US2561840A - Centrifugal fan - Google Patents
Centrifugal fan Download PDFInfo
- Publication number
- US2561840A US2561840A US674560A US67456046A US2561840A US 2561840 A US2561840 A US 2561840A US 674560 A US674560 A US 674560A US 67456046 A US67456046 A US 67456046A US 2561840 A US2561840 A US 2561840A
- Authority
- US
- United States
- Prior art keywords
- blades
- impeller
- centrifugal fan
- casing
- fan
- 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
- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/462—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
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- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
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- 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
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/51—Inlet
Definitions
- This invention relates to a centrifugal fan in which the fluid to be propelled enters the irnpeller centrally at one or both sides thereof and i the inlet branch or branches of the fan casing being provided with a set of guide blades which are adjustable in such a manner that the passage area between said blades may be varied.
- the adjustable guide blades in a more closed position impart a greater swirl to the incoming air than in a more open position the blades should have a different shape for each position of adjustment.
- the entrance part of the blades must always be radially directed whereas their outlet portion at full load should be radially and at zero load should be tangentially directed, so that in said rst case the blades have to be straight throughout their length and in said second case must be bent across an angle of 90.
- an intermediate form between both said blade-forms is chosen, which is slightly curved and is the exact shape of the blades for one position of adjustment only.
- the adjustable guide blades as well as the impeller blades are of aerofoil form.
- Fig. 1 of which shows a longitudinal section of a fan according to the invention
- Fig. 2 of which is a cross section taken on line II-II of Fig. 1.
- the impeller I is keyed to the shaft 2 which is supported in bearing 3, 4 and is driven by an electric motor 5 directly coupled therewith.
- the impeller has eight blades 6 of aerofoil section which are welded to the backwall of the impeller and a supporting ring I.
- the casing 8 of the fan is provided with a cylindrical inlet branch 9 to which a wall I0 is secured extending perpendicularly to the impeller shaft 2.
- a wall II Parallel to the wall I a wall II is provided which carries a cone-shaped piece I2 bounding the guide channel formed between the walls I0, I I and merging said channel into the axial portion 9- of the inlet branch of the fan casing.
- guide blades I3 are pivotally mounted by means of trunnions I4.
- the trunnions I4 projecting out of the wall II each carry an arm I connected to a ring I6 so that upon rotation of said ring the blades I3 are adjusted about an axis extending parallel to the impeller shaft 2 and the passage area between the blades is varied.
- the guide blades I3 on both sides are bounded by convex faces.
- the length I of the blades I3 is nearly equal to their mean pitch measured at the mean radius Tri-T2 2 in which r1 denotes the largest radius and ri is the smallest radius of the rim of blades.
- the blades I3 are relatively thick and their greatest thickness is at least 10% of their length I. Said form of the blades presents the advantage that the flow of the fluid not under any condition is released from the blade surface so that a very favourable efiiciency is obtained.
- the invention may also be applied to a fan in which the fluid enters at both sides and which has a set of adjustable guide blades in each inlet branch.
- a centrifugal fan comprising a fan casing, a rotatable shaft journalled in said casing, an impeller secured to said shaft in said casing and having a backwall, a supporting ring in said casing, a series of impeller blades secured to said backwall and said supporting ring adjacent the periphery of said impeller, a cylindrical mem ber secured to said casing providing an inlet branch to said impeller centrally thereof, a rst wall secured to said cylindrical member perpendicular to said rotatable shaft, a second wall spaced from said rst wall and forming therewith a guide channel, guide blades adjustably mounted between said walls and attaching said walls together, a coneshaped member secured to said second wall and merging said guide channel into said inlet branch of said casing, said impeller blades and said guide blades being of aerofoil form.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
J. C. BUSQUET CENTRIFUGAL FAN Juy 24g9 195i Filed June 5, 19@` Patented July 24, 17951 2,561,840 F F I CE 2,561,840 CENTRIFUGAL FAN Jan C. Busquet, Hengelo, Netherlands, assigner to Machinefabriek Gebr. Stork & Co. N. V.,
Hengelo, erlands Netherlands, a company of the Neth- Application June 5, 1946, serial No. 674,560 In the Netherlands April 9, 1940 section 1, PublieLaw 690, August s, 1946 Patent expires April 9, 1960 1 claim.
This invention relates to a centrifugal fan in which the fluid to be propelled enters the irnpeller centrally at one or both sides thereof and i the inlet branch or branches of the fan casing being provided with a set of guide blades which are adjustable in such a manner that the passage area between said blades may be varied.
As in centrifugal fans of this kind the adjustable guide blades in a more closed position impart a greater swirl to the incoming air than in a more open position the blades should have a different shape for each position of adjustment. The entrance part of the blades must always be radially directed whereas their outlet portion at full load should be radially and at zero load should be tangentially directed, so that in said rst case the blades have to be straight throughout their length and in said second case must be bent across an angle of 90. In practice, therefore, an intermediate form between both said blade-forms is chosen, which is slightly curved and is the exact shape of the blades for one position of adjustment only.
In order to avoid said drawback and to obtain greater efficiency in connection with the deflection of the flow of the fluid in the guide apparatus according to the invention the adjustable guide blades as well as the impeller blades are of aerofoil form.
The invention will be described with reference to the accompanying drawings, Fig. 1 of which shows a longitudinal section of a fan according to the invention and Fig. 2 of which is a cross section taken on line II-II of Fig. 1.
The impeller I is keyed to the shaft 2 which is supported in bearing 3, 4 and is driven by an electric motor 5 directly coupled therewith. The impeller has eight blades 6 of aerofoil section which are welded to the backwall of the impeller and a supporting ring I.
As appears from Fig. 2 the length of the blades 6 is considerably smaller than their mean pitch and the blades are relatively thick.
The casing 8 of the fan is provided with a cylindrical inlet branch 9 to which a wall I0 is secured extending perpendicularly to the impeller shaft 2. Parallel to the wall I a wall II is provided which carries a cone-shaped piece I2 bounding the guide channel formed between the walls I0, I I and merging said channel into the axial portion 9- of the inlet branch of the fan casing. Between the walls I 0, II guide blades I3 are pivotally mounted by means of trunnions I4.
The trunnions I4 projecting out of the wall II each carry an arm I connected to a ring I6 so that upon rotation of said ring the blades I3 are adjusted about an axis extending parallel to the impeller shaft 2 and the passage area between the blades is varied.
lli
As shown in Fig. 2 the guide blades I3 on both sides are bounded by convex faces. The length I of the blades I3 is nearly equal to their mean pitch measured at the mean radius Tri-T2 2 in which r1 denotes the largest radius and ri is the smallest radius of the rim of blades. The blades I3 are relatively thick and their greatest thickness is at least 10% of their length I. Said form of the blades presents the advantage that the flow of the fluid not under any condition is released from the blade surface so that a very favourable efiiciency is obtained.
The invention may also be applied to a fan in which the fluid enters at both sides and which has a set of adjustable guide blades in each inlet branch. f
What I claim is:
A centrifugal fan comprising a fan casing, a rotatable shaft journalled in said casing, an impeller secured to said shaft in said casing and having a backwall, a supporting ring in said casing, a series of impeller blades secured to said backwall and said supporting ring adjacent the periphery of said impeller, a cylindrical mem ber secured to said casing providing an inlet branch to said impeller centrally thereof, a rst wall secured to said cylindrical member perpendicular to said rotatable shaft, a second wall spaced from said rst wall and forming therewith a guide channel, guide blades adjustably mounted between said walls and attaching said walls together, a coneshaped member secured to said second wall and merging said guide channel into said inlet branch of said casing, said impeller blades and said guide blades being of aerofoil form.
JAN C. BUSQUET.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL2561840X | 1940-04-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2561840A true US2561840A (en) | 1951-07-24 |
Family
ID=19874758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US674560A Expired - Lifetime US2561840A (en) | 1940-04-09 | 1946-06-05 | Centrifugal fan |
Country Status (1)
Country | Link |
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US (1) | US2561840A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3069072A (en) * | 1960-06-10 | 1962-12-18 | Birmann Rudolph | Impeller blading for centrifugal compressors |
US3135684A (en) * | 1959-03-09 | 1964-06-02 | Holderbank Cement | Separating pulverous or granular material from a carrier medium |
US3642386A (en) * | 1967-10-12 | 1972-02-15 | Howden James & Co Ltd | Cooling-gas circulators for nuclear-reactor power stations |
US20080276478A1 (en) * | 2007-05-07 | 2008-11-13 | Miele & Cie. Kg | Laundry dryer having an air duct |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB302953A (en) * | 1927-09-21 | 1928-12-21 | Neil Shaw Muir | Improvements in or relating to centrifugal blowers, compressors and the like |
US1892303A (en) * | 1927-07-02 | 1932-12-27 | B F Sturtevant Co | Method and apparatus for propelling fluids |
US1906180A (en) * | 1928-10-05 | 1933-04-25 | Rees Edmund Scott Gustave | Propeller, pump, or fan |
US1978129A (en) * | 1932-03-14 | 1934-10-23 | Clarage Fan Company | Vortex control for fans |
US1997506A (en) * | 1930-09-29 | 1935-04-09 | Adamcikas Mykas | Guide vane for rotary machines |
USRE20394E (en) * | 1937-06-08 | Edward i | ||
US2201437A (en) * | 1937-05-26 | 1940-05-21 | American Blower Corp | Volume control for fans |
-
1946
- 1946-06-05 US US674560A patent/US2561840A/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE20394E (en) * | 1937-06-08 | Edward i | ||
US1892303A (en) * | 1927-07-02 | 1932-12-27 | B F Sturtevant Co | Method and apparatus for propelling fluids |
GB302953A (en) * | 1927-09-21 | 1928-12-21 | Neil Shaw Muir | Improvements in or relating to centrifugal blowers, compressors and the like |
US1906180A (en) * | 1928-10-05 | 1933-04-25 | Rees Edmund Scott Gustave | Propeller, pump, or fan |
US1997506A (en) * | 1930-09-29 | 1935-04-09 | Adamcikas Mykas | Guide vane for rotary machines |
US1978129A (en) * | 1932-03-14 | 1934-10-23 | Clarage Fan Company | Vortex control for fans |
US2201437A (en) * | 1937-05-26 | 1940-05-21 | American Blower Corp | Volume control for fans |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3135684A (en) * | 1959-03-09 | 1964-06-02 | Holderbank Cement | Separating pulverous or granular material from a carrier medium |
US3069072A (en) * | 1960-06-10 | 1962-12-18 | Birmann Rudolph | Impeller blading for centrifugal compressors |
US3642386A (en) * | 1967-10-12 | 1972-02-15 | Howden James & Co Ltd | Cooling-gas circulators for nuclear-reactor power stations |
US20080276478A1 (en) * | 2007-05-07 | 2008-11-13 | Miele & Cie. Kg | Laundry dryer having an air duct |
US8333019B2 (en) * | 2007-05-07 | 2012-12-18 | Miele & Cie. Kg | Laundry dryer having an air duct |
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