US1961228A - Fan - Google Patents
Fan Download PDFInfo
- Publication number
- US1961228A US1961228A US603800A US60380032A US1961228A US 1961228 A US1961228 A US 1961228A US 603800 A US603800 A US 603800A US 60380032 A US60380032 A US 60380032A US 1961228 A US1961228 A US 1961228A
- Authority
- US
- United States
- Prior art keywords
- vanes
- fan
- hub
- ring
- plate
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
Definitions
- This invention relates to a fan.
- the principal object of the invention is to provide a fan whose velocity will be automatically varied inversely to the speed of the motor driving the fan.
- a further object is to provide an arrangement of the vanes which will insure equal loading over the entire area of the vane.
- the invention consists in the construction, arrangement and com- 16 bination of elements described hereinafter and pointed out in the claim forming a part of this specification.
- Fig. 1 is a View in front elevation of a fan constructed in accordance with the invention.
- Fig. 2 is a longitudinal sectional view through a portion of the fan.
- Fig. 3 is a view in side elevation of one of the vanes and indicating in dotted lines the deflected position at high speed.
- the fan is of the Sirocco type comprising a hub 6, which in the present-instance is the driven flywheel of an engine, and oblong vanes '7 arranged annularly about the hub and supported in spaced relation thereto with their trailing portions on a battle plate 8 and with their leading portions on a ring 9 carried by. spokes 10.
- the bafiie plate 8 and spokes 10 are secured respectively to the margin and theperiphery of the hub 6 by means of bolts 8a and 10a.
- the baflle plate 8 is inclined with respect to the hub 6 and its periphery is on a shorter radius than the periphery of the ring 9 so that the vanes supported by these members are inclined relative to the axis of rotation of the fan.
- the vanes '7 are flexible and are capable of being deflected to position indicated in dotted lines in Fig. 3, when the fan is being driven at the rate of 2,000 R. P. M.
- the flexibility of the blades is determined on a basis of initial deflection at 500 R. P. M. As the deflection varies between these velocities the area of the vane will automatically vary, being decreased as the velocity increases. This provision effects a considerable saving in motive power.
- the flexibility of the vanes is preferably obtained by forming them of a plurality of leaves of varying height.
- four leaves are employed, designated a, b, c, and d, secured at their base by means of rivets 16.
- the leaf d is essentially a reinforcing strip and may be of thicker metal without flexibility to facilitate mounting of the vane in the slots 11 and 12. 7
- a shroud 1'7 terminates adjacent the leading edge of the vanes.
- a fan including a hub, a bailie plate secured in an inclined position on the periphery of the hub, spokes on the periphery of the hub and spaced from the baiiie plate, a ring carried by the spokes, said ring and bafiie plate formed with a plurality of slots, an annular series of flexible vanes mounted in the slots of the ring and baflie plates, lugs on the vanes engageable with the sides of the ring and bafiie plate, and a cable passing through all of the vanes and holding them in place.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
H. A. KNOX June 5, 1934.
FAN
Filed April 7, 1932 Inventor Harr Alinux Patented June 5, 1934 UNITED STATES PATENT OFFICE 1 Claim.
(Granted under the act of March 3, 1883, as
amended April 30, 1928; 370 0. G. 757) The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment to me of any royalty thereon.
This invention relates to a fan.
The principal object of the invention is to provide a fan whose velocity will be automatically varied inversely to the speed of the motor driving the fan.
A further object is to provide an arrangement of the vanes which will insure equal loading over the entire area of the vane.
To these and other ends, the invention consists in the construction, arrangement and com- 16 bination of elements described hereinafter and pointed out in the claim forming a part of this specification.
'A practical embodiment of the invention is illustrated in the accompanying drawing, wherein:
Fig. 1 is a View in front elevation of a fan constructed in accordance with the invention.
Fig. 2 is a longitudinal sectional view through a portion of the fan.
Fig. 3 is a view in side elevation of one of the vanes and indicating in dotted lines the deflected position at high speed.
The fan is of the Sirocco type comprising a hub 6, which in the present-instance is the driven flywheel of an engine, and oblong vanes '7 arranged annularly about the hub and supported in spaced relation thereto with their trailing portions on a baiile plate 8 and with their leading portions on a ring 9 carried by. spokes 10. The bafiie plate 8 and spokes 10 are secured respectively to the margin and theperiphery of the hub 6 by means of bolts 8a and 10a.
The baflle plate 8 is inclined with respect to the hub 6 and its periphery is on a shorter radius than the periphery of the ring 9 so that the vanes supported by these members are inclined relative to the axis of rotation of the fan. By virtue of this arrangement the leading portion of the vane being required to travel through a greater circle locity than the trailing portion for a purpose in the same unit of time will have a higher ve'- .apertures in the vanes and each having its ends secured in a turnbuckle 15.
The vanes '7 are flexible and are capable of being deflected to position indicated in dotted lines in Fig. 3, when the fan is being driven at the rate of 2,000 R. P. M. The flexibility of the blades is determined on a basis of initial deflection at 500 R. P. M. As the deflection varies between these velocities the area of the vane will automatically vary, being decreased as the velocity increases. This provision effects a considerable saving in motive power.
The flexibility of the vanes is preferably obtained by forming them of a plurality of leaves of varying height. In the present instance four leaves are employed, designated a, b, c, and d, secured at their base by means of rivets 16. The leaf d is essentially a reinforcing strip and may be of thicker metal without flexibility to facilitate mounting of the vane in the slots 11 and 12. 7
As shown in Fig. 2 a shroud 1'7 terminates adjacent the leading edge of the vanes.
In operation the air passing through the fan tends to pile up against the baffle plate 8 so that where the vanes are disposed parallel to the axis of rotation there is an unequal loading or distribution and the trailing portion of the vanes performs most of the work. By inclining the vanes as proposed herein and giving the leading portion a higher velocity the pressures and loading are equally distributed over the entire area of the vanes. By thus eliminating the inefi'ective portions of the vane it is possible to reduce their size. This arrangement is also of particular advantage in connection with the use of flexible vanes as it prevents distortion of the vanes.
I claim:
A fan including a hub, a bailie plate secured in an inclined position on the periphery of the hub, spokes on the periphery of the hub and spaced from the baiiie plate, a ring carried by the spokes, said ring and bafiie plate formed with a plurality of slots, an annular series of flexible vanes mounted in the slots of the ring and baflie plates, lugs on the vanes engageable with the sides of the ring and bafiie plate, and a cable passing through all of the vanes and holding them in place.
HARRY A. KNOX,
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US603800A US1961228A (en) | 1932-04-07 | 1932-04-07 | Fan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US603800A US1961228A (en) | 1932-04-07 | 1932-04-07 | Fan |
Publications (1)
Publication Number | Publication Date |
---|---|
US1961228A true US1961228A (en) | 1934-06-05 |
Family
ID=24416970
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US603800A Expired - Lifetime US1961228A (en) | 1932-04-07 | 1932-04-07 | Fan |
Country Status (1)
Country | Link |
---|---|
US (1) | US1961228A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442783A (en) * | 1944-07-01 | 1948-06-08 | Us Sec War | Turbine rotor |
US2692563A (en) * | 1949-07-12 | 1954-10-26 | John J Kovacs | Impeller |
US3990808A (en) * | 1975-11-24 | 1976-11-09 | Boris Isaacson | Inflatable blower |
US4900227A (en) * | 1988-06-14 | 1990-02-13 | Thomson-Brandt-Armements | Wind power of hydraulic power machine with axial feed, radial outflow, and variable geometry vanes, and projectiles fitted with wind power or hydraulic power machines of this type |
WO1999020523A1 (en) * | 1997-10-17 | 1999-04-29 | Dbs Manufacturing, Inc. | Method and apparatus for aeration using flexible blade impeller |
-
1932
- 1932-04-07 US US603800A patent/US1961228A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442783A (en) * | 1944-07-01 | 1948-06-08 | Us Sec War | Turbine rotor |
US2692563A (en) * | 1949-07-12 | 1954-10-26 | John J Kovacs | Impeller |
US3990808A (en) * | 1975-11-24 | 1976-11-09 | Boris Isaacson | Inflatable blower |
US4900227A (en) * | 1988-06-14 | 1990-02-13 | Thomson-Brandt-Armements | Wind power of hydraulic power machine with axial feed, radial outflow, and variable geometry vanes, and projectiles fitted with wind power or hydraulic power machines of this type |
WO1999020523A1 (en) * | 1997-10-17 | 1999-04-29 | Dbs Manufacturing, Inc. | Method and apparatus for aeration using flexible blade impeller |
US5993158A (en) * | 1997-10-17 | 1999-11-30 | Dbs Manufacturing, Inc. | Method and apparatus for aeration using flexible blade impeller |
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