EP1211426B1 - Boîtier d'un ventilateur, en particulier pour ventilateur axial - Google Patents
Boîtier d'un ventilateur, en particulier pour ventilateur axial Download PDFInfo
- Publication number
- EP1211426B1 EP1211426B1 EP01127602A EP01127602A EP1211426B1 EP 1211426 B1 EP1211426 B1 EP 1211426B1 EP 01127602 A EP01127602 A EP 01127602A EP 01127602 A EP01127602 A EP 01127602A EP 1211426 B1 EP1211426 B1 EP 1211426B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- contour
- fan
- discharge opening
- fan housing
- contour elements
- 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.)
- Expired - Lifetime
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
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/545—Ducts
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
Definitions
- the present invention relates to a fan housing having a flow passage with a one-sided suction port and a discharge opening on the other side, as defined in the preamble of claim 1.
- a fan housing is known e.g. from US-A-3 531 221.
- Fans are often used for applications in which it depends on a very uniform, especially over the entire flow cross-section away as laminar as possible air flow.
- axial fans are used side by side, particularly in a row arrangement, in order to apply a stream of air to large sheets of paper after printing, so that these sheets can be deposited more quickly on a piece of paper.
- the highest possible fluidic surface pressure is to be caused, which acts on the sheet, thereby supporting the gravitational force in the storage of the sheets and thus pushes out the obstructive and last filed sheet on the underside of the sheet and the tray hindering air.
- the filing speed and filing quality have a direct influence on the profitability of a printing press, since they decisively determine the throughput speed of the printing press. An improvement of the filing and an increase in the filing speed would therefore result in a direct increase in machine economy.
- the present invention has for its object to improve a fan housing of the type described above, generic type with respect to the flow characteristics of the delivered air flow, in particular so that a with The fan housing according to the invention fan is particularly suitable for use in printing machines described above.
- the invention is based on the recognition that, naturally, a free jet forms behind each fan, which mixes only after a certain distance with the ambient air and / or with the free jet of adjacent fans.
- These free jets have the property that they have a relatively low degree of turbulence in the center.
- the blown out, moving air mixes with the attracted, resting air in a shear layer (entrainment effect).
- this shear layer exist almost exclusively large-scale, low-frequency vortex forms. These are long-lived due to their high energy content.
- this has the consequence that is stimulated by the vortex shedding of the sheet to oscillate in its natural frequency. Under certain circumstances, even the natural frequency of the arc correlates with the vortex shedding frequency. This mechanism prevents an increase in the filing speed and can continue to lead to temporary disturbances of the filing process.
- the drawing figures show an axial fan housing 1 with an axial flow passage 2 with a one-sided suction port 4 and an opposite one Blow-out opening 6.
- the suction opening 4 and the blow-off opening 6 each have a circular outer contour. This results in a substantially annular configuration of the axial fan housing 1 (so-called wall ring).
- centric holding means 8 are arranged for a motor / Lüfterradü, not shown, wherein the holding means 8 are connected via spoke-like connecting elements 10 with the outer housing ring.
- an annular or circular disk-shaped flow cross section is thus formed.
- the contour elements 14 are fixed with a base (in the illustrated case a triangle base) at the opening edge of the exhaust opening 6 or in the surrounding area of the housing end face, while with its opposite tip or edge (as shown in its triangular Tip) on the one hand axially in the flow direction and on the other hand obliquely radially inwardly or outwardly protrude. 1 and 2, all contour elements 14 are aligned obliquely axially and radially inwardly, namely at an angle ⁇ 1 to the radial plane (plane of the exhaust opening 6 and the housing end face), starting from the peripheral region of the exhaust opening. 6
- part of the contour elements 14 are aligned at an angle ⁇ 2 obliquely axially and radially outwards.
- ⁇ 1 obliquely radially inwardly projecting contour elements
- ⁇ 2 obliquely radially outwardly projecting contour elements 14
- angles ⁇ 1 and ⁇ 2 may be equal or different.
- the respective angle ⁇ 1 or ⁇ 2 lies in the range between 0 ° and 90 ° and can - as well as the number, size and contour shape of the contour elements 14 - be adapted and adjusted to the particular application, with a combination of contour elements may be provided may differ from each other in shape and / or size and / or angular orientation.
- FIGS. 1 and 2 exemplify a comparison of the operation of a non-inventive embodiment (Fig. 5) without Abströmkonturstoff 12 and the equally not-inventive embodiment of FIGS. 1 and 2 (Fig. 6).
- Fig. 5 it is illustrated that in a conventional "normal" axial fan, an outer shear layer 16a is formed, which encloses an inner, undisturbed flow 18.
- This outer shear layer 16a has a relatively large radially measured thickness d 1 and contains large-scale vortices and a large proportion of low-frequency excitation components. This leads to a non-stabilized air jet.
- Fig. 6 it is clear from Fig. 6 that the embodiment of Figs.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Claims (3)
- Boîtier de ventilateur (1) avec un passage d'écoulement (2) comprenant une ouverture d'aspiration (4) et une ouverture de soufflage (6), dans lequel, au niveau de l'ouverture de soufflage (6), des moyens de contour de flux de sortie (12) entourant sa section d'écoulement sont formés de manière à au moins réduire une formation de turbulences dans une couche de cisaillement (16) qui entoure le courant d'air proprement dit (18) résultant du fonctionnement du ventilateur, qui se forme entre le courant d'air (18) et l'air environnant, caractérisé par le fait
que les moyens de contour de flux de sortie (12) sont constitués d'éléments de contour (14) individuels, répartis sur la circonférence de l'ouverture de soufflage (6), partant du bord de l'ouverture de soufflage (6) et dépassant au moins partiellement dans la zone de la couche de cisaillement naissante (16b),
qu'une partie des éléments de contour (14) est orientée axialement en biais et radialement vers l'extérieur, et
qu'il est prévu en direction circonférentielle alternativement des éléments de contour (14) radialement en biais dépassant vers l'intérieur et des éléments de contour (14) radialement en biais dépassant vers l'extérieur. - Boîtier de ventilateur selon la revendication 1,
caractérisé par une réalisation sous forme de boîtier de ventilateur axial (1), dans lequel l'ouverture d'aspiration (4) et l'ouverture de soufflage (6) présentent chacune un contour extérieur circulaire et sont disposées axialement en face l'une de l'autre et dans lequel il est prévu en particulier à l'intérieur du passage d'écoulement (2) des moyens de fixation (8) pour un ensemble moteur-roue de ventilateur. - Boîtier de ventilateur selon la revendication 1,
caractérisé par le fait que les éléments de contour (14) sont réalisés sous la forme de pointes de couronne ayant un contour globalement triangulaire.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE20020512 | 2000-12-01 | ||
DE20020512U | 2000-12-01 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1211426A2 EP1211426A2 (fr) | 2002-06-05 |
EP1211426A3 EP1211426A3 (fr) | 2003-07-23 |
EP1211426B1 true EP1211426B1 (fr) | 2006-06-07 |
Family
ID=7949615
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01127602A Expired - Lifetime EP1211426B1 (fr) | 2000-12-01 | 2001-11-20 | Boîtier d'un ventilateur, en particulier pour ventilateur axial |
Country Status (4)
Country | Link |
---|---|
US (1) | US6659719B2 (fr) |
EP (1) | EP1211426B1 (fr) |
AT (1) | ATE329157T1 (fr) |
DE (2) | DE20118939U1 (fr) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TWI290978B (en) * | 2005-11-18 | 2007-12-11 | Delta Electronics Inc | Fan and fan housing with toothed-type connecting elements |
US20080273961A1 (en) | 2007-03-05 | 2008-11-06 | Rosenkrans William E | Flutter sensing and control system for a gas turbine engine |
US20110027067A1 (en) * | 2007-03-23 | 2011-02-03 | Flodesign Wind Turbine Corporation | Coated shrouded wind turbine |
US8622688B2 (en) * | 2007-03-23 | 2014-01-07 | Flodesign Wind Turbine Corp. | Fluid turbine |
US20110014038A1 (en) * | 2007-03-23 | 2011-01-20 | Flodesign Wind Turbine Corporation | Wind turbine with skeleton-and-skin structure |
US8657572B2 (en) | 2007-03-23 | 2014-02-25 | Flodesign Wind Turbine Corp. | Nacelle configurations for a shrouded wind turbine |
US8021100B2 (en) * | 2007-03-23 | 2011-09-20 | Flodesign Wind Turbine Corporation | Wind turbine with mixers and ejectors |
US20110085901A1 (en) * | 2007-03-23 | 2011-04-14 | Presz Jr Walter M | Shrouded wind turbine with scalloped lobes |
US20100314885A1 (en) * | 2007-03-23 | 2010-12-16 | Flodesign Wind Turbine Corporation | Shrouded wind turbine with rim generator and halbach array |
US20100270802A1 (en) * | 2007-03-23 | 2010-10-28 | Flodesign Wind Turbine Corporation | Wind turbine |
US20110008164A1 (en) * | 2007-03-23 | 2011-01-13 | Flodesign Wind Turbine Corporation | Wind turbine |
US20110002781A1 (en) * | 2007-03-23 | 2011-01-06 | Flodesign Wind Turbine Corporation | Wind turbine with pressure profile and method of making same |
US20110135458A1 (en) * | 2007-03-23 | 2011-06-09 | Presz Jr Walter M | Fluid turbine with shroud having segmented lobes |
US8714923B2 (en) * | 2007-03-23 | 2014-05-06 | Ogin, Inc. | Fluid turbine |
US20100316493A1 (en) * | 2007-03-23 | 2010-12-16 | Flodesign Wind Turbine Corporation | Turbine with mixers and ejectors |
CA2745323A1 (fr) * | 2008-12-02 | 2010-06-10 | Flodesign Wind Turbine Corp. | Interface a supercondensateur dans une generatrice annulaire d'eolienne |
DE102009015104A1 (de) * | 2009-03-31 | 2010-10-14 | Behr Gmbh & Co. Kg | Axiallüfter, insbesondere für ein Kraftfahrzeug |
CA2787948A1 (fr) * | 2010-02-11 | 2011-08-18 | Flodesign Wind Turbine Corp. | Turbine a fluide |
US9157455B2 (en) * | 2011-05-25 | 2015-10-13 | Robert Bosch Gmbh | Airflow assembly having improved acoustical performance |
JP6551173B2 (ja) * | 2015-11-09 | 2019-07-31 | 株式会社デンソー | 遠心送風機 |
US20170211589A1 (en) * | 2016-01-22 | 2017-07-27 | Minebea Co., Ltd. | Axial Fan |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1752427A (en) * | 1923-06-09 | 1930-04-01 | Elisha N Fales | Device for improving the aerodynamic efficiency of an exhauster fan |
FR1576254A (fr) * | 1967-08-23 | 1969-07-25 | ||
FR2358550A1 (fr) * | 1976-07-16 | 1978-02-10 | Milloux Maurice | Dispositif pour elever le rendement d'une helice |
JPS53115912A (en) * | 1977-03-18 | 1978-10-09 | Matsushita Electric Ind Co Ltd | Electric blower |
US5393197A (en) * | 1993-11-09 | 1995-02-28 | Lemont Aircraft Corporation | Propulsive thrust ring system |
FR2736400B1 (fr) * | 1995-07-05 | 1997-09-19 | Gec Alsthom Transport Sa | Motoventilateur de refroidissement |
GB9925193D0 (en) * | 1999-10-26 | 1999-12-22 | Rolls Royce Plc | Gas turbine engine exhaust nozzle |
US6502383B1 (en) * | 2000-08-31 | 2003-01-07 | General Electric Company | Stub airfoil exhaust nozzle |
-
2001
- 2001-11-20 DE DE20118939U patent/DE20118939U1/de not_active Expired - Lifetime
- 2001-11-20 AT AT01127602T patent/ATE329157T1/de not_active IP Right Cessation
- 2001-11-20 DE DE50110023T patent/DE50110023D1/de not_active Expired - Lifetime
- 2001-11-20 EP EP01127602A patent/EP1211426B1/fr not_active Expired - Lifetime
- 2001-11-28 US US09/995,932 patent/US6659719B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE20118939U1 (de) | 2002-04-25 |
EP1211426A2 (fr) | 2002-06-05 |
US20020067988A1 (en) | 2002-06-06 |
ATE329157T1 (de) | 2006-06-15 |
US6659719B2 (en) | 2003-12-09 |
EP1211426A3 (fr) | 2003-07-23 |
DE50110023D1 (de) | 2006-07-20 |
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