US20030123988A1 - Fan blades - Google Patents
Fan blades Download PDFInfo
- Publication number
- US20030123988A1 US20030123988A1 US10/160,785 US16078502A US2003123988A1 US 20030123988 A1 US20030123988 A1 US 20030123988A1 US 16078502 A US16078502 A US 16078502A US 2003123988 A1 US2003123988 A1 US 2003123988A1
- Authority
- US
- United States
- Prior art keywords
- blades
- fan blades
- present
- fan
- noise
- 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
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
Definitions
- the present invention relates to a set of fan blades, particularly to a set of fan blades delivering increased air pressure at reduced noise for better usability.
- a fan has blades 10 moving through air 20 .
- air 20 splits into an upper stream 21 and a lower stream 22 , which are combined again at a rear edge 12 of the blade 10 . Since the way from the front edge 11 to a rear edge 12 is longer for the upper stream 11 than for the lower stream 22 , the upper stream 11 flows faster than the lower stream 22 , according to Bernoulli's law generating under pressure on the upper side of the fan blade 10 and consequently a dynamic lift.
- FIG. 1 is a perspective view of the set of fan blades of the present invention.
- FIG. 2 is a top view of the set of fan blades of the present invention.
- FIG. 3 is a sectional view along line 3 - 3 of FIG. 2.
- FIG. 4 is diagram illustrating experimental data with regard to static pressure with respect to airflow rate for the present invention and two conventional fan blades respectively.
- FIG. 5 is a schematic illustration of air currents around a conventional fan blade.
- FIG. 6 is a perspective schematic illustration of vortices at a conventional set of fan blades.
- the present invention is a set of fan blades 30 comprising a plurality of blades 32 evenly distributed around a hub case 31 .
- Each of the blades 32 has an outer edge 321 from which a projection 322 extends away at an angle ⁇ . Since the projection 322 points upward, no vortices are generated at the outer edge 321 so that more effective operation at a lower noise is achieved.
- the present invention achieves the object of lower noise and more effective operation for better dissipation of heat.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A set of fan blades comprises a plurality of blades evenly distributed around a hub case, wherein each of the blades has an outer edge from which a projection extends away at an angle.
Description
- 1. Field of the Invention
- The present invention relates to a set of fan blades, particularly to a set of fan blades delivering increased air pressure at reduced noise for better usability.
- 2. Description of Related Art
- Producing fans is done with the object of high effectiveness at low noise. Crucial for this object is the design of fan blades, which accordingly is done with great care.
- As shown in FIGS. 5 and 6, a fan has
blades 10 moving throughair 20. At afront edge 11 of each of theblades 10,air 20 splits into anupper stream 21 and alower stream 22, which are combined again at arear edge 12 of theblade 10. Since the way from thefront edge 11 to arear edge 12 is longer for theupper stream 11 than for thelower stream 22, theupper stream 11 flows faster than thelower stream 22, according to Bernoulli's law generating under pressure on the upper side of thefan blade 10 and consequently a dynamic lift. - When the upper and
lower streams rear edge 12, different velocities thereof cause a mutual influence, with vortices developing. If each of thefan blades 10 had an unlimited length and an unlimited area, there would be no path from a region of relatively high pressure to a region of relatively low pressure, and direct flow of the upper andlower streams front edge 11 to therear edge 12 would result. Since, however, both the length and the area of each of theblades 10 are limited, thelower stream 22 flows upward to a region of relatively low pressure. Then, as shown in FIG. 6,vortices 23 are generated atouter edges 13. This leads to an increased resistance against the movement of theblades 10 and to a reduced dynamic lift so that the fan works less effective at higher noise. - It is the main object of the present invention to provide a set of fan blades having outer edges with projections, which prevent vortices from developing for more effective operation at lower noise.
- The present invention can be more fully understood by reference to the following description and accompanying drawings.
- FIG. 1 is a perspective view of the set of fan blades of the present invention.
- FIG. 2 is a top view of the set of fan blades of the present invention.
- FIG. 3 is a sectional view along line3-3 of FIG. 2.
- FIG. 4 is diagram illustrating experimental data with regard to static pressure with respect to airflow rate for the present invention and two conventional fan blades respectively.
- FIG. 5 is a schematic illustration of air currents around a conventional fan blade.
- FIG. 6 is a perspective schematic illustration of vortices at a conventional set of fan blades.
- As shown in FIGS.1 to 3, the present invention is a set of
fan blades 30 comprising a plurality ofblades 32 evenly distributed around ahub case 31. Each of theblades 32 has anouter edge 321 from which aprojection 322 extends away at an angle θ. Since theprojection 322 points upward, no vortices are generated at theouter edge 321 so that more effective operation at a lower noise is achieved. - The effect of the present invention has been verified in experiments, the results of which are shown in the following table and the chart shown in FIG. 4. Therein, the present invention is compared with two conventional designs. At the same rotational speed, the present invention attains higher static pressure and higher airflow rate while noise is lower.
Rotational Static Airflow speed pressure rate Noise (rpm) (mm-H2O) (CFM) (dBA) Present invention 3800 4.0125 32.9525 36.2 Conventional 1 3800 3.6525 31.9 37.4 Conventional 2 3800 3.241 23.1709 37.0 - As the above explanation shows, the present invention achieves the object of lower noise and more effective operation for better dissipation of heat.
- While the invention has been described with reference to a preferred embodiment thereof, it is to be understood that modifications or variations may be easily made without departing from the spirit of this invention which is defined by the appended claim.
Claims (1)
1. A set of fan blades, comprising a plurality of blades evenly distributed around a hub case, wherein each of the blades has an outer edge from which a projection extends away at an angle.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW090224133U TW585227U (en) | 2001-12-31 | 2001-12-31 | Improved structure for fan blade |
TW090224133 | 2001-12-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
US20030123988A1 true US20030123988A1 (en) | 2003-07-03 |
Family
ID=21688003
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/160,785 Abandoned US20030123988A1 (en) | 2001-12-31 | 2002-06-03 | Fan blades |
Country Status (3)
Country | Link |
---|---|
US (1) | US20030123988A1 (en) |
DE (1) | DE20208410U1 (en) |
TW (1) | TW585227U (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060200445A1 (en) * | 2005-03-03 | 2006-09-07 | Google, Inc. | Providing history and transaction volume information of a content source to users |
US20060257251A1 (en) * | 2005-05-10 | 2006-11-16 | Carlson Jeremy S | Rotary axial fan assembly |
US20070154309A1 (en) * | 2005-12-29 | 2007-07-05 | Minebea Co., Ltd. | Cooling fan with integral housing and impeller |
US20070237656A1 (en) * | 2006-04-11 | 2007-10-11 | Pipkorn Nicholas T | Rotary fan with encapsulated motor assembly |
US20080093860A1 (en) * | 2004-11-30 | 2008-04-24 | Masahiko Suzuki | Propeller And Horizontal-Axis Wind Turbine |
US20080253896A1 (en) * | 2007-04-13 | 2008-10-16 | Walls Gary C | High efficiency fan blades with airflow-directing baffle elements |
US7438522B2 (en) | 2003-04-19 | 2008-10-21 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Fan |
EP2199620A2 (en) | 2008-12-22 | 2010-06-23 | Sanyo Denki Co., Ltd. | Axial flow fan |
DE102010034604A1 (en) * | 2010-08-13 | 2012-02-16 | Ziehl-Abegg Ag | Impeller for a fan |
US20170257007A1 (en) * | 2014-09-08 | 2017-09-07 | Siemens Aktiengesellschaft | Generator for a power plant |
CN108087327A (en) * | 2017-12-12 | 2018-05-29 | 无锡市盛源汽车配件厂 | High strength reinforcement type Water-pump impeller of automobile |
US20180258947A1 (en) * | 2017-03-10 | 2018-09-13 | Nidec Corporation | Axial fan |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11965522B2 (en) | 2015-12-11 | 2024-04-23 | Delta Electronics, Inc. | Impeller |
USD804647S1 (en) | 2016-02-02 | 2017-12-05 | Delta Electronics, Inc. | Fan blade |
CN112459962B (en) * | 2020-11-23 | 2021-11-02 | 重庆交通大学绿色航空技术研究院 | Wind power blade with tip end plate |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4222710A (en) * | 1976-12-20 | 1980-09-16 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Axial flow fan having auxiliary blade |
US5193983A (en) * | 1991-08-05 | 1993-03-16 | Norm Pacific Automation Corp. | Axial-flow fan-blade with profiled guide fins |
US5445215A (en) * | 1992-12-22 | 1995-08-29 | Herbert; Edward | Fan assembly with heat sink |
US5564901A (en) * | 1993-12-14 | 1996-10-15 | The Moore Company | Low noise fan |
US6352408B1 (en) * | 2000-10-16 | 2002-03-05 | Robert B. Kilian | Slip inhibiting boat propeller |
US6375427B1 (en) * | 2000-04-14 | 2002-04-23 | Borgwarner Inc. | Engine cooling fan having supporting vanes |
-
2001
- 2001-12-31 TW TW090224133U patent/TW585227U/en not_active IP Right Cessation
-
2002
- 2002-05-31 DE DE20208410U patent/DE20208410U1/en not_active Expired - Lifetime
- 2002-06-03 US US10/160,785 patent/US20030123988A1/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4222710A (en) * | 1976-12-20 | 1980-09-16 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Axial flow fan having auxiliary blade |
US5193983A (en) * | 1991-08-05 | 1993-03-16 | Norm Pacific Automation Corp. | Axial-flow fan-blade with profiled guide fins |
US5445215A (en) * | 1992-12-22 | 1995-08-29 | Herbert; Edward | Fan assembly with heat sink |
US5564901A (en) * | 1993-12-14 | 1996-10-15 | The Moore Company | Low noise fan |
US6375427B1 (en) * | 2000-04-14 | 2002-04-23 | Borgwarner Inc. | Engine cooling fan having supporting vanes |
US6352408B1 (en) * | 2000-10-16 | 2002-03-05 | Robert B. Kilian | Slip inhibiting boat propeller |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7438522B2 (en) | 2003-04-19 | 2008-10-21 | Ebm-Papst St. Georgen Gmbh & Co. Kg | Fan |
US8128338B2 (en) * | 2004-11-30 | 2012-03-06 | Kabushiki Kaisha Bellsion | Propeller and horizontal-axis wind turbine |
US20080093860A1 (en) * | 2004-11-30 | 2008-04-24 | Masahiko Suzuki | Propeller And Horizontal-Axis Wind Turbine |
EP1832744B1 (en) * | 2004-11-30 | 2019-09-18 | NTN Corporation | Propeller and horizontal-shaft windmill |
US20060200445A1 (en) * | 2005-03-03 | 2006-09-07 | Google, Inc. | Providing history and transaction volume information of a content source to users |
US20060257251A1 (en) * | 2005-05-10 | 2006-11-16 | Carlson Jeremy S | Rotary axial fan assembly |
US7484925B2 (en) | 2005-05-10 | 2009-02-03 | Emp Advanced Development, Llc | Rotary axial fan assembly |
US20070154309A1 (en) * | 2005-12-29 | 2007-07-05 | Minebea Co., Ltd. | Cooling fan with integral housing and impeller |
US20070237656A1 (en) * | 2006-04-11 | 2007-10-11 | Pipkorn Nicholas T | Rotary fan with encapsulated motor assembly |
US20080253896A1 (en) * | 2007-04-13 | 2008-10-16 | Walls Gary C | High efficiency fan blades with airflow-directing baffle elements |
EP2199620A2 (en) | 2008-12-22 | 2010-06-23 | Sanyo Denki Co., Ltd. | Axial flow fan |
US8770943B2 (en) | 2008-12-22 | 2014-07-08 | Sanyo Denki Co., Ltd. | Axial flow fan |
US20100158677A1 (en) * | 2008-12-22 | 2010-06-24 | Sanyo Denki Co., Ltd. | Axial flow fan |
DE102010034604A1 (en) * | 2010-08-13 | 2012-02-16 | Ziehl-Abegg Ag | Impeller for a fan |
US8915717B2 (en) | 2010-08-13 | 2014-12-23 | Ziehl-Abegg Ag | Impeller wheel for a ventilator |
US20170257007A1 (en) * | 2014-09-08 | 2017-09-07 | Siemens Aktiengesellschaft | Generator for a power plant |
US20180258947A1 (en) * | 2017-03-10 | 2018-09-13 | Nidec Corporation | Axial fan |
CN108087327A (en) * | 2017-12-12 | 2018-05-29 | 无锡市盛源汽车配件厂 | High strength reinforcement type Water-pump impeller of automobile |
Also Published As
Publication number | Publication date |
---|---|
DE20208410U1 (en) | 2002-10-02 |
TW585227U (en) | 2004-04-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |