROUND OF THE INVENTION
  • 1. Field of the Invention
  • The present invention relates to a fan, in particular to a fan structure which is capable of reducing an aerodynamic drag.
  • 2. Description of Prior Art
  • A conventional heat-dissipating system applied to a computer host or other electronic apparatus includes a heat-dissipating fan for generating compulsive airflow for dissipating the heat to the outside. Since the heat-dissipating fan operates for a long period of time, the heat-dissipating effect thereof is much relevant to its operating efficiency. On the other hand, if the noise generated by the heat-dissipating fan is too large, the user will feel very uncomfortable.
  • In general, airflow is generated when a fan rotates. The airflow forms a thin layer, referred to as a boundary layer, when it passes through the surface of blades of the fan. The boundary layer of airflow may generate turbulent flows beyond separating points where the airflow separates from the blades. The turbulent flows may cause the blades to vibrate and thus generate undesirable noise. Further, due to the turbulent flows, a frictional force may generate between the surface of the blade and the airflow, which deteriorates the rotating efficiency of the fan. According to experimental data, controlling a flow field is one method for reducing the frictional force and extending the distance of the separating points from the boundary layer. Thus, it is an important issue for the present Inventor to change the flow field around the surface of an article so as to reduce the frictional force.
  • In view of the above, the present Inventor proposes a reasonable and novel structure based on his research and expert knowledge.
  • SUMMARY OF THE INVENTION
  • The present invention is to provide a fan structure, which is capable of reducing a frictional force and noise generated by the fan.
  • The present invention is to provide a fan structure, whereby the rotation of blades is smoother, labor-saving and power-saving, and the heat-dissipating efficiency of the fan is increased.
  • The present invention is to provide a fan structure including a hub and a plurality of blades extending from the periphery of the hub, the airflow generated by the fan forming a boundary layer on the surface of each blade, characterized in that: each of the blades is provided with a plurality of polygonal dents, a turbulent flow is generated in each dent when the airflow passes through the dent, and a plurality of the turbulent flows collect together to form an air film between the surface of blade and the boundary layer.
  • The present invention is to provide a fan structure, in which the periphery of a casing is formed with recessed portions recessed toward an accommodating space in the fan. With this arrangement, more external air can be introduced into an intake side and the exhaust resistance generated on an exhaust side can be lowered.
  • The present invention is to provide a fan structure, in which the polygonal dents provided on the surface of each blade is formed into a shape selected from a group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon. With this arrangement, the fan can generate turbulent flows in each polygonal dent at different rotating speeds.
  • In comparison with prior art, the fan structure of the present invention is provided on the blade with a plurality of polygonal dents. When the airflow passes through the surface of each blade, the airflow is brought into contact with the periphery of each polygonal dent to generate a turbulent flow. The turbulent flow stays in the polygonal dent. A plurality of the turbulent flows collect together to form an air film for separating the surface of the blade from the boundary layer. Since the air film can extend the distance of the separating points from the boundary layer to thereby prevent the generation of the turbulent flows near the blades, the noise and the frictional force generated by the turbulent flows can be reduced. Therefore, the rotation of the blades is smoother, labor-saving and power-saving, and the heat-dissipating efficiency of the fan is increased.
  • BRIEF DESCRIPTION OF DRAWING
  • FIG. 1 is an assembled perspective view showing the external appearance of the fan according to the present invention;
  • FIG. 2 is a perspective view showing the external appearance of the hub and the blades according to the present invention;
  • FIG. 3 is an assembled cross-sectional view showing the hub and the blades according to the present invention;
  • FIG. 4 is a schematic view showing the airflow generated by the fan according to the present invention;
  • FIG. 5 is a schematic view showing the relationship between the blade and the airflow generated by the fan according to the present invention; and
  • FIG. 6 is a schematic view showing the blade according to a second embodiment of the present invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The detailed description and technical contents of the present invention will become apparent with the following detailed description accompanied with related drawings. It is noteworthy to point out that the drawings is provided for the illustration purpose only, but not intended for limiting the scope of the present invention.
  • Please refer to FIGS. 1 to 3. The present invention provides a fan 1, which includes a casing 10, a hub 20 and a plurality of blades 30 extending from the periphery of the hub 20.
  • The casing 10 is formed into a square frame and has an accommodating space 100 therein. The hub 20 and the plurality of blades 30 are combined in the accommodating space 100. The casing 10 comprises an intake side 11 and an exhaust side 12 opposite to the intake side 11. The peripheries of the intake side 11 and the exhaust side 12 are formed with a recessed portion 13 respectively which is recessed toward the accommodating space 100. In the present embodiment, four recessed portions 13 are provided, and each recessed portion 13 is provided in the center of each side of the casing 10.
  • The hub 20 and the blades 30 extending from the periphery of the hub 20 are combined in the accommodating space 100. The interior of the hub 20 has a shaft 21 and a motor (not shown). The motor drives the shaft 21 of the hub 20 to rotate, which causes the blades 30 provided at the periphery of the hub 20 to rotate accordingly to thereby generate airflow.
  • Each of the blades 30 comprises a first surface 31 and a second surface 32 opposite to the first surface 31. Each of the blades 30 is provided on its surfaces with a plurality of polygonal dents 33. These polygonal dents 33 may be formed into any one shape selected from the group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon. Thus, two adjacent sides of the polygonal dent 33 form an angle. In the present embodiment, the first surface 31 and the second surface 32 of the blade 30 are provided with the polygonal dents 33. In practice, the polygonal dents 33 may be only provided on the first surface 31 or the second surface 32.
  • Please refer to FIGS. 4 and 5. FIG. 4 is a schematic view showing the airflow generated by the fan according to the present invention, and FIG. 5 is a schematic view showing the relationship between the blade and the airflow generated by the fan according to the present invention. When the fan 1 rotates, the recessed portions 13 are configured to facilitate more external air to be introduced into the intake side 11. When the airflow is exhausted from the exhaust side 12, the recessed portions 13 are configured to lower the exhaust resistance of the airflow.
  • The airflow A generated by the fan 1 forms a boundary layer B on the surface of each blade 30. On the other hand, when the airflow A passes through the periphery of each polygonal dent 31, the airflow A generates a turbulent flow T in the polygonal dent 33. Many turbulent flows T collect together to form an air film between the surface of the blade 30 and the boundary layer B. The air film can extend the distance of separating points S from the boundary layer B, so that the separating points S are formed outside the blade 30. With this arrangement, the generation of the turbulent flows can be prevented in the vicinity of the blades 30, whereby the noise and the frictional force caused by the turbulent flows can be reduced.
  • In the above structure, the turbulent flow T is often generated at the periphery of each polygonal dent 33. Further, when the speed of the airflow A increases, the turbulent flow A can be generated more easily. Thus, when the speed of the airflow A is larger, each of the polygonal dents 33 may be formed into a shape of fewer sides such as a triangle or quadrangle shape. Contrarily, when the speed of the airflow A is smaller, each of the polygonal dents 33 may be formed into a shape of more sides such as a hexagon or heptagon shape.
  • Please refer to FIG. 6, which shows the second embodiment of the present invention. The difference between the second embodiment and the first embodiment lies in that: the polygonal dents 33 a on the blade 30 a may be formed into at least two shapes selected from the group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon.
  • Although the present invention has been described with reference to the foregoing preferred embodiments, it will be understood that the invention is not limited to the details thereof Various equivalent variations and modifications can still occur to those skilled in this art in view of the teachings of the present invention. Thus, all such variations and equivalent modifications are also embraced within the scope of the invention as defined in the appended claims.

Claims (7)

1. A fan structure including a hub and a plurality of blades extending from the periphery of the hub, the airflow generated by the fan forming a boundary layer on the surface of each blade, characterized in that:
each of the blades is provided with a plurality of polygonal dents, a turbulent flow is generated in each dent when the airflow passes through the dent, and a plurality of the turbulent flows collect together to form an air film between the surface of blade and the boundary layer.
2. The fan structure according to claim 1, further including a casing, the casing being formed into a square frame and having an accommodating space, the hub and the blades being combined in the accommodating space.
3. The fan structure according to claim 2, wherein the periphery of the casing is formed with at least one recessed portion recessed toward the accommodating space.
4. The fan structure according to claim 1, wherein two adjacent sides of the polygonal dent form an angle.
5. The fan structure according to claim 1, wherein each of the polygonal dents is formed into any one shape selected from the group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon.
6. The fan structure according to claim 1, wherein each of the polygonal dents on the blades is formed into at least two shapes selected from the group constituting of triangle, quadrangle, pentagon, hexagon, heptagon and octagon.
7. The fan structure according to claim 1, wherein the blade includes a first surface and a second surface opposite to the first surface, the polygonal dents are provided on the first surface and the second surface.
US12/908,059 2010-10-20 2010-10-20 Fan structure Abandoned US20120100001A1 (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106015043A (en) * 2016-06-22 2016-10-12 柳州市瑞日信息科技有限公司 Display card fan
CN106838598A (en) * 2017-04-06 2017-06-13 吉林大学 A kind of bionical Anti-erosion surface texture
DE102019105190A1 (en) * 2019-02-28 2020-09-03 Ebm-Papst St. Georgen Gmbh & Co. Kg Axial fan with noise-reducing fan blades
CN113669299A (en) * 2020-05-15 2021-11-19 广东美的环境电器制造有限公司 Fan blade assembly and electric appliance
CN114046268A (en) * 2021-11-19 2022-02-15 杭州贝丰科技有限公司 Fan blade suitable for motor frame front axial flow fan

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2238749A (en) * 1939-01-30 1941-04-15 Clarence B Swift Fan blade
US4128363A (en) * 1975-04-30 1978-12-05 Kabushiki Kaisha Toyota Chuo Kenkyusho Axial flow fan
US4846629A (en) * 1986-05-19 1989-07-11 Usui Kokusai Sangyo Kabushiki Kaisha Blades for high speed propeller fan
US4859150A (en) * 1986-05-19 1989-08-22 Usui Kokusai Sangyo Kabushiki Kaisha Blades for low speed propeller fan
US6504274B2 (en) * 2001-01-04 2003-01-07 General Electric Company Generator stator cooling design with concavity surfaces
US20030202879A1 (en) * 2002-04-30 2003-10-30 Wen-Shi Huang Cooling fan
US6872048B2 (en) * 2001-11-26 2005-03-29 Lennox Industries, Inc. Fan with reduced noise generation
JP2008157113A (en) * 2006-12-25 2008-07-10 Daikin Ind Ltd Blower
US20100119364A1 (en) * 2006-09-29 2010-05-13 General Electric Company Stator - rotor assemblies having surface features for enhanced containment of gas flow, and related processes
US8596958B2 (en) * 2008-05-09 2013-12-03 Daikin Industries, Ltd. Cross-flow fan and air conditioner equipped with same

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2238749A (en) * 1939-01-30 1941-04-15 Clarence B Swift Fan blade
US4128363A (en) * 1975-04-30 1978-12-05 Kabushiki Kaisha Toyota Chuo Kenkyusho Axial flow fan
US4846629A (en) * 1986-05-19 1989-07-11 Usui Kokusai Sangyo Kabushiki Kaisha Blades for high speed propeller fan
US4859150A (en) * 1986-05-19 1989-08-22 Usui Kokusai Sangyo Kabushiki Kaisha Blades for low speed propeller fan
US6504274B2 (en) * 2001-01-04 2003-01-07 General Electric Company Generator stator cooling design with concavity surfaces
US6872048B2 (en) * 2001-11-26 2005-03-29 Lennox Industries, Inc. Fan with reduced noise generation
US20030202879A1 (en) * 2002-04-30 2003-10-30 Wen-Shi Huang Cooling fan
US20100322764A1 (en) * 2002-04-30 2010-12-23 Wen-Shi Huang Cooling fan
US20100119364A1 (en) * 2006-09-29 2010-05-13 General Electric Company Stator - rotor assemblies having surface features for enhanced containment of gas flow, and related processes
JP2008157113A (en) * 2006-12-25 2008-07-10 Daikin Ind Ltd Blower
US8596958B2 (en) * 2008-05-09 2013-12-03 Daikin Industries, Ltd. Cross-flow fan and air conditioner equipped with same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106015043A (en) * 2016-06-22 2016-10-12 柳州市瑞日信息科技有限公司 Display card fan
CN106838598A (en) * 2017-04-06 2017-06-13 吉林大学 A kind of bionical Anti-erosion surface texture
DE102019105190A1 (en) * 2019-02-28 2020-09-03 Ebm-Papst St. Georgen Gmbh & Co. Kg Axial fan with noise-reducing fan blades
US11391282B2 (en) 2019-02-28 2022-07-19 Ebm-Papst St. Georgen Gmbh & Co. Kg Axial ventilator having noise reducing fan wheel blades
CN113669299A (en) * 2020-05-15 2021-11-19 广东美的环境电器制造有限公司 Fan blade assembly and electric appliance
CN114046268A (en) * 2021-11-19 2022-02-15 杭州贝丰科技有限公司 Fan blade suitable for motor frame front axial flow fan

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Owner name: ZAWARD CORPORATION, TAIWAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:CHEN, CHENG-KANG;REEL/FRAME:025164/0047

Effective date: 20100903

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION