US20150132121A1 - Fan - Google Patents
Fan Download PDFInfo
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/002—Axial flow fans
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/403—Casings; Connections of working fluid especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/601—Mounting; Assembling; Disassembling specially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
- F04D29/685—Inducing 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 .
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
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
- 1. Technical Field
- The present disclosure relates to a fan.
- 2. Description of Related Art
-
FIG. 1 shows atypical fan 80 comprising aframe 81 and animpeller 83. Acircular hole 85 is defined in a middle of theframe 81, for receiving theimpeller 83. An inner surface of theframe 81 bounding thehole 85 is smooth. When theimpeller 83 is rotated, air is drawn into thehole 85 from a side of thefan 80, and a considerable amount of air is radially flown out of thehole 85 from an opposite side of thefan 80. Thereby, thefan 80 may not effectively dissipate heat for some devices which need heat dissipation by more concentrated air. - 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 ofFIG. 2 in use. - 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 afan 10 comprising aframe 12 and animpeller 14. - The
frame 12 comprises twoopposite sidewalls 121. Ahole 123 having an elliptic cross section is defined in a middle of theframe 12, extending through thesidewalls 121. Theimpeller 14 is mounted in thehole 123. A plurality ofcircumferential grooves 125 is defined in aninner wall 124 of theframe 12 bounding thehole 123, such that twocircumferential protrusions 126 are formed on theinner wall 124 adjoining opposite sides of eachgroove 125. In the embodiment, a cross section of eachgroove 125 and eachprotrusion 126 is arc-shaped, such that thegrooves 125 and theprotrusions 126 cooperate to form a wave-shaped surface on theinner wall 124 of theframe 12. - In use, the
impeller 14 is rotated, airflow is drawn into thehole 123 from an end of thehole 123, and is blown out of thehole 123 from an opposite end of thehole 123. Because thespaced grooves 125 andprotrusions 126 are formed on theinner wall 124 bounding thehole 123, the airflow through thehole 123 is pressurized by thegrooves 125 and theprotrusions 126, and concentrates when the airflow is blown out of thehole 123. Thereby, thefan 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 onecircumferential groove 125 and form only onecircumferential protrusion 126 adjoining thegroove 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)
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.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW102141539A TW201518607A (en) | 2013-11-14 | 2013-11-14 | Fan |
TW102141539 | 2013-11-14 |
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)
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)
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 |
-
2013
- 2013-11-14 TW TW102141539A patent/TW201518607A/en unknown
- 2013-12-31 US US14/144,585 patent/US20150132121A1/en not_active Abandoned
Patent Citations (28)
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 (4)
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 |
US12055150B2 (en) | 2021-05-12 | 2024-08-06 | Sanyo Denki Co., Ltd. | Reversible fan |
Also Published As
Publication number | Publication date |
---|---|
TW201518607A (en) | 2015-05-16 |
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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 |