US1473066A - Fan for automobile radiators or the like - Google Patents
Fan for automobile radiators or the like Download PDFInfo
- Publication number
- US1473066A US1473066A US545170A US54517022A US1473066A US 1473066 A US1473066 A US 1473066A US 545170 A US545170 A US 545170A US 54517022 A US54517022 A US 54517022A US 1473066 A US1473066 A US 1473066A
- Authority
- US
- United States
- Prior art keywords
- fan
- face
- blades
- trailing
- leading
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P5/00—Pumping cooling-air or liquid coolants
- F01P5/02—Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
-
- 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
Definitions
- This invention relates to improvements 1n the construction of fans of the so-called Aaropeller or screw type wherein the air or uid passing through the fan, flows along lines which are approximately parallel to the axis rather than radial or tangential as may be true in a centrifugal fan.
- the object of the invention consists in so shaping the vanes or blades as to induce, to a greater degree, the production of cavitation or negative pressure over the trailing face of the blades and so varying this negative pressure that it is greater near the trailing edge of the blade than at the leading edge.
- it is the object of this invention to produce a negative pressure over the trailing face which will promote the flow of air or fluid to and through the fan and which will operate in addition to the positive urging force or action which takes place over the leading face of the blade, thereby greatly increasing the capacity of the fan.
- My preferred means for producing this cavitation or negative pressure over the trailing face of the blades consists in so curving or shaping one or both of their faces that the angle between the same and the axial plane not only decreases to zero from the leading edge towards the trailing edge but actuallyreverses or becomes negative over a portion of the rear or trailing face of the blade.
- This reversal need not extend completely to the trailing edge.
- the. idea seems to have prevailed that .the angle referred to might decrease to zero but should never become. negative.
- leading face of the blade should be made approximately parallel to the trailing face. F or structural reasons, however, as for instance where the blades are cast and of considerable ence numeral 1.
- edges should be thinned to a certain extent and the leading face given a contour different from that of the trailing face.
- the leading face may even present a convex surface. That portion of the leading face nearest the trailing edge may be varied considerably and either curved forward, backward or left straight depending upon the relative importance of large capacity, maximum efficiency and high or low difference of premure between the two faces of the fan.
- FIG. 1 shows a perspective view of a fan constructed according to my invention
- Figs. 2 to 12 inclusive are cross sections taken through various forms of blades which can be used in carrying out my invention.
- the fan is composed of four blades of the type referred to, suitably attached to a spider 2 and shaft 3 with pulley 4 for driving the fan in the direction indicated by the arrows.
- the blades have been formed from rectangular sheets of material and are set approximately radial to the shaft. It is obvious that the blades may, if desired, be formed integral with the spider, that the blades may be tipped away from the radial position, that the number of blades, their outline or contour can be altered and various other modifications resorted to without departing from the spirit of the invention.
- Fig. 1 the leading edge is indicated by reference numeral 1, the leading face by reference numeral 1 the trailing face by numeral 1 and the trailing edge by refer-
- the other various forms of blades have corresponding portions and edges.
- Figs. 2, 8 and 9 show different forms of blades made from sheet material while Figs. 3 to 7 and 10 to 12 show difl'erent forms of blades which are cast.
- Fig. 3 shows a blade generally similar to that shown in Fig. 2 as regards contour of the leading and trailin faces but differs as to thickness of the bla e wall, thereby necessitating variation of the two faces from parallelism.
- the variation between parallelism of the two faces is more marked in Fig. 4.
- the leading face is a plane surface.
- the leading face has both concave and convex portions and also the angularity of the leading face is not reversed, or in other wordsfdoes not go beyond the zeroplane.
- Fig. 6 shows a form generally similar to Fig.4, but the leading face is curved beyond a plane surface and has become convex.
- Fig. 4 shows a blade generally similar to that shown in Fig. 2 as regards contour of the leading and trailin faces but differs as to thickness of the bla e wall, thereby necessitating variation of the two faces from parallelism.
- the variation between parallelism of the two faces is more marked in
- Fig. 7 the plane is generally similar to that in Fig. 3, but again, the angularity of the leading face does not reverse.
- Fig. 8 is like Fig. 2 except -that the trailing edge has a second reversal as to both of its faces.
- Fig. 9 the blade is quite similar to that in Fig. 2 but toward its leading edge the blade has a straight portion, whereas that in Fig. 2 is curved from edge to edge.
- the second reversal occurs only on the trailing face.
- Fig. 11 the reversal occurs on the leading face and in Fig. 12, two reversals oc. cur on'the leading face, while in both views there is no reversal of the trailing face as distinguished from all otherviews.
- a fan of the propeller or screw type for circulating air or other fluids having one or more blades, the trailing face of each blade being" so shaped that the angle between the same and the axial plane decreases to zero from the leading edge towards the trailing edge and reverses so ;as to become negative over a portion of such face.
- a fan of the propeller or screw type for circulating air or other fluids having one or more blades, the leading face of each blade being so shaped that the angle between the same and the axial plane decreases to zero from the leading edge towards the trailing edge and reverses so as to become negative over'a portion of such face.
- a fan of the propeller or screw type for circulating air or other fluids having one or more blades, the leading and trailing faces of which are so shaped that the angle between the same and the axial plane decreases to zero from the leading edge towards the trailing edge and then reverses so as to become negative over a portion of such face.
- a fan of the propeller or screw type for circulating air or 'other fluids havin one or more blades, the trailing face of eac blade .being so shaped that the angle between the same and the axial'planedecreases to zero from the'leading edge towards the 1 trailing edge, then reverses so as'to become negative over a portion of such face and again reverses adjacent to the trailing edge.
- a fan of the propeller or screw type for circulating air or o-ther fiuids having one or more blades, the leading face of each blade being so shaped that the angle between same and the axial plane decreases to zero from the leading edge towards the trailing edge,then .reverses so as to become negative over a portion of such face, and again reverses adjacent to the trailing edge.
- a fan ofthe propeller or screw type -for circulating air orother fluids having one or more blades, the leadingand trailing faces of which are so shaped that the anglebetween. the same and the axial plane decreases to zero from the leading edge towards the trailing edge, then reverses so as to become negative over a. portion of the rear or trailing half of such faces, and again reverses adjacent to the trailing edge.
Description
NW, 6,1923. mums- M. R. WELLS FAN FOR AUTOMOBILE RADIATORS OR THE LIKE Filed March 20. 1922 2 1?? J. fig 11. fzgi #02 a fizz/2222101:
Patented Nev. d, 11923.
at are MERRIT'T R. WELLS, 01E CLEVELAND, OHIO.
ran FOR AUTOMOBILE RADIATORS OR THE LIKE.
Application filed March 20, 1922. Serial No. EMM'IO.
To all whom it may concern:
Be it known that T, Mnnnrr'r R. WELLS, a citizen of the United States, residing at Cleveland, in the county of'C'uyahoga and State of Ohio, have invented certain new and useful Improvements in Fans for Automobile Radiators or the like, of which the following is a specification.
This invention relates to improvements 1n the construction of fans of the so-called Aaropeller or screw type wherein the air or uid passing through the fan, flows along lines which are approximately parallel to the axis rather than radial or tangential as may be true in a centrifugal fan.
The object of the invention consists in so shaping the vanes or blades as to induce, to a greater degree, the production of cavitation or negative pressure over the trailing face of the blades and so varying this negative pressure that it is greater near the trailing edge of the blade than at the leading edge. Thus it is the object of this invention to produce a negative pressure over the trailing face which will promote the flow of air or fluid to and through the fan and which will operate in addition to the positive urging force or action which takes place over the leading face of the blade, thereby greatly increasing the capacity of the fan.
My preferred means for producing this cavitation or negative pressure over the trailing face of the blades, consists in so curving or shaping one or both of their faces that the angle between the same and the axial plane not only decreases to zero from the leading edge towards the trailing edge but actuallyreverses or becomes negative over a portion of the rear or trailing face of the blade. This reversal need not extend completely to the trailing edge. In fact under certain conditions it may be advisable to give the face a second reversal so that its portion near the trailing edge lies in a zero plane or makes a positive angle with respect to the axial plane. Heretofore, the. idea seems to have prevailed that .the angle referred to might decrease to zero but should never become. negative.
In order to obtain the full advantage of the cavitation mentioned, the leading face of the blade should be made approximately parallel to the trailing face. F or structural reasons, however, as for instance where the blades are cast and of considerable ence numeral 1.
thickness, it is apparent that the edges should be thinned to a certain extent and the leading face given a contour different from that of the trailing face. In such a case, the leading face may even present a convex surface. That portion of the leading face nearest the trailing edge may be varied considerably and either curved forward, backward or left straight depending upon the relative importance of large capacity, maximum efficiency and high or low difference of premure between the two faces of the fan.
On the accompanying drawings, Fig. 1 shows a perspective view of a fan constructed according to my invention; Figs. 2 to 12 inclusive are cross sections taken through various forms of blades which can be used in carrying out my invention.
In the drawings the fan is composed of four blades of the type referred to, suitably attached to a spider 2 and shaft 3 with pulley 4 for driving the fan in the direction indicated by the arrows. In Fig. 1 the blades have been formed from rectangular sheets of material and are set approximately radial to the shaft. It is obvious that the blades may, if desired, be formed integral with the spider, that the blades may be tipped away from the radial position, that the number of blades, their outline or contour can be altered and various other modifications resorted to without departing from the spirit of the invention.
In Fig. 1 the leading edge is indicated by reference numeral 1, the leading face by reference numeral 1 the trailing face by numeral 1 and the trailing edge by refer- The other various forms of blades have corresponding portions and edges.
Figs. 2, 8 and 9 show different forms of blades made from sheet material while Figs. 3 to 7 and 10 to 12 show difl'erent forms of blades which are cast.
Fig. 3 shows a blade generally similar to that shown in Fig. 2 as regards contour of the leading and trailin faces but differs as to thickness of the bla e wall, thereby necessitating variation of the two faces from parallelism. The variation between parallelism of the two faces is more marked in Fig. 4. Indeed, in this view the leading face is a plane surface. In Fig. 5 the leading face has both concave and convex portions and also the angularity of the leading face is not reversed, or in other wordsfdoes not go beyond the zeroplane. Fig. 6 shows a form generally similar to Fig.4, but the leading face is curved beyond a plane surface and has become convex. In Fig. 7 the plane is generally similar to that in Fig. 3, but again, the angularity of the leading face does not reverse. Fig. 8 is like Fig. 2 except -that the trailing edge has a second reversal as to both of its faces. In Fig. 9 the blade is quite similar to that in Fig. 2 but toward its leading edge the blade has a straight portion, whereas that in Fig. 2 is curved from edge to edge. In Fig. 10 the second reversal occurs only on the trailing face. In Fig. 11 the reversal occurs on the leading face and in Fig. 12, two reversals oc. cur on'the leading face, while in both views there is no reversal of the trailing face as distinguished from all otherviews.
fans or blades constructed according to this- It has been found from experience that scribed course with a. definite load and for two trips during one of which it was equipped with an ordinary fan and during another of which it was equipped with a fan embodying this invention. During the two trips, the load, speed and other conditions were identical and the ground travelled was the same. The conditions were intentionally aggravated s0 that during both trips the automobileope-rated with the radiator. steaming. In other words, the duty was unusually high. It was found from this test that when the automobile was'equipped with a fan embodying the present invention the production of steam'was' at least cut in half, if not further reduced. Other tests have also demonstrated in practice that fans embodying this invention produce. greater flow of air or fluid pressure than other fans for the same purpose.
While the drawings show quite a number of different forms of blade, it will of course, be understoodthat the invention is not limited to the forms shown, but is capable of considerable modification within the scope of the appended. claims.
What I claim is: 1. A fan of the propeller or screw type for circulating air or other fluids, having one or more blades, the trailing face of each blade being" so shaped that the angle between the same and the axial plane decreases to zero from the leading edge towards the trailing edge and reverses so ;as to become negative over a portion of such face.
2. A fan of the propeller or screw type for circulating air or other fluids, having one or more blades, the leading face of each blade being so shaped that the angle between the same and the axial plane decreases to zero from the leading edge towards the trailing edge and reverses so as to become negative over'a portion of such face.'
3. A fan of the propeller or screw type for circulating air or other fluids, having one or more blades, the leading and trailing faces of which are so shaped that the angle between the same and the axial plane decreases to zero from the leading edge towards the trailing edge and then reverses so as to become negative over a portion of such face. i 4. A fan of the propeller or screw type for circulating air or 'other fluids, havin one or more blades, the trailing face of eac blade .being so shaped that the angle between the same and the axial'planedecreases to zero from the'leading edge towards the 1 trailing edge, then reverses so as'to become negative over a portion of such face and again reverses adjacent to the trailing edge.
5. A fan" of the propeller or screw type for circulating air or o-ther fiuids, having one or more blades, the leading face of each blade being so shaped that the angle between same and the axial plane decreases to zero from the leading edge towards the trailing edge,then .reverses so as to become negative over a portion of such face, and again reverses adjacent to the trailing edge. I
6. A fan ofthe propeller or screw type -for circulating air orother fluids, having one or more blades, the leadingand trailing faces of which are so shaped that the anglebetween. the same and the axial plane decreases to zero from the leading edge towards the trailing edge, then reverses so as to become negative over a. portion of the rear or trailing half of such faces, and again reverses adjacent to the trailing edge.
In testimony whereof I hereby affix my signature.
MERRITT R. WELLS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US545170A US1473066A (en) | 1922-03-20 | 1922-03-20 | Fan for automobile radiators or the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US545170A US1473066A (en) | 1922-03-20 | 1922-03-20 | Fan for automobile radiators or the like |
Publications (1)
Publication Number | Publication Date |
---|---|
US1473066A true US1473066A (en) | 1923-11-06 |
Family
ID=24175144
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US545170A Expired - Lifetime US1473066A (en) | 1922-03-20 | 1922-03-20 | Fan for automobile radiators or the like |
Country Status (1)
Country | Link |
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US (1) | US1473066A (en) |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2460849A (en) * | 1945-07-16 | 1949-02-08 | Jurg A Senn | Constant speed rotor for turbines |
US2709035A (en) * | 1950-11-13 | 1955-05-24 | Gilbert Co A C | Air streaming fan |
US2957621A (en) * | 1956-12-26 | 1960-10-25 | Philip L Haims | Impeller blade |
US4653985A (en) * | 1983-11-18 | 1987-03-31 | Moulded Plywood Products Pty. Ltd. | Fan blade |
US5575624A (en) * | 1996-02-14 | 1996-11-19 | Bogage; Gerald I. | Metal contoured blade for a reversible ceiling fan |
US20020176322A1 (en) * | 2001-05-22 | 2002-11-28 | Frank Kupidlowski | Sanitary mixing assembly for vessels and tanks |
US6659724B2 (en) * | 2001-02-07 | 2003-12-09 | Denso Corporation | Axial fan for vehicles |
US20040228210A1 (en) * | 2003-05-08 | 2004-11-18 | Ekato Ruhr- Und Mischtechnik Gmbh | Agitator |
US6881034B1 (en) | 2002-01-24 | 2005-04-19 | Thomas J. Riggs | Leaf rotor |
US20070104582A1 (en) * | 2005-11-04 | 2007-05-10 | Rahai Hamid R | Vertical axis wind turbine with optimized blade profile |
US20070115663A1 (en) * | 2005-11-23 | 2007-05-24 | Margaret Weiser | Twirler novelty |
US20080166235A1 (en) * | 2007-01-09 | 2008-07-10 | General Electric Company | Wind Turbine Airfoil Family |
US20090010763A1 (en) * | 2005-12-12 | 2009-01-08 | Axiom Water Propellers Ltd. | Propeller |
US7625186B1 (en) * | 2004-05-07 | 2009-12-01 | Lueddecke Leon L | Large area fan and fan blades usable for large spaces |
US20110123348A1 (en) * | 2008-01-02 | 2011-05-26 | Technion-Research &Development Foundation Ltd. | Fan and propeller performance enhancements using outsized gurney flaps |
US20110189024A1 (en) * | 2007-01-09 | 2011-08-04 | General Electric Company | Wind Turbine Airfoil Family |
USD766658S1 (en) * | 2014-11-06 | 2016-09-20 | Outotec (Finland) Oy | Impeller for mixer |
US11002292B2 (en) * | 2016-11-18 | 2021-05-11 | Mitsubishi Electric Corporation | Propeller fan and refrigeration cycle device |
USD983603S1 (en) * | 2020-12-31 | 2023-04-18 | Sharkninja Operating Llc | Blade for a micro puree machine |
US11672382B2 (en) | 2020-12-31 | 2023-06-13 | Sharkninja Operating Llc | Micro puree machine |
US11832767B2 (en) | 2020-12-31 | 2023-12-05 | Sharkninja Operating Llc | Micro puree machine |
US11864690B2 (en) | 2020-12-31 | 2024-01-09 | Sharkninja Operating Llc | Micro puree machine |
US11871765B2 (en) | 2020-12-31 | 2024-01-16 | Sharkninja Operating Llc | Micro puree machine |
-
1922
- 1922-03-20 US US545170A patent/US1473066A/en not_active Expired - Lifetime
Cited By (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2460849A (en) * | 1945-07-16 | 1949-02-08 | Jurg A Senn | Constant speed rotor for turbines |
US2709035A (en) * | 1950-11-13 | 1955-05-24 | Gilbert Co A C | Air streaming fan |
US2957621A (en) * | 1956-12-26 | 1960-10-25 | Philip L Haims | Impeller blade |
US4653985A (en) * | 1983-11-18 | 1987-03-31 | Moulded Plywood Products Pty. Ltd. | Fan blade |
US5575624A (en) * | 1996-02-14 | 1996-11-19 | Bogage; Gerald I. | Metal contoured blade for a reversible ceiling fan |
US6659724B2 (en) * | 2001-02-07 | 2003-12-09 | Denso Corporation | Axial fan for vehicles |
US6866414B2 (en) * | 2001-05-22 | 2005-03-15 | Jv Northwest, Inc. | Sanitary mixing assembly for vessels and tanks |
US20020176322A1 (en) * | 2001-05-22 | 2002-11-28 | Frank Kupidlowski | Sanitary mixing assembly for vessels and tanks |
US20050175460A1 (en) * | 2001-05-22 | 2005-08-11 | Frank Kupidlowski | Sanitary mixing assembly for vessels and tanks |
US20050175464A1 (en) * | 2001-05-22 | 2005-08-11 | Frank Kupidlowski | Sanitary mixing assembly for vessels and tanks |
US7402023B2 (en) | 2001-05-22 | 2008-07-22 | J.V. Northwest, Inc. | Sanitary mixing assembly for vessels and tanks |
US6881034B1 (en) | 2002-01-24 | 2005-04-19 | Thomas J. Riggs | Leaf rotor |
US20040228210A1 (en) * | 2003-05-08 | 2004-11-18 | Ekato Ruhr- Und Mischtechnik Gmbh | Agitator |
US7296925B2 (en) * | 2003-05-08 | 2007-11-20 | EKATO Rühr- und Mischtechnik GmbH | Agitator with improved blade configuration |
US7625186B1 (en) * | 2004-05-07 | 2009-12-01 | Lueddecke Leon L | Large area fan and fan blades usable for large spaces |
US20070104582A1 (en) * | 2005-11-04 | 2007-05-10 | Rahai Hamid R | Vertical axis wind turbine with optimized blade profile |
US7393177B2 (en) * | 2005-11-04 | 2008-07-01 | Rahai Hamid R | Vertical axis wind turbine with optimized blade profile |
US20070115663A1 (en) * | 2005-11-23 | 2007-05-24 | Margaret Weiser | Twirler novelty |
US20090010763A1 (en) * | 2005-12-12 | 2009-01-08 | Axiom Water Propellers Ltd. | Propeller |
US8221086B2 (en) * | 2005-12-22 | 2012-07-17 | Alan Edward Watts | Propeller |
US20080166235A1 (en) * | 2007-01-09 | 2008-07-10 | General Electric Company | Wind Turbine Airfoil Family |
US7883324B2 (en) * | 2007-01-09 | 2011-02-08 | General Electric Company | Wind turbine airfoil family |
US20110189024A1 (en) * | 2007-01-09 | 2011-08-04 | General Electric Company | Wind Turbine Airfoil Family |
US8226368B2 (en) * | 2007-01-09 | 2012-07-24 | General Electric Company | Wind turbine airfoil family |
US20110123348A1 (en) * | 2008-01-02 | 2011-05-26 | Technion-Research &Development Foundation Ltd. | Fan and propeller performance enhancements using outsized gurney flaps |
US8764403B2 (en) * | 2008-01-02 | 2014-07-01 | Technion Research & Development Foundation Ltd. | Fan and propeller performance enhancements using outsized gurney flaps |
USD767332S1 (en) * | 2014-11-06 | 2016-09-27 | Outotec (Finland) Oy | Impeller for mixer |
USD766658S1 (en) * | 2014-11-06 | 2016-09-20 | Outotec (Finland) Oy | Impeller for mixer |
US11002292B2 (en) * | 2016-11-18 | 2021-05-11 | Mitsubishi Electric Corporation | Propeller fan and refrigeration cycle device |
USD983603S1 (en) * | 2020-12-31 | 2023-04-18 | Sharkninja Operating Llc | Blade for a micro puree machine |
US11672382B2 (en) | 2020-12-31 | 2023-06-13 | Sharkninja Operating Llc | Micro puree machine |
US11832767B2 (en) | 2020-12-31 | 2023-12-05 | Sharkninja Operating Llc | Micro puree machine |
USD1008735S1 (en) | 2020-12-31 | 2023-12-26 | Sharkninja Operating Llc | Blade for a micro puree machine |
US11864690B2 (en) | 2020-12-31 | 2024-01-09 | Sharkninja Operating Llc | Micro puree machine |
US11871765B2 (en) | 2020-12-31 | 2024-01-16 | Sharkninja Operating Llc | Micro puree machine |
US11925298B2 (en) | 2020-12-31 | 2024-03-12 | Sharkninja Operating Llc | Micro puree machine |
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