US2894681A - Centrifugal blower wheel structure - Google Patents

Centrifugal blower wheel structure Download PDF

Info

Publication number
US2894681A
US2894681A US501484A US50148455A US2894681A US 2894681 A US2894681 A US 2894681A US 501484 A US501484 A US 501484A US 50148455 A US50148455 A US 50148455A US 2894681 A US2894681 A US 2894681A
Authority
US
United States
Prior art keywords
blade
flanges
blades
hub plate
blower wheel
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
US501484A
Inventor
Lunde Einar
William T Nichols
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.)
Trane Co
Original Assignee
Trane Co
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 Trane Co filed Critical Trane Co
Priority to US501484A priority Critical patent/US2894681A/en
Application granted granted Critical
Publication of US2894681A publication Critical patent/US2894681A/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
    • F04D29/282Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
    • F04D29/283Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis rotors of the squirrel-cage type
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49236Fluid pump or compressor making
    • Y10T29/49243Centrifugal type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

7 July 14, 1959 E. LUNDE ETAL CENTRIFUGAL BLOWER WHEEL STRUCTURE 3 Sheets-Sheet 1 Filed April 15, 1955 INVENTORS E INAR LUNDE WILL/AM 7f NICHOLS BY Mu v W ATTORNEYS July 14, 1959 E. LUNDE ET AL 2,894,681
CENTRIFUGAL BLOWER WHEEL STRUCTURE Filed April 15, 1955 3 Sheets5heet 2 INVENTORS E/NAR LUNDE WILLIAM 1: NICHOLS BY, v.
ATTORNEYS July 14, 1959 E. LUNDE ET AL 2,394,681
CENTRIFUGAL BLOWER WHEEL" STRUCTURE Filed April 15, 1955 5 Sheets-$heet 3 Fig.10.
Fig.11.
INV EN TORS EINAR LUNDE WILLIAM 7T NICHOLS BY V2 I ATTORNEYS United States Patent 2,894,681 CENTRIFUGAL BLOWER WHE'EL STRUCTURE Einar Lunde and William T. Nichols, La Crosse, Wis., assignors to The Trane Company, La Crosse, Wis.
Application April 15, 1955, Serial No. 501,484 3 Claims. (Cl. 230- 134) This invention relates to improvements in centrifugal blower wheels and more particularly to an improved arrangement for assembling the cylindrical body structure of a blower wheel to an associated hub plate.
Heretofore in the manufacture of centrifugual blower wheels, the process of assembling the large number of parts required for the complete wheel has been a time consuming and expensive operation. The blade structure of this invention is such that the fan blades are assembled into a unitary flexible strip by the machine which forms the blades. By reason of this construction, the number of parts required for a complete wheel is reduced and the assembly of the wheel is simplified.
It is an object of this invention to provide a blade structure by which the blades are interlocked into a unitary flexible strip.
It is another object of the invention to provide a blade structure by which flanges on the blades form rim portions of the wheel.
It is another object to provide a blower wheel which has a maximum effective blade length with only a relatively small space at the ends for blade retention.
It is still another object of the invention to provide a centrifugal blower wheel in which the parts thereof can be assembled very rapidly so that the wheels can be manufactured in quantities with low cost for labor and material.
Other objects and advantages of the invention will become apparent as the specification proceeds to describe the invention with reference to the accompanying drawings in which:
Figure 1 is a sectional view of the blower wheel taken on line 11 of Figure 4;
Figure 2 is a perspective view of a portion of the blower wheel showing the blade structure;
Figure 3 is a perspective view of a part of the hub plate of a double width blower wheel;
Figure 4 is a sectional view taken on line 44 of Figure 1;
Figure 5 is a sectional view of the end of a blade taken on line 55 of Figure 6.
Figure 6 is an elevational end view of a blade.
Figure 7 is a sectional view of part of the hub plate of a double width wheel taken on a radial plane.
Figure 8 is a partial sectional view of a double Width wheel taken on a radial plane.
Figure 9 is an elevational view of part of a wheel showing the welds securing the blades together.
Figure 10 is an elevational view of part of a wheel showing a modification of the invention in which the blades are spot welded to each other.
Figure 11 is an elevational view of part of a wheel showing another modification of the invention in which the blades are seam welded to each other.
Referring now to the drawings and particularly Figures 1 and 2, numeral 10 designates a hub plate to which is secured a hub 12 and blades 14. The blade 14 has a vane portion 16 which is curved in cross-section and a flange base portion 18 at each end extending at rig t angles to the vane portion 16. Extending from the flange base portions 18 are flange end portions 20 ofiset out wardly from the flange base portions 18 so that the flange end portions 20 will receive therebetween the flange base portions 18 of the next adjacent blade.
The flange base portion 18 of each blade has an inwardly extending dimple 22 having its center substantially at the axis of curvature of the convex surface of the vane portion 16 of the blade. The flange end portion 20 of each blade has an inwardly extending dimple 24 which engages in the dimple 22 in the flange base portion of the next adjacent blade to hold the blades in the form of a flexible strip leaving the blade forming press. The dimple 24 may be formed prior to the assembly of the blade to the next adjacent blade. The resiliency of the flange portions 18 and 20 will permit the blade to be nested on the next adjacent blade and the dimple 24 will snap into place in the dimple 22. Alternatively the press can assemble the blade in nested position on the next adjacent blade and form the dimple 24 into the dimple 22.
A strip having the required number of blades 14 for a given wheel is then removed from the continuous strip produced by the press. After removal this strip is held in annular form and the first blade is nested in the last blade with the dimples of the blades in engagement. The blades 14 are then secured to each other by welding. Various forms of welding may be used.
Figure 9 shows a brazing weld which is produced by placing brazing material in contact with the flange portions 18 and 20 of the blade and then heating the blade the flange end portion of each blade is electrically spot welded at 26 to the flange base portion of the adjacent blade.
Still another form of weld is shown in Figure 11 in which a seam weld 28 is produced between the flanges of the blades by an electric or gas welding process.
The hub plate 10 has a hub 12 secured thereto in any suitable manner as by swaging the flange 30 against the hub plate 10. The hub plate 10 has a peripheral channel 32 which receives one end of the blade assembly as shown in Figure 4.
The hub plate 10 is then secured to the blade assembly by welding or riveting at the peripheral channel 32. We prefer to electrically spot weld the blade assembly to the hub plate at several spaced points. If desired the brazing procedure described with reference to Figure 9 can be used to simultaneously braze the hub plate 10 and the assembled blades into a unitary structure.
As shown in Figure 8 a double width blower wheel comprises a hub plate 34 with a blade assembly secured to each side of the hub plate at the periphery. Hub plate 34 has a hub 36 secured thereto in any suitable manner as by swaging the flange 38 against the hub plate 34. The hub plate 34 has peripheral flanges 40 extending at right angles from the hub side of the hub plate and peripheral flanges 42 extending at right angles from the other side of the hub plate. Hub plate 34 has a plurality of projections 44 extending from one side and a plurality of projections 46 extending from the other side. One blade assembly is positioned and supported by flanges 40 and projections 44, the other blade assembly is posi tioned and supported by flanges 42 and projections 46. The blade assemblies are secured to the hub plate 34 by welding or riveting. We prefer to electrically spot weld the blade assemblies to the hub plate 34 at several spaced points. If desired, the brazing procedure de- Patented July 14, 1959 scribed with reference to Figure 9 can be used to simultaneously braze the hub plate and the assembled blades on both sides of the hub plate into a unitary structure.
While we have described the foregoing preferred embodiments of our invention, we contemplate that many changes may be made without departing from the scope or spirit of our invention and we desire to be limited only by the claims.
We claim:
1. An assembly for incorporation in a centrifugal blower wheel comprising a plurality of blades, each of said blades having a vane portion and flanges extending from each end of the vane portion and lying in planes which are substantially at right angles to said vane portion, each of said flanges having a base portion and an outwardly oflset end portion, said base portions and said outwardly offset end portions having substantially circular indentations, the outwardly ofl'set end portions of the flanges of a blade receiving therebetween the base portions of the flanges of the next adjacent blade, with the substantially circular indentations of the end portions extending into the substantially circular indentations of the base portions.
2. In a centrifugal blower wheel the combination of a plurality of elongated blades, each of said blades having a vane portion of curved cross-section and flanges extending from each end of the vane portion and lying in planes Which are substantially at right angles to said vane portion, each of said flanges having a base portion, an outwardly offset end portion, and a shoulder portion between said base portion and said end portion, said shoulder portion having a curvature substantially the same as the curvature of said vane portion, said outwardly offset end portions of the flanges of a blade receiving therebetween the base portions of the flanges of the next blade, the base portions and the end portions of said flanges having nesting substantially circular indentations connecting said base portions of the flanges of one blade with the end portions of the flanges of the next blade and a continuous annular welding bead welded to said flanges at their outwardly facing sides.
3. An assembly for incorporation in a centrifugal blower Wheel comprising a plurality of elongated blades, each of said blades having a vane portion of curved cross section and flanges extending from each end of the vane portion and lying in planes which are substantially at right angles to said vane portion, each of said flanges having a base portion, an outwardly offset end portion, and a shoulder portion between said base portion and said end portion, said shoulder portion having a curvature substantially the same as the curvature of said vane portion, said outwardly oflset end portions of the flanges of a blade receiving therebetween the base portions of the flanges of the next blade, the base portions and the outwardly offset end portions of said flanges having nesting substantially circular indentations and providing a means pivotally connecting said base portions of the flanges of one blade with the outwardly offset end portions of the flanges of the next blade.
References Cited in the file of this patent UNITED STATES PATENTS 1,029,554 Neumayer June 11, 1912 1,745,854 Lawaczeck Feb. 4, 1930 2,044,028 Szekely June 16, 1936 2,231,062 Evans Feb. 11, 1941 2,258,231 Evans Oct. 7, 1941 2,336,231 Dodge Dec. 7, 1943 2,392,113 Anderson Jan. 1, 1946 2,458,041 Wessel Jan. 4, 1949 2,592,851 Beranek Apr. 15, 1952 2,632,397 Jandasek Mar. 24, 1953 2,711,285 Burrowes June 21, 1955 2,724,547 Abbott et a1 Nov. 22, 1955 FOREIGN PATENTS 12,347 Great Britain of 1901 759,514 Germany Apr. 9, 1953
US501484A 1955-04-15 1955-04-15 Centrifugal blower wheel structure Expired - Lifetime US2894681A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US501484A US2894681A (en) 1955-04-15 1955-04-15 Centrifugal blower wheel structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US501484A US2894681A (en) 1955-04-15 1955-04-15 Centrifugal blower wheel structure

Publications (1)

Publication Number Publication Date
US2894681A true US2894681A (en) 1959-07-14

Family

ID=23993754

Family Applications (1)

Application Number Title Priority Date Filing Date
US501484A Expired - Lifetime US2894681A (en) 1955-04-15 1955-04-15 Centrifugal blower wheel structure

Country Status (1)

Country Link
US (1) US2894681A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2988006A (en) * 1959-06-11 1961-06-13 John E Becker Fluid couplings
US3091384A (en) * 1960-03-17 1963-05-28 Torrington Mfg Co Blower wheel blade construction and method of assembly
US3107897A (en) * 1961-08-24 1963-10-22 Gen Electric Gas turbine nozzle and vane assembly
US3165258A (en) * 1963-04-04 1965-01-12 Lau Blower Co Blower
JPS5430515A (en) * 1977-08-10 1979-03-07 Hitachi Ltd Electric blower
JPS5450804U (en) * 1977-09-16 1979-04-09
EP0609871A1 (en) * 1993-02-04 1994-08-10 PUNKER GmbH & CO. Radial blower
WO1999064746A1 (en) * 1998-06-09 1999-12-16 Escola Del Treball Del Ripolles, Fundacio Sf Rotor for fans
US20150260201A1 (en) * 2014-03-11 2015-09-17 Revcor, Inc. Blower Assembly And Method
US11274677B2 (en) 2018-10-25 2022-03-15 Revcor, Inc. Blower assembly
US11644045B2 (en) 2011-02-07 2023-05-09 Revcor, Inc. Method of manufacturing a fan assembly

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB190112347A (en) * 1901-06-17 1902-06-17 Charles Algernon Parsons Improvements in and relating to Steam Turbine Blades.
US1029554A (en) * 1908-07-24 1912-06-11 Maximillian Neumayer Centrifugal pump or blower.
US1745854A (en) * 1926-12-18 1930-02-04 Worthington Pump & Mach Corp Rotary hydraulic machine, especially centrifugal pump
US2044028A (en) * 1935-07-18 1936-06-16 Bayley Blower Company Rotor for a blower
US2231062A (en) * 1939-01-07 1941-02-11 Torrington Mfg Co Centrifugal blower
US2258231A (en) * 1941-02-15 1941-10-07 Alden Milton Fuse holder
US2336231A (en) * 1941-02-14 1943-12-07 Adiel Y Dodge Hydraulic torque transmitting device
US2392113A (en) * 1944-07-22 1946-01-01 American Blower Corp Fan wheel
US2458041A (en) * 1945-07-14 1949-01-04 Utillity Appliance Corp Rotor
US2592851A (en) * 1950-04-10 1952-04-15 American Blower Corp Fan wheel
US2632397A (en) * 1949-02-10 1953-03-24 Chrysler Corp Rotor wheel
DE759514C (en) * 1940-04-10 1953-04-09 Aeg Blading produced by cutting a rolled profile for the guide wheels of turbines
US2711285A (en) * 1949-12-14 1955-06-21 Lau Blower Co Blower
US2724547A (en) * 1950-12-01 1955-11-22 Utility Appliance Corp Blower wheel

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB190112347A (en) * 1901-06-17 1902-06-17 Charles Algernon Parsons Improvements in and relating to Steam Turbine Blades.
US1029554A (en) * 1908-07-24 1912-06-11 Maximillian Neumayer Centrifugal pump or blower.
US1745854A (en) * 1926-12-18 1930-02-04 Worthington Pump & Mach Corp Rotary hydraulic machine, especially centrifugal pump
US2044028A (en) * 1935-07-18 1936-06-16 Bayley Blower Company Rotor for a blower
US2231062A (en) * 1939-01-07 1941-02-11 Torrington Mfg Co Centrifugal blower
DE759514C (en) * 1940-04-10 1953-04-09 Aeg Blading produced by cutting a rolled profile for the guide wheels of turbines
US2336231A (en) * 1941-02-14 1943-12-07 Adiel Y Dodge Hydraulic torque transmitting device
US2258231A (en) * 1941-02-15 1941-10-07 Alden Milton Fuse holder
US2392113A (en) * 1944-07-22 1946-01-01 American Blower Corp Fan wheel
US2458041A (en) * 1945-07-14 1949-01-04 Utillity Appliance Corp Rotor
US2632397A (en) * 1949-02-10 1953-03-24 Chrysler Corp Rotor wheel
US2711285A (en) * 1949-12-14 1955-06-21 Lau Blower Co Blower
US2592851A (en) * 1950-04-10 1952-04-15 American Blower Corp Fan wheel
US2724547A (en) * 1950-12-01 1955-11-22 Utility Appliance Corp Blower wheel

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2988006A (en) * 1959-06-11 1961-06-13 John E Becker Fluid couplings
US3091384A (en) * 1960-03-17 1963-05-28 Torrington Mfg Co Blower wheel blade construction and method of assembly
US3107897A (en) * 1961-08-24 1963-10-22 Gen Electric Gas turbine nozzle and vane assembly
US3165258A (en) * 1963-04-04 1965-01-12 Lau Blower Co Blower
JPS5430515A (en) * 1977-08-10 1979-03-07 Hitachi Ltd Electric blower
JPS5732759B2 (en) * 1977-08-10 1982-07-13
JPS5450804U (en) * 1977-09-16 1979-04-09
JPS6026238Y2 (en) * 1977-09-16 1985-08-07 三菱電機株式会社 Multi-blade blower impeller
EP0609871A1 (en) * 1993-02-04 1994-08-10 PUNKER GmbH & CO. Radial blower
WO1999064746A1 (en) * 1998-06-09 1999-12-16 Escola Del Treball Del Ripolles, Fundacio Sf Rotor for fans
ES2153282A1 (en) * 1998-06-09 2001-02-16 Escola Del Trebal Del Ripolles Rotor for fans
US11644045B2 (en) 2011-02-07 2023-05-09 Revcor, Inc. Method of manufacturing a fan assembly
US20150260201A1 (en) * 2014-03-11 2015-09-17 Revcor, Inc. Blower Assembly And Method
US9995316B2 (en) * 2014-03-11 2018-06-12 Revcor, Inc. Blower assembly and method
US11274677B2 (en) 2018-10-25 2022-03-15 Revcor, Inc. Blower assembly
US11732730B2 (en) 2018-10-25 2023-08-22 Revcor, Inc. Blower assembly

Similar Documents

Publication Publication Date Title
US2894681A (en) Centrifugal blower wheel structure
US3298444A (en) Turbine impeller assembly
US2242586A (en) Method of making blowers
US3211364A (en) Blower wheel
US3225422A (en) Method of fabricating centrifugal fan impellers
US4329118A (en) Centrifugal blower wheels
US2231062A (en) Centrifugal blower
US1938382A (en) Method of manufacturing nozzle diaphragms and the like
US2431647A (en) Centrifugal fan
US2884187A (en) Centrifugal blower wheel
US2470966A (en) Rotor
US2932489A (en) Trussed radiator core-unit
US2344444A (en) Construction of turbomachines
US2079473A (en) Nozzle diaphragm and the like and method of making the same
US3004326A (en) Support structure and method for making a blower wheel
US3659959A (en) Air fan impeller blade assembly
US2915239A (en) Blower
US2662686A (en) Fan wheel
US3021591A (en) Method of making blower rotor
US2628769A (en) Blower
JPS5992746A (en) Commuttor for electric machine
US2701120A (en) Turbine blade construction with provision for cooling
US2714485A (en) Blower rotor construction
US2117107A (en) Turbine blade lashing
US4053260A (en) Double spider stiffening assembly for fan blades