US2327841A - Propeller fan - Google Patents
Propeller fan Download PDFInfo
- Publication number
- US2327841A US2327841A US420930A US42093041A US2327841A US 2327841 A US2327841 A US 2327841A US 420930 A US420930 A US 420930A US 42093041 A US42093041 A US 42093041A US 2327841 A US2327841 A US 2327841A
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- United States
- Prior art keywords
- air
- vanes
- outlet
- spin
- casing
- 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.)
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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
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/009—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by bleeding, by passing or recycling fluid
-
- 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
- This invention relates to propeller fans, and relates more particularly to methods of and apparatus for, varying the air pressure and the air volume in propeller fan systems.
- propeller fans for moving air against substantial static resistance, in the field heretofore served by centrifugal fans, and to vary the air quantities as required.
- Thecharacteristics of propeller fans are such that they require less horse power at substantially reduced loads when they are operated substantially at or to move larger volumes of air or other gases than are required by the loads.
- This invention provides for operating propeller fans to maintain relatively large total volumes of air flowing through the A feature of the invention resides in combinin the recirculation of air through propeller :fans,
- Another feature of the invention resides in recirculating air through the impeller of a propeller fan, in spinning the recirculated air, and in controlling the spin, and in providing that at reduced fanoutputs, a greater volume of air is recirculated through the impeller than is delivered to the load.
- An object of the invention is to reduce the power required to operate propeller fans under different loads.
- Fig. l is an elevation view in section, of a propeller fan embodying this invention.
- Fig. 2 is a sectional view along the lines 22 of Fig. 1.
- the cover 9 is supported from the casing II! by the struts II which are preferably cylindrical'so as to avoid their having any effect I
- the motor 8 is attached to the stream-lined cover H which in turn is supported from the casing it by the stationary vanes I3.
- the vanes i3 serve to straighten out the spin in the air from the blades. 5 and are positioned to accomplish this most effectively.
- the casing l0 has a circumferential air outlet opening at it between the fan blades 5 and the spin straightening vanes i3, in which opening are supported the spin adjusting vanes Iii.
- the vanes l5 are fixedly secured to the studs 20 which are pivoted in the annular ring 2
- the cranks 22 are attached to the ends of the studs 20 and are interconnected by the links 23 which are the cranks.
- the links 23 form a polygon around the fan casing, each link connecting parallel pivot radii.
- the lever 24 movable by the arm 25 adjusts the lowermost vane I5 at its pivot point and simultaneously through the cranks 22 and the links 23 adjusts the other vanes l5. This mechanism is similar to that disclosed in my Patent No. 1,846,863 which issued Feb. 23, 1932. a
- the blades 5 are intended to rotate in a clock-wise direction and therefore to produce a spin in a clock-wise direction.
- a portion of the spinning air proceeds axially through the casing l0; its spin is eliminated by the vanes l3 and it passes out the outlet connection [9 to the load to which the fan is connected.
- Another portion of the spinning air passes outwardly between the vanes l5 and the spin in this air portion is of the vanes l5.
- the wall IS with the casing [0 forms an air guiding passage II for directing the air passing the fan to operate with resulting between the vanes l5 into the inlet ll of the i'an.
- the wall I8 is connected to the casing III at the back or air outlet side 01' the opening ll.
- Varying the spin of the air entering the inlet i8 varies conformably the pressure imparted to the air by the fan. This action is explained in detail in my patents, No. Re. 20,408 which was reissued June 15, 1937, and in my said Patent No. 1,846,863 and in my Patent No. 1,989,413 which issued Jan. 29, 1935.
- a propeller fan having a casing with an air inlet and an outlet and having propeller blades mounted therein between said inlet and outlet, means forming a recirculated air outlet in said casing between said blades and said first mentioned outlet, means comprising an extension from said casing and forming an air guiding passage for air from ,said recirculated air outlet to said inlet, and means for spinning the air in said passage.
- a propeller tan having a casing with an air inlet and an air outlet and having propeller blades mounted therein and having spin straight a ening vanes-between said blades and said outlet,
- a propeller fan having a casing with an air inlet and an axial, air outlet and having propeller blades mounted therein and having spin straightening vanes between said blades and said outlet, means forming a circumferentially extend,- ing, recirculated air outlet slot in said casing between said blades and said vanes, means comprising an extension from said casing and formin an air guiding passage for air from said recirculated air outlet to said inlet, and spin adjusting vanes in said circumferential outlet slot.
- a propeller fan having a casing with an air inlet and an outlet and having propeller blades mounted therein between said inlet and outlet,
- a propeller fan having a casing with an air inlet and an air outlet and having propeller blades mounted therein and having spin straight ening vanes between said blades and said outlet,
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- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Aug. 24, 1943 H. F. HAGEN PROPELLER FAN Original Filed June 12, 1940 Patented Aug. 24, 1943 Harold F. Hagen, Wellesiey, Mass.,
B. F. Sturtevant Company, Hyde Park,
Mass.
Original application 340,126. Divided 8nd assignor to Boston,
June 12, 1940, Serial No.
this application November 29, 1941, Serial No. 420,930
6 Claims.
This invention relates to propeller fans, and relates more particularly to methods of and apparatus for, varying the air pressure and the air volume in propeller fan systems.
This application is a division of my co-pendin application, Serial No. 340,126, which was filed June 1 2, 1940.
In many systems utilizing fans, such for example, as steam power plant systems, it is desirable to vary the air quantities from a fan. For example, in a steam power plant, it is usual to vary the volume of air supplied by a forced draft fan conformably with changes in the load'upon the plant. Heretofore, it has been customary to utilize centrifugal fans for such duties requirin the fans to work against substantial static resistance and to vary the volumes .0! air delivered to the systems by means for example, of dampers in the fan inlets or outlets, or change oi speed.
I propose to utilize propeller fans for moving air against substantial static resistance, in the field heretofore served by centrifugal fans, and to vary the air quantities as required. Thecharacteristics of propeller fansare such that they require less horse power at substantially reduced loads when they are operated substantially at or to move larger volumes of air or other gases than are required by the loads. This invention provides for operating propeller fans to maintain relatively large total volumes of air flowing through the A feature of the invention resides in combinin the recirculation of air through propeller :fans,
with the spinning of the air for supplying desired air quantities with minimum power.
Another feature Of the invention resides in recirculating air through the impeller of a propeller fan, in spinning the recirculated air, and in controlling the spin, and in providing that at reduced fanoutputs, a greater volume of air is recirculated through the impeller than is delivered to the load. I
An object of the invention is to reduce the power required to operate propeller fans under different loads.
The invention will now be described with reference to the drawing, of which:
Fig. l is an elevation view in section, of a propeller fan embodying this invention, and
Fig. 2 is a sectional view along the lines 22 of Fig. 1.
1 upon the spin ofthe air.
. impellers at all times, and for varying the voladiusted by adjustment Y pivoted at their ends to In the embodiment of Figs. 1 and 2, air for recirculation through the fan, is taken through a circumferentially extending opening between the fan wheel' and the spin straightening vanes, and recirculated through the fan inlet, and the spin of the recirculated air is adjusted by vanes in the circumferentially extending opening. Referring now to Figs. 1 and 2, the propeller v blades 5 are formed on the hub 6 which in turn is keyed to the shaft I. The shaft 1 is supported at one end by the bearings of the electric motor 8 and at the other end by a bearing in the streamlined cover 9. The cover 9 is supported from the casing II! by the struts II which are preferably cylindrical'so as to avoid their having any effect I The motor 8 is attached to the stream-lined cover H which in turn is supported from the casing it by the stationary vanes I3. The vanes i3 serve to straighten out the spin in the air from the blades. 5 and are positioned to accomplish this most effectively.
The casing l0 has a circumferential air outlet opening at it between the fan blades 5 and the spin straightening vanes i3, in which opening are supported the spin adjusting vanes Iii. The vanes l5 are fixedly secured to the studs 20 which are pivoted in the annular ring 2|. The cranks 22 are attached to the ends of the studs 20 and are interconnected by the links 23 which are the cranks. The links 23 form a polygon around the fan casing, each link connecting parallel pivot radii. The lever 24 movable by the arm 25 adjusts the lowermost vane I5 at its pivot point and simultaneously through the cranks 22 and the links 23 adjusts the other vanes l5. This mechanism is similar to that disclosed in my Patent No. 1,846,863 which issued Feb. 23, 1932. a
With the vanes l5 positioned as illustrated by Fig. 2, the blades 5 are intended to rotate in a clock-wise direction and therefore to produce a spin in a clock-wise direction. A portion of the spinning air proceeds axially through the casing l0; its spin is eliminated by the vanes l3 and it passes out the outlet connection [9 to the load to which the fan is connected. Another portion of the spinning air passes outwardly between the vanes l5 and the spin in this air portion is of the vanes l5. when the vanes [5 are adjusted towards closed position, the spin is increased and when the vanes l5 are adjusted towards open position, the spin isreduced.
The wall IS with the casing [0 forms an air guiding passage II for directing the air passing the fan to operate with resulting between the vanes l5 into the inlet ll of the i'an.
The wall I8 is connected to the casing III at the back or air outlet side 01' the opening ll.
Varying the spin of the air entering the inlet i8 varies conformably the pressure imparted to the air by the fan. This action is explained in detail in my patents, No. Re. 20,408 which was reissued June 15, 1937, and in my said Patent No. 1,846,863 and in my Patent No. 1,989,413 which issued Jan. 29, 1935.
In operation at reduced outputs, a relatively large volume of air consisting of direct air through the inlet I8 into the inlet l8 and of recirculated air through the passage i! into the inlet l8 passes spinning of the air are combined. Through recirculation relatively large volumes of air pass through the impeller at all times, thus enabling minimum power requirements, and the controlled spinning of the air results in the desired pressure changes also with minimum power requirements.
While one embodiment of the invention has been described for the purpose of illustration, it
should be understood that the invention is not limited tothe exact apparatus and arrangements of apparatus illustrated, as modifications thereof may be devised by those skilled in the art without departure from the essence of the invention.
What is claimed is:
1. In a propeller fan having a casing with an air inlet and an outlet and having propeller blades mounted therein between said inlet and outlet, means forming a recirculated air outlet in said casing between said blades and said first mentioned outlet, means comprising an extension from said casing and forming an air guiding passage for air from ,said recirculated air outlet to said inlet, and means for spinning the air in said passage.
2 In a propeller tan having a casing with an air inlet and an air outlet and having propeller blades mounted therein and having spin straight a ening vanes-between said blades and said outlet,
means forming a recirculated air outlet in said casing between said blades and said vanes, means comprising an extension from said casing and forming an air guiding passage for air from said recirculated air outlet to said inlet, and spin ad- Justing means in said recirculated air outlet. 3. In a propeller fan having a casing with an air inlet and an axial, air outlet and having propeller blades mounted therein and having spin straightening vanes between said blades and said outlet, means forming a circumferentially extend,- ing, recirculated air outlet slot in said casing between said blades and said vanes, means comprising an extension from said casing and formin an air guiding passage for air from said recirculated air outlet to said inlet, and spin adjusting vanes in said circumferential outlet slot. I
4. In a propeller fan having a casing with an air inlet and an outlet and having propeller blades mounted therein between said inlet and outlet,
means forming a recirculated air outlet in saidcasing between said blades and said first mentioned outlet, means forming an air guiding passage for air from said recirculated air outlet to said inlet, and means for spinning the air in said passage.
, 5. In a propeller fan having a casing with an air inlet and an air outlet and having propeller blades mounted therein and having spin straight ening vanes between said blades and said outlet,
means forming a recirculated air outlet in said casing between said blades and said vanes, means forming an air guiding passage for air from said recirculated air outlet to said inlet, and spin adlusting means in saidrecirculated air outlet.
' 6. In a propeller i'an having a casing with an.
air inlet and an air axial outlet and having propeller blades mounted therein and having spin straightening vanes between said blades and said outlet, means forming a lcircumferentially ex tending, recirculated air outlet slot in said casing between said blades and said vanes, means forming an air guiding passage for. air from saidv recirculated air outlet to said inlet, and spin adjusting vanes in said slot.
HAROLD F. HAGEN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US420930A US2327841A (en) | 1940-06-12 | 1941-11-29 | Propeller fan |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US34012640A | 1940-06-12 | 1940-06-12 | |
US420930A US2327841A (en) | 1940-06-12 | 1941-11-29 | Propeller fan |
Publications (1)
Publication Number | Publication Date |
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US2327841A true US2327841A (en) | 1943-08-24 |
Family
ID=26991976
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US420930A Expired - Lifetime US2327841A (en) | 1940-06-12 | 1941-11-29 | Propeller fan |
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US (1) | US2327841A (en) |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2638158A (en) * | 1950-04-19 | 1953-05-12 | Peabody Engineering Corp | Register control |
US2653754A (en) * | 1949-11-01 | 1953-09-29 | Westinghouse Electric Corp | Axial flow fan regulator |
US2660366A (en) * | 1950-05-03 | 1953-11-24 | Klein Harold | Compressor surge inhibitor |
US2693914A (en) * | 1951-04-11 | 1954-11-09 | El Roy L Payne | Hot air furnace control |
US2798658A (en) * | 1955-03-01 | 1957-07-09 | Westinghouse Electric Corp | Volume controls for centrifugal fans |
US2808197A (en) * | 1955-12-27 | 1957-10-01 | Licencia Talalmanyokat | Fan assembly |
US2981461A (en) * | 1958-04-18 | 1961-04-25 | Westinghouse Electric Corp | Centrifugal fans |
US3019963A (en) * | 1955-07-08 | 1962-02-06 | Eck Bruno Christian | Radial blower for gases with high dust content |
US3023709A (en) * | 1958-05-26 | 1962-03-06 | Kondo Masukichi | Vanes of an impeller for axial flow propeller pumps |
US3107046A (en) * | 1958-07-18 | 1963-10-15 | Richardsons Westgarth & Co | Turbines, blowers and the like |
US3226938A (en) * | 1962-05-14 | 1966-01-04 | William H Anderson | Air-conditioning systems for enclosed spaces such as automobiles |
US3723019A (en) * | 1971-05-21 | 1973-03-27 | Worthington Corp | Means to overcome low flow problems of inducers in centrifugal pumps |
US4255080A (en) * | 1978-03-28 | 1981-03-10 | James Howden & Company Limited | Fans or the like |
US4391570A (en) * | 1981-04-29 | 1983-07-05 | Clarence Stutzman | Apparatus for cooling a ceiling mounted fan motor |
US4630993A (en) * | 1983-07-28 | 1986-12-23 | Nordisk Ventilator Co. | Axial-flow fan |
US5749702A (en) * | 1996-10-15 | 1998-05-12 | Air Handling Engineering Ltd. | Fan for air handling system |
US20140178173A1 (en) * | 2012-12-21 | 2014-06-26 | Hamilton Sundstrand Corporation | Ejector assembly |
-
1941
- 1941-11-29 US US420930A patent/US2327841A/en not_active Expired - Lifetime
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2653754A (en) * | 1949-11-01 | 1953-09-29 | Westinghouse Electric Corp | Axial flow fan regulator |
US2638158A (en) * | 1950-04-19 | 1953-05-12 | Peabody Engineering Corp | Register control |
US2660366A (en) * | 1950-05-03 | 1953-11-24 | Klein Harold | Compressor surge inhibitor |
US2693914A (en) * | 1951-04-11 | 1954-11-09 | El Roy L Payne | Hot air furnace control |
US2798658A (en) * | 1955-03-01 | 1957-07-09 | Westinghouse Electric Corp | Volume controls for centrifugal fans |
US3019963A (en) * | 1955-07-08 | 1962-02-06 | Eck Bruno Christian | Radial blower for gases with high dust content |
US2808197A (en) * | 1955-12-27 | 1957-10-01 | Licencia Talalmanyokat | Fan assembly |
US2981461A (en) * | 1958-04-18 | 1961-04-25 | Westinghouse Electric Corp | Centrifugal fans |
US3023709A (en) * | 1958-05-26 | 1962-03-06 | Kondo Masukichi | Vanes of an impeller for axial flow propeller pumps |
US3107046A (en) * | 1958-07-18 | 1963-10-15 | Richardsons Westgarth & Co | Turbines, blowers and the like |
US3226938A (en) * | 1962-05-14 | 1966-01-04 | William H Anderson | Air-conditioning systems for enclosed spaces such as automobiles |
US3723019A (en) * | 1971-05-21 | 1973-03-27 | Worthington Corp | Means to overcome low flow problems of inducers in centrifugal pumps |
US4255080A (en) * | 1978-03-28 | 1981-03-10 | James Howden & Company Limited | Fans or the like |
US4391570A (en) * | 1981-04-29 | 1983-07-05 | Clarence Stutzman | Apparatus for cooling a ceiling mounted fan motor |
US4630993A (en) * | 1983-07-28 | 1986-12-23 | Nordisk Ventilator Co. | Axial-flow fan |
US5749702A (en) * | 1996-10-15 | 1998-05-12 | Air Handling Engineering Ltd. | Fan for air handling system |
US20140178173A1 (en) * | 2012-12-21 | 2014-06-26 | Hamilton Sundstrand Corporation | Ejector assembly |
US9347455B2 (en) * | 2012-12-21 | 2016-05-24 | Hamilton Sundstrand Corporation | Ejector assembly |
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