US20150132121A1 - Fan - Google Patents

Fan Download PDF

Info

Publication number
US20150132121A1
US20150132121A1 US14/144,585 US201314144585A US2015132121A1 US 20150132121 A1 US20150132121 A1 US 20150132121A1 US 201314144585 A US201314144585 A US 201314144585A US 2015132121 A1 US2015132121 A1 US 2015132121A1
Authority
US
United States
Prior art keywords
hole
frame
fan
groove
impeller
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
US14/144,585
Inventor
Shu-Ying Yuan
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.)
Hon Hai Precision Industry Co Ltd
Original Assignee
Hon Hai Precision Industry Co Ltd
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 Hon Hai Precision Industry Co Ltd filed Critical Hon Hai Precision Industry Co Ltd
Assigned to HON HAI PRECISION INDUSTRY CO., LTD. reassignment HON HAI PRECISION INDUSTRY CO., LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: YUAN, Shu-ying
Publication of US20150132121A1 publication Critical patent/US20150132121A1/en
Abandoned 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
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/403Casings; Connections of working fluid especially adapted for elastic fluid 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/522Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • F04D29/526Details of the casing section radially opposing blade tips
    • 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
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/601Mounting; Assembling; Disassembling specially adapted for elastic fluid 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
    • F04D29/68Combating 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
    • F04D29/685Inducing localised fluid recirculation in the stator-rotor interface

Definitions

  • the present disclosure relates to a fan.
  • FIG. 1 shows a typical fan 80 comprising a frame 81 and an impeller 83 .
  • a circular hole 85 is defined in a middle of the frame 81 , for receiving the impeller 83 .
  • An inner surface of the frame 81 bounding the hole 85 is smooth.
  • FIG. 1 is a plan, sketch view of a conventional fan in use.
  • FIG. 2 is an assembled, isometric view of an embodiment of a fan.
  • FIG. 3 is a plan, sketch view of the fan of FIG. 2 in use.
  • FIGS. 2 and 3 show an exemplary embodiment of a fan 10 comprising a frame 12 and an impeller 14 .
  • the frame 12 comprises two opposite sidewalls 121 .
  • a hole 123 having an elliptic cross section is defined in a middle of the frame 12 , extending through the sidewalls 121 .
  • the impeller 14 is mounted in the hole 123 .
  • a plurality of circumferential grooves 125 is defined in an inner wall 124 of the frame 12 bounding the hole 123 , such that two circumferential protrusions 126 are formed on the inner wall 124 adjoining opposite sides of each groove 125 .
  • a cross section of each groove 125 and each protrusion 126 is arc-shaped, such that the grooves 125 and the protrusions 126 cooperate to form a wave-shaped surface on the inner wall 124 of the frame 12 .
  • the impeller 14 In use, the impeller 14 is rotated, airflow is drawn into the hole 123 from an end of the hole 123 , and is blown out of the hole 123 from an opposite end of the hole 123 . Because the spaced grooves 125 and protrusions 126 are formed on the inner wall 124 bounding the hole 123 , the airflow through the hole 123 is pressurized by the grooves 125 and the protrusions 126 , and concentrates when the airflow is blown out of the hole 123 . Thereby, the fan 10 can provide stronger, concentrated airflow.
  • a cross section of the hole 123 is elliptic, which can reduce wind noise.
  • the inner wall 124 can define only one circumferential groove 125 and form only one circumferential protrusion 126 adjoining the groove 125 .

Abstract

A fan includes a frame and an impeller. The frame defines a hole in a middle of the frame. An inner wall of the frame bounding the hole defines a circumferential groove and forms a circumferential protrusion adjoining the groove. The impeller is received in the hole of the frame. When the impeller is rotated, airflow through the hole is pressurized by the groove and the protrusion, and concentrates when the airflow is blown out of the hole.

Description

    BACKGROUND
  • 1. Technical Field
  • The present disclosure relates to a fan.
  • 2. Description of Related Art
  • FIG. 1 shows a typical fan 80 comprising a frame 81 and an impeller 83. A circular hole 85 is defined in a middle of the frame 81, for receiving the impeller 83. An inner surface of the frame 81 bounding the hole 85 is smooth. When the impeller 83 is rotated, air is drawn into the hole 85 from a side of the fan 80, and a considerable amount of air is radially flown out of the hole 85 from an opposite side of the fan 80. Thereby, the fan 80 may not effectively dissipate heat for some devices which need heat dissipation by more concentrated air.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Many aspects of the present embodiments can be better understood with reference to the following drawings. The components in the drawings are not necessarily drawn to scale, the emphasis instead being placed upon clearly illustrating the principles of the present embodiments. Moreover, in the drawings, all the views are schematic, and like reference numerals designate corresponding parts throughout the several views.
  • FIG. 1 is a plan, sketch view of a conventional fan in use.
  • FIG. 2 is an assembled, isometric view of an embodiment of a fan.
  • FIG. 3 is a plan, sketch view of the fan of FIG. 2 in use.
  • DETAILED DESCRIPTION
  • The disclosure, including the accompanying drawings, is illustrated by way of example and not by way of limitation. It should be noted that references to “an” or “one” embodiment in this disclosure are not necessarily to the same embodiment, and such references can mean “at least one.”
  • FIGS. 2 and 3 show an exemplary embodiment of a fan 10 comprising a frame 12 and an impeller 14.
  • The frame 12 comprises two opposite sidewalls 121. A hole 123 having an elliptic cross section is defined in a middle of the frame 12, extending through the sidewalls 121. The impeller 14 is mounted in the hole 123. A plurality of circumferential grooves 125 is defined in an inner wall 124 of the frame 12 bounding the hole 123, such that two circumferential protrusions 126 are formed on the inner wall 124 adjoining opposite sides of each groove 125. In the embodiment, a cross section of each groove 125 and each protrusion 126 is arc-shaped, such that the grooves 125 and the protrusions 126 cooperate to form a wave-shaped surface on the inner wall 124 of the frame 12.
  • In use, the impeller 14 is rotated, airflow is drawn into the hole 123 from an end of the hole 123, and is blown out of the hole 123 from an opposite end of the hole 123. Because the spaced grooves 125 and protrusions 126 are formed on the inner wall 124 bounding the hole 123, the airflow through the hole 123 is pressurized by the grooves 125 and the protrusions 126, and concentrates when the airflow is blown out of the hole 123. Thereby, the fan 10 can provide stronger, concentrated airflow.
  • In the embodiment, a cross section of the hole 123 is elliptic, which can reduce wind noise.
  • In other embodiments, the inner wall 124 can define only one circumferential groove 125 and form only one circumferential protrusion 126 adjoining the groove 125.
  • Even though numerous characteristics and advantages of the embodiments have been set forth in the foregoing description, together with details of the structure and the functions of the embodiments, the disclosure is illustrative only, and changes may be made in details, especially in the matters of shape, size, and arrangement of parts within the principles of the embodiments to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed.

Claims (8)

What is claimed is:
1. A fan, comprising:
a frame defining a hole in a middle of the frame, an inner wall of the frame bounding the hole defining a circumferential groove and forming a circumferential protrusion adjoining the groove; and
an impeller received in the hole of the frame, wherein when the impeller is rotated, airflow through the hole is pressurized by the groove and the protrusion, and concentrates when the airflow is blown out of the hole.
2. The fan of claim 1, wherein the groove and the protrusion cooperate to form a wave-shaped surface on the inner wall of the frame.
3. The fan of claim 2, wherein a cross section of each of the groove and the protrusion is arc-shaped.
4. The fan of claim 1, wherein a cross section of the hole is elliptic.
5. A fan, comprising:
a frame defining a hole in a middle of the frame, an inner wall of the frame bounding the hole defining a plurality of circumferential grooves and forming two circumferential protrusions adjoining opposite sides of each groove; and
an impeller received in the hole of the frame, wherein when the impeller is rotated, airflow through the hole is pressurized by the plurality of grooves and protrusions, and concentrates when the airflow is blown out of the hole.
6. The fan of claim 5, wherein the plurality of grooves and protrusions cooperate to form a wave-shaped surface on the inner wall of the frame.
7. The fan of claim 6, wherein a cross section of each groove and each protrusion is arc-shaped.
8. The fan of claim 5, wherein a cross section of the hole is elliptic.
US14/144,585 2013-11-14 2013-12-31 Fan Abandoned US20150132121A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TW102141539 2013-11-14
TW102141539A TW201518607A (en) 2013-11-14 2013-11-14 Fan

Publications (1)

Publication Number Publication Date
US20150132121A1 true US20150132121A1 (en) 2015-05-14

Family

ID=53043945

Family Applications (1)

Application Number Title Priority Date Filing Date
US14/144,585 Abandoned US20150132121A1 (en) 2013-11-14 2013-12-31 Fan

Country Status (2)

Country Link
US (1) US20150132121A1 (en)
TW (1) TW201518607A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3301306A1 (en) * 2016-09-29 2018-04-04 Sanyo Denki Co., Ltd. Blast fan
EP4089286A1 (en) * 2021-05-12 2022-11-16 Sanyo Denki Co., Ltd. Reversible fan

Citations (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684723A (en) * 1950-09-07 1954-07-27 Guy S Faber Propeller-type fan blade
US3261228A (en) * 1964-04-02 1966-07-19 United Aircraft Corp Disk fragment energy absorption and containment means
US3893787A (en) * 1974-03-14 1975-07-08 United Aircraft Corp Centrifugal compressor boundary layer control
US3934410A (en) * 1972-09-15 1976-01-27 The United States Of America As Represented By The Secretary Of The Navy Quiet shrouded circulation control propeller
US3937189A (en) * 1974-01-28 1976-02-10 International Harvester Company Fan shroud exit structure
US4061188A (en) * 1975-01-24 1977-12-06 International Harvester Company Fan shroud structure
US4063848A (en) * 1976-03-24 1977-12-20 Caterpillar Tractor Co. Centrifugal compressor vaneless space casing treatment
US4086022A (en) * 1975-09-25 1978-04-25 Rolls-Royce Limited Gas turbine engine with improved compressor casing for permitting higher air flow and pressure ratios before surge
US4239452A (en) * 1978-06-26 1980-12-16 United Technologies Corporation Blade tip shroud for a compression stage of a gas turbine engine
US4311431A (en) * 1978-11-08 1982-01-19 Teledyne Industries, Inc. Turbine engine with shroud cooling means
US5137419A (en) * 1984-06-19 1992-08-11 Rolls-Royce Plc Axial flow compressor surge margin improvement
US5197854A (en) * 1991-09-05 1993-03-30 Industrial Design Laboratories, Inc. Axial flow fan
US5342173A (en) * 1991-11-07 1994-08-30 Ecia-Equipements Et Composants Pour L'industrie Automobile Cowl for fan and its application to a vehicle motorized fan unit
US5707206A (en) * 1995-07-18 1998-01-13 Ebara Corporation Turbomachine
US5884589A (en) * 1995-04-10 1999-03-23 Hitachi Construction Machinery Co., Ltd. Cooling apparatus for heat exchanger
US6254343B1 (en) * 1999-12-06 2001-07-03 Motorola, Inc. Low-noise cooling fan for electronic components and method of making the same
US6375416B1 (en) * 1993-07-15 2002-04-23 Kevin J. Farrell Technique for reducing acoustic radiation in turbomachinery
US6450760B1 (en) * 1999-11-22 2002-09-17 Komatsu Ltd. Fan device
US6514039B1 (en) * 1999-11-25 2003-02-04 Rolls-Royce Plc Processing tip treatment bars in a gas turbine engine
US6863496B2 (en) * 2002-02-27 2005-03-08 Halla Climate Control Corporation Fan and shroud assembly
US6866475B2 (en) * 2002-06-25 2005-03-15 John F. Rivers Fan assembly for use in powered airborne vehicles
US7110255B2 (en) * 2003-04-11 2006-09-19 Delta Electronics, Inc. Heat-dissipating device and a housing thereof
US20070147989A1 (en) * 2005-12-22 2007-06-28 Rolls-Royce Plc Fan or compressor casing
US7416386B2 (en) * 2005-09-21 2008-08-26 Delta Electronics, Inc. Heat dissipation apparatus
US7481615B2 (en) * 2005-03-26 2009-01-27 Halla Climate Control Corp. Fan and shroud assembly
US7645121B2 (en) * 2006-01-12 2010-01-12 Rolls Royce Plc Blade and rotor arrangement
US20100040457A1 (en) * 2008-08-15 2010-02-18 Chih-Chun Tsen Light-emitting fan
US7766614B2 (en) * 2006-03-10 2010-08-03 Rolls-Royce Plc Compressor casing

Patent Citations (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684723A (en) * 1950-09-07 1954-07-27 Guy S Faber Propeller-type fan blade
US3261228A (en) * 1964-04-02 1966-07-19 United Aircraft Corp Disk fragment energy absorption and containment means
US3934410A (en) * 1972-09-15 1976-01-27 The United States Of America As Represented By The Secretary Of The Navy Quiet shrouded circulation control propeller
US3937189A (en) * 1974-01-28 1976-02-10 International Harvester Company Fan shroud exit structure
US3893787A (en) * 1974-03-14 1975-07-08 United Aircraft Corp Centrifugal compressor boundary layer control
US4061188A (en) * 1975-01-24 1977-12-06 International Harvester Company Fan shroud structure
US4086022A (en) * 1975-09-25 1978-04-25 Rolls-Royce Limited Gas turbine engine with improved compressor casing for permitting higher air flow and pressure ratios before surge
US4063848A (en) * 1976-03-24 1977-12-20 Caterpillar Tractor Co. Centrifugal compressor vaneless space casing treatment
US4239452A (en) * 1978-06-26 1980-12-16 United Technologies Corporation Blade tip shroud for a compression stage of a gas turbine engine
US4311431A (en) * 1978-11-08 1982-01-19 Teledyne Industries, Inc. Turbine engine with shroud cooling means
US5137419A (en) * 1984-06-19 1992-08-11 Rolls-Royce Plc Axial flow compressor surge margin improvement
US5197854A (en) * 1991-09-05 1993-03-30 Industrial Design Laboratories, Inc. Axial flow fan
US5342173A (en) * 1991-11-07 1994-08-30 Ecia-Equipements Et Composants Pour L'industrie Automobile Cowl for fan and its application to a vehicle motorized fan unit
US6375416B1 (en) * 1993-07-15 2002-04-23 Kevin J. Farrell Technique for reducing acoustic radiation in turbomachinery
US5884589A (en) * 1995-04-10 1999-03-23 Hitachi Construction Machinery Co., Ltd. Cooling apparatus for heat exchanger
US5707206A (en) * 1995-07-18 1998-01-13 Ebara Corporation Turbomachine
US6450760B1 (en) * 1999-11-22 2002-09-17 Komatsu Ltd. Fan device
US6514039B1 (en) * 1999-11-25 2003-02-04 Rolls-Royce Plc Processing tip treatment bars in a gas turbine engine
US6254343B1 (en) * 1999-12-06 2001-07-03 Motorola, Inc. Low-noise cooling fan for electronic components and method of making the same
US6863496B2 (en) * 2002-02-27 2005-03-08 Halla Climate Control Corporation Fan and shroud assembly
US6866475B2 (en) * 2002-06-25 2005-03-15 John F. Rivers Fan assembly for use in powered airborne vehicles
US7110255B2 (en) * 2003-04-11 2006-09-19 Delta Electronics, Inc. Heat-dissipating device and a housing thereof
US7481615B2 (en) * 2005-03-26 2009-01-27 Halla Climate Control Corp. Fan and shroud assembly
US7416386B2 (en) * 2005-09-21 2008-08-26 Delta Electronics, Inc. Heat dissipation apparatus
US20070147989A1 (en) * 2005-12-22 2007-06-28 Rolls-Royce Plc Fan or compressor casing
US7645121B2 (en) * 2006-01-12 2010-01-12 Rolls Royce Plc Blade and rotor arrangement
US7766614B2 (en) * 2006-03-10 2010-08-03 Rolls-Royce Plc Compressor casing
US20100040457A1 (en) * 2008-08-15 2010-02-18 Chih-Chun Tsen Light-emitting fan

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3301306A1 (en) * 2016-09-29 2018-04-04 Sanyo Denki Co., Ltd. Blast fan
US10837345B2 (en) 2016-09-29 2020-11-17 Sanyo Denki Co., Ltd. Blast fan
EP4089286A1 (en) * 2021-05-12 2022-11-16 Sanyo Denki Co., Ltd. Reversible fan

Also Published As

Publication number Publication date
TW201518607A (en) 2015-05-16

Similar Documents

Publication Publication Date Title
US9897094B2 (en) Axial flow fan
US8570740B2 (en) Electronic device with expansion cards
US8240989B2 (en) Fan
US20190120243A1 (en) Fan impeller structure and cooling fan thereof
US20130170995A1 (en) Axial flow fan blade structure and axial flow fan thereof
US20150132121A1 (en) Fan
US20150167691A1 (en) Fan assembly
US9398727B2 (en) Server assembly
US10502226B2 (en) Centrifugal blower
US20150146363A1 (en) Server
US20200217593A1 (en) Flat-plate heat pipe structure
US9267545B2 (en) Bearing retaining structure
CN105604972B (en) Combination of fans
US9086861B2 (en) Heat dissipation system with air duct
CN105090103A (en) Fan blade structure and cooling fan with same
US10024334B2 (en) Centrifugal fan and fan frame thereof
US20120026687A1 (en) Housing and electronic device using the same
US9265183B2 (en) Mounting system for hard disk drive
US8936433B2 (en) Anti-relief fan frame body structure
US20150044042A1 (en) Fan assembly
US20160290365A1 (en) Fan and fan assembly
US20130233426A1 (en) Air duct
US20150159673A1 (en) Fan assembly
US20130216404A1 (en) Bladeless fan structure
US20130146269A1 (en) Heat sink

Legal Events

Date Code Title Description
AS Assignment

Owner name: HON HAI PRECISION INDUSTRY CO., LTD., TAIWAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:YUAN, SHU-YING;REEL/FRAME:033568/0591

Effective date: 20131231

STCB Information on status: application discontinuation

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