US1961228A - Fan - Google Patents

Fan Download PDF

Info

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
Application number
US603800A
Inventor
Harry A Knox
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US603800A priority Critical patent/US1961228A/en
Application granted granted Critical
Publication of US1961228A publication Critical patent/US1961228A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors 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,
US603800A 1932-04-07 1932-04-07 Fan Expired - Lifetime US1961228A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (6)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
US2314572A (en) Turboengine
US2191341A (en) Ventilator
SU917709A3 (en) Impeller of centrifugal blower
US2392113A (en) Fan wheel
US2385070A (en) Fan
GB996729A (en) Improvements relating to turbines and compressors
US4171937A (en) Grill panel and motor mount assembly
GB1567584A (en) Low-noise cooling system for international combustion engines
US1961228A (en) Fan
US3289924A (en) Flexible blade fan
GB1395957A (en) Fluid flow machines and rotors therefor
US1447915A (en) Centrifugal fan
US2802618A (en) Foreign object separator
GB1474644A (en) Fan blade and root assembly
US2115367A (en) Blower wheel and impeller
US2368392A (en) Car heater and defroster
GB1050879A (en)
US1781165A (en) Centrifugal fan
US1345951A (en) Self-alining fan-wheel
US3127094A (en) Rotor with impeller vanes
US1429570A (en) Turbine
US1718869A (en) Windmill accelerator
US2135939A (en) Differential pressure mechanism
US1356063A (en) High-pressure fluid-pump
SU1073495A1 (en) Outward-flow turbo-machine wheel