US1535417A - Open impeller - Google Patents

Open impeller Download PDF

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Publication number
US1535417A
US1535417A US724244A US72424424A US1535417A US 1535417 A US1535417 A US 1535417A US 724244 A US724244 A US 724244A US 72424424 A US72424424 A US 72424424A US 1535417 A US1535417 A US 1535417A
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United States
Prior art keywords
shaft
blades
groove
blade
hub
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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
US724244A
Inventor
Leslie R Huff
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.)
Ingersoll Rand Co
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Ingersoll Rand 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.)
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Publication date
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Priority to US724244A priority Critical patent/US1535417A/en
Application granted granted Critical
Publication of US1535417A publication Critical patent/US1535417A/en
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Expired - Lifetime legal-status Critical Current

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    • 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 blowers but more particularly to impellers for blowers of the 10 type in which the vanes or blades are opened or unshrouded.
  • One object of the invention is to secure the blades to the hub or shaft of the blower rigidly and securely in a simple and inex- 18 pensive manner.
  • Figure 1 is a longitudinal section of a blower in which the vanes are attached to the shaft in accordance with the practice of the invention
  • Figure 2 is a cross section through the impeller blades and shaft along the line 2-2 looking in the direction of the arrows,
  • Figure 3 is a perspective view of one of the vanes before insertion of the shaft, and.
  • Figure 4 is a longitudinal section of a blower having a double suction impeller with blades secured to the shaft and to each other in accordance with the invention.
  • the blower comprises a casing A of a'ny desired form, a shaft B extending through the casing having hubs O preferably formed integrally thereon to support impeller blades D.
  • Each of the hubs G is provided with a plurality of grooves E which are preferably dovetailed in form and extend longitudinally with respect to the shaft B.
  • Each of the blades D is formed with a. base F corresponding to the shape of the groove E.
  • the groove is cut in the arc of the circle and the base F of the blade is also constructed in the form of the arc of'a circle of the same radius as the groove E.
  • the blade D is adapted to be attached to the hub C by inserting the base 1924. Serial No. 724,244.
  • FIG 4 there is illustrated a modification in which the double suction impeller is provided with two sets of blades D inserted in the hubs G as in the modification shown in Figure 1.
  • the slots are here cut in alignment with each other and opposite to each other on the hub C and may be held in the grooves E by means of a plate G riveted to each, but the slots may be staggered if desired.
  • a blower comprising a shaft, a hub on the shaft having a circular groove in a plane extending longitudinally with respect to the shaft, a blade, and a base for said blade insertable in said groove and adapted to be held in the hub thereby.
  • a blower comprising a shaft, a hub formed thereon having a circular dovetailed groove in a plane extending longitudinally with respect to the shaft, a blade and a circular dove-tailed base on said blade adapted to be inserted in said groove and held therein by peening the ends of said groove.
  • a blower comprising a shaft, a hub on said shaft having opposite circular dovetailed grooves in alignment with each other and extending longitudinally with respect to the shaft, oppositely disposed impeller blades, a dove-tailed base for each of said blades insertable in said grooves, and means for clamping said blades together whereby said blades are held against removal from said grooves.

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

Description

L. R. HUFF OPEN IMPELLER April 28, 1925.
Filed July 5, 192 2 Sheets-Sheet 1 INVENTOR L sa'ellfluff Hi5 'ATT NEY Aprii 28, 1925;
' 1,535,417 L. R. HUFF OPEN IMPELLER Filed July 5, 1924 2 Sheets-Sheet 2 INVENTOR Leqlz'eRHaff HIS ATTOR Y Patented Apr. 28, 1925.
UNITED. STATES PATENT OFFlCE.
,LESLIE R. HUFF, OF PHILLIPSB'UR-G, NEW JERSEY, ASSIGNOR TO INGERSO'LL-RAND (lOMPANY, OF JERSEY CITY. NEW JERSEY, A CORPORATION OF NEW JERSEY.
OPEN IMPELLER.
Application filed July 5,
To all whom it may concern:
Be it known that I, LESLIE R. HUFF, a citizen of the United States, and a resident of Phillipsburg, county of Warren, and State of New Jersey, have invented a certain Open Impeller, of which the following is a specification accompanied by drawings.
This invention relates to blowers but more particularly to impellers for blowers of the 10 type in which the vanes or blades are opened or unshrouded.
One object of the invention is to secure the blades to the hub or shaft of the blower rigidly and securely in a simple and inex- 18 pensive manner.
Other, objects and advantages thereof will be in part obvious and in part pointed out in the following description in conjunction with the accompanying drawing in which,
Figure 1 is a longitudinal section of a blower in which the vanes are attached to the shaft in accordance with the practice of the invention,
Figure 2 is a cross section through the impeller blades and shaft along the line 2-2 looking in the direction of the arrows,
Figure 3 is a perspective view of one of the vanes before insertion of the shaft, and.
Figure 4 is a longitudinal section of a blower having a double suction impeller with blades secured to the shaft and to each other in accordance with the invention.
Referring toxthe drawings, the blower comprises a casing A of a'ny desired form, a shaft B extending through the casing having hubs O preferably formed integrally thereon to support impeller blades D. Each of the hubs G is provided with a plurality of grooves E which are preferably dovetailed in form and extend longitudinally with respect to the shaft B. Each of the blades D is formed with a. base F corresponding to the shape of the groove E.
In order to insert the base F of the blades into the dove-tailed groove E, the groove is cut in the arc of the circle and the base F of the blade is also constructed in the form of the arc of'a circle of the same radius as the groove E. The blade D is adapted to be attached to the hub C by inserting the base 1924. Serial No. 724,244.
into the groove E from the position shown in dotted lines in Figure 1 and rotating the blade to an upright position, generally perpendicular to the axis of the shaft B. With the blade in this position the ends of the groove E may be peened over to partly close the groove and prevent the blade from rotating. The circular shape of the base F stilfens the blade D and prevents looseness in the connection between the blade and the hub C.
In Figure 4 there is illustrated a modification in which the double suction impeller is provided with two sets of blades D inserted in the hubs G as in the modification shown in Figure 1. The slots are here cut in alignment with each other and opposite to each other on the hub C and may be held in the grooves E by means of a plate G riveted to each, but the slots may be staggered if desired. In order to remove the blades 1) from the grooves E, it is necessary to swing the blades in opposite directions, this being normally prevented by the plate Gr and also peening over the ends of the grooves E.
I claim:
1. A blower comprising a shaft, a hub on the shaft having a circular groove in a plane extending longitudinally with respect to the shaft, a blade, and a base for said blade insertable in said groove and adapted to be held in the hub thereby. 2. A blower comprising a shaft, a hub formed thereon having a circular dovetailed groove in a plane extending longitudinally with respect to the shaft, a blade and a circular dove-tailed base on said blade adapted to be inserted in said groove and held therein by peening the ends of said groove.
3. A blower comprising a shaft, a hub on said shaft having opposite circular dovetailed grooves in alignment with each other and extending longitudinally with respect to the shaft, oppositely disposed impeller blades, a dove-tailed base for each of said blades insertable in said grooves, and means for clamping said blades together whereby said blades are held against removal from said grooves.
for clamping said blades together whereby said blades are held against removal from said grooves.
In testimony whereof I have signed this specification.
LESLIE R. HUFF.
US724244A 1924-07-05 1924-07-05 Open impeller Expired - Lifetime US1535417A (en)

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US724244A US1535417A (en) 1924-07-05 1924-07-05 Open impeller

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445154A (en) * 1944-03-04 1948-07-13 Ingersoll Rand Co Blade mounting
US2469458A (en) * 1945-09-24 1949-05-10 United Aircraft Corp Blade form for supercharger impellers
US2483610A (en) * 1943-03-23 1949-10-04 Mini Of Supply Bladed impeller for turboblowers
US2582702A (en) * 1936-05-13 1952-01-15 Pangborn Corp Abrading apparatus
US2835320A (en) * 1954-07-21 1958-05-20 Cleaver Brooks Co Fan structure
US2848190A (en) * 1952-10-02 1958-08-19 Power Jets Res & Dev Ltd Radial flow turbo-machines
US2935296A (en) * 1951-12-26 1960-05-03 Gen Motors Corp Blade retaining means
US3071195A (en) * 1959-07-10 1963-01-01 Osmaston Ronald Propeller for outboard motor
US3175804A (en) * 1963-04-01 1965-03-30 Bendix Corp Radial-flow turbine safety
DE2558436A1 (en) * 1975-12-23 1977-07-07 Motoren Turbinen Union RADIAL BLADE FOR A TURBO ROTOR AND METHOD OF MANUFACTURING IT
US4047843A (en) * 1976-02-16 1977-09-13 Alfred Gutmann Gesellschaft Fur Maschinenbau Centrifugal impeller for sandblasting installations
US4483054A (en) * 1982-11-12 1984-11-20 United Technologies Corporation Method for making a drum rotor
US5632601A (en) * 1995-04-10 1997-05-27 Abb Research Ltd. Compressor
US20170306761A1 (en) * 2014-11-25 2017-10-26 Mitsubishi Heavy Industries, Ltd. Impeller and rotary machine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2582702A (en) * 1936-05-13 1952-01-15 Pangborn Corp Abrading apparatus
US2483610A (en) * 1943-03-23 1949-10-04 Mini Of Supply Bladed impeller for turboblowers
US2445154A (en) * 1944-03-04 1948-07-13 Ingersoll Rand Co Blade mounting
US2469458A (en) * 1945-09-24 1949-05-10 United Aircraft Corp Blade form for supercharger impellers
US2935296A (en) * 1951-12-26 1960-05-03 Gen Motors Corp Blade retaining means
US2848190A (en) * 1952-10-02 1958-08-19 Power Jets Res & Dev Ltd Radial flow turbo-machines
US2835320A (en) * 1954-07-21 1958-05-20 Cleaver Brooks Co Fan structure
US3071195A (en) * 1959-07-10 1963-01-01 Osmaston Ronald Propeller for outboard motor
US3175804A (en) * 1963-04-01 1965-03-30 Bendix Corp Radial-flow turbine safety
DE2558436A1 (en) * 1975-12-23 1977-07-07 Motoren Turbinen Union RADIAL BLADE FOR A TURBO ROTOR AND METHOD OF MANUFACTURING IT
US4047843A (en) * 1976-02-16 1977-09-13 Alfred Gutmann Gesellschaft Fur Maschinenbau Centrifugal impeller for sandblasting installations
US4483054A (en) * 1982-11-12 1984-11-20 United Technologies Corporation Method for making a drum rotor
US5632601A (en) * 1995-04-10 1997-05-27 Abb Research Ltd. Compressor
US20170306761A1 (en) * 2014-11-25 2017-10-26 Mitsubishi Heavy Industries, Ltd. Impeller and rotary machine
US10655470B2 (en) * 2014-11-25 2020-05-19 Mitsubishi Heavy Industries, Ltd. Impeller and rotary machine

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