US1052291A - Centrifugal blower-wheel. - Google Patents

Centrifugal blower-wheel. Download PDF

Info

Publication number
US1052291A
US1052291A US63824211A US1911638242A US1052291A US 1052291 A US1052291 A US 1052291A US 63824211 A US63824211 A US 63824211A US 1911638242 A US1911638242 A US 1911638242A US 1052291 A US1052291 A US 1052291A
Authority
US
United States
Prior art keywords
shaft
wheel
blades
hub
slots
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
US63824211A
Inventor
Charles Head Smoot
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.)
RATEAU BATTU SMOOT Co
Original Assignee
RATEAU BATTU SMOOT 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 RATEAU BATTU SMOOT Co filed Critical RATEAU BATTU SMOOT Co
Priority to US63824211A priority Critical patent/US1052291A/en
Application granted granted Critical
Publication of US1052291A publication Critical patent/US1052291A/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
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/006Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps double suction pumps
    • 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
    • Y10T29/49316Impeller making
    • Y10T29/49329Centrifugal blower or fan

Definitions

  • ' object of the invention is the production of such a rotary element especially adapted for operation at very high speeds.
  • such a rotary element has comprised as essential elements a shaft, radially extending blades or vanes, and a hub separate from but surrounding the shaft and serving to connect the blades or vanes to the shaft.
  • a hub separate from but surrounding the shaft and serving to connect the blades or vanes to the shaft.
  • the rotary element constructed in accordance with the resent invention is inherently capable of sa e operation at higher speeds than, and possessesmarked advantages over, the construction with separate hub and shaft elements heretofore employed, as is hereinafter explained.
  • Figure 1 is a horizontal sectional elevation of a compressorhaving a single wheel with two inlets for the fluid to be compressed.
  • Fig. 2 is a transverse section through the shaft, illustrating the manner in which the blades are attached to the shaft.
  • Figs. 3 and 4 are side and end elevations, respectively, of one of the blades,
  • Fig. 5 is a section of the shaft taken similarly to Fig. 2 but on a larger scale, and with, all of the blades removed.
  • C represents the stationarycasing or framework element of the compressor.
  • C and C represent the ducts by which the fluid to be compressed enters the compressor, t e fluid passing from these ducts into the wheel chamber through the central openings 0 At its periphery the Wheel chamber opens to the customary volute discharge passage 0 from which leads the discharge duct C of the compressor.
  • the framework is provided with bearings C and C for the shaft R of the rotary element, and O represents a coupling memher by means of which the compressor may be connected to and driven by a suitable power device such as ,a turbine.
  • the blades R of the compressor wheel are received in axial undercut slots R formed in the enlarged central portion of the shaft R the blades being enlarged at their bases to fit the slots R, as shown clearly in Fig. 2.
  • Sections R providing curved guide surfaces for the fluid passing into the compressor wheel, are secured'by-screws R to the teeth R between the slots R of the shaft B.
  • These guide sections R in the assembled wheel unite to form what may be regarded as a ring sur 'ounding the shaft and slotted to receive the lades R R and R represent nuts threaded on to the portionsof the shaft R at the opposite ends of the slotted portion and serving to hold the blades R against axial movement with respect to the shaft.
  • each blade R decreases as the distance from the base of the blade increases, thus giving more metal to hold the blade in place at its base where the centrifugal strain is the greatest.
  • the invention is not limited to use in blowers in which the shaft carries a single wheel as a pluralityof wheels may be formed on a single shaft by lengthening the latter and inserting in each 3 and 4, the crossslot R several blades, thus building up several wheels on a single shaft.
  • the increase in critical shaft speed obtained by following this plan is due both to the increase in stiffness of the shaft and to the decrease in the weight of the wheel.
  • the decrease in the diameter of the hub portion of the shaft enables me to decrease the diameter of the inlet openings 0 to the wheel chamber, while at the same time securing the desirably large cross-section of the annular space between the hub portion of the shaft and the outer margin of the inlet openings C necessary for the efiicient influx of the maximum quantity of air desired to be passed into the wheel chamber.
  • the increased radial blade depth in a wheel of given diameter thus obtained increases the efliciency of the machine and desirably increases the delivery pressure of the fluid compressed by the wheel, which it is possible to obtain with a wheel of given diameter operated at a given speed.
  • ahigh speed rotary pump the combination with a casing formed with an impeller wheel chamber having a peripheral outlet and an axial intake, and having impeller shaft bearings at opposite sides of said chamber, of an impeller comprising a shaft journaled in said bearings and formed between them with an axially slotted integral hub enlargement, and impeller blades secured at their bases in the slots of said hub enlargement and extending into said wheel chamber.

Description

G. H. SMOOT.
GENTRIPUGAL BLOWER WHEEL.
APPLICATION FILED JULY 13,1911.
Patented Feb. 4, 1913.
INVENTOR.
a STATES PATENT orricn.
I CHARLES HEAD SMOOT, OF NEW YORK, N. Y., ASSIGNOB TO RATEAU BAT'IU SMOO'I.
COMPANY, OF NEW YORK, N. Y.
' CENTB-IFUGAL BLOWER-WHEEL.
Specification of Letters Patent.
Patented Feb. 4:, 1913.
Application filed July 13, 1911. Serial No. 338,5242:
' object of the invention is the production of such a rotary element especially adapted for operation at very high speeds. Heretofore,
. such a rotary element has comprised as essential elements a shaft, radially extending blades or vanes, and a hub separate from but surrounding the shaft and serving to connect the blades or vanes to the shaft. With my present invention 1 dispense with the hub as an element separate from the shaft and secure the blades in axial slots formed in the shaft proper. The latter may advantageously be enlarged in circumference at what I may call the hub portion where the axial blade receiving slots are formed.
The rotary element constructed in accordance with the resent invention is inherently capable of sa e operation at higher speeds than, and possessesmarked advantages over, the construction with separate hub and shaft elements heretofore employed, as is hereinafter explained.
.:' The various features of novelty which characterize my invention are pointed out with particularity in the claims annexed to and forming a part of this specificat om For a better understanding of the lnvention,
however, and the" advantages possessed by it, reference should be had to the .accorn pa'nyin'g drawings and'descriptlve matter 1n which I have illustrated and described forms in which my invention may be embodied.
Of the drawings, Figure 1 is a horizontal sectional elevation of a compressorhaving a single wheel with two inlets for the fluid to be compressed. Fig. 2 is a transverse section through the shaft, illustrating the manner in which the blades are attached to the shaft. Figs. 3 and 4 are side and end elevations, respectively, of one of the blades,
and Fig. 5 is a section of the shaft taken similarly to Fig. 2 but on a larger scale, and with, all of the blades removed.
In the drawings, C, represents the stationarycasing or framework element of the compressor.
C and C represent the ducts by which the fluid to be compressed enters the compressor, t e fluid passing from these ducts into the wheel chamber through the central openings 0 At its periphery the Wheel chamber opens to the customary volute discharge passage 0 from which leads the discharge duct C of the compressor.
The framework is provided with bearings C and C for the shaft R of the rotary element, and O represents a coupling memher by means of which the compressor may be connected to and driven by a suitable power device such as ,a turbine.
The blades R of the compressor wheel are received in axial undercut slots R formed in the enlarged central portion of the shaft R the blades being enlarged at their bases to fit the slots R, as shown clearly in Fig. 2. Sections R providing curved guide surfaces for the fluid passing into the compressor wheel, are secured'by-screws R to the teeth R between the slots R of the shaft B. These guide sections R in the assembled wheel unite to form what may be regarded as a ring sur 'ounding the shaft and slotted to receive the lades R R and R represent nuts threaded on to the portionsof the shaft R at the opposite ends of the slotted portion and serving to hold the blades R against axial movement with respect to the shaft.
'As shown best by Figs. sectional area of each blade R decreases as the distance from the base of the blade increases, thus giving more metal to hold the blade in place at its base where the centrifugal strain is the greatest. By properly shaping the blades in this manner I can obtain a practically uniform stress at all points in the blades and which, even for very high speeds of rotation, can be brought within a practical working limit.
It will be apparent that the invention is not limited to use in blowers in which the shaft carries a single wheel as a pluralityof wheels may be formed on a single shaft by lengthening the latter and inserting in each 3 and 4, the crossslot R several blades, thus building up several wheels on a single shaft.
To appreciate the advantages of my invention it should be understood that it is desirable in many cases to make the speed or rotation as high as possible in machines of the kind described. The speed of rotation of such a machine is limited in general by the strength of the parts subjected to center, and is decreased by increasing the weight of the .shaft and the wheel supported by it. With the new construction the entire section of the metal of the shaft out -by a plane, as that indicated in Fig. 5 by the line AA, which passes axially through theshaft and intersects an opposed pair. of axial slots R is effective to resist the bursting tendency of the resultant centrifugal forces acting on,
or transmitted by the blades to the shaft. If the hub portion of the wheel and shaft are divided into separate hub and shaft elements, as by the cylindrical. surface indicated in Fig. 5 by the dotted circle B, only that portion of the metal cut by the plane A' A which lies on the outer side of the circle B, would be effective to resist the tendency of the centrifugal forces to burst the shaft apart along the plane AA. In other words, the centrifugal forces acting on or transmitted by the blades to the separate hub element of the machine would have to be borne entirely by the hub element and would not be transmitted to the shaft element surrounded by the hub.
With the construction described and claimed herein the stifiness of the shaft and its critical speed is markedly increased by .the portion of the shaft including the teeth R lying on the outer side of the cylindrical surface indicated in Fig. 5 by the circle B, whereas, if the hub portion of the shaft were divided into separate shaft and hub ele-. ments, as by said cylindrical surface, the
- construction disclosed herein is such that with the new construction a peripheral speed shaft and hub elements.
than that of the shaft proper, and is less than that of the hub element of prior wheels of the salne diameter. but having separate 7 By proceeding in this manner I am enabled to obtain a wheel having an increased capacity to resist centrifugal forces and having a higher critical shaft speed than is had with a wheel of the same diameter as heretofore constructed.
This obviously permits of a desirable increase in the speed of rotation of the wheel. The increase in critical shaft speed obtained by following this plan is due both to the increase in stiffness of the shaft and to the decrease in the weight of the wheel. Moreover, the decrease in the diameter of the hub portion of the shaft enables me to decrease the diameter of the inlet openings 0 to the wheel chamber, while at the same time securing the desirably large cross-section of the annular space between the hub portion of the shaft and the outer margin of the inlet openings C necessary for the efiicient influx of the maximum quantity of air desired to be passed into the wheel chamber.
The increased radial blade depth in a wheel of given diameter thus obtained increases the efliciency of the machine and desirably increases the delivery pressure of the fluid compressed by the wheel, which it is possible to obtain with a wheel of given diameter operated at a given speed.
WVhile in accordance with the provisions of the statutes I have illustrated and described the best forms of my invention now known to me, it will be apparent to those skilled in the art that changes maybe made in the form of the apparatus disclosed without departing from the spirit of my invention, and that under some conditions certain features of my invention may be used with advantage without a corresponding use of other features.
Having now described my invention what I claim as new and desire tosecure by Letters Patent is:
1. In ahigh speed rotary pump, the combination with a casing formed with an impeller wheel chamber having a peripheral outlet and an axial intake, and having impeller shaft bearings at opposite sides of said chamber, of an impeller comprising a shaft journaled in said bearings and formed between them with an axially slotted integral hub enlargement, and impeller blades secured at their bases in the slots of said hub enlargement and extending into said wheel chamber.
2., In a high speed rotary pump, the com-' .bination with a casing formed with an impeller wheel chamber having a peripheral outlet and an axial intake opening and having impeller shaft bearings at opposite sides of said chamber, of an impeller comprising a shaft extending through, but not filling,
said intake opening, and journaled in said In witness whereof, I have hereunto subbeanngs and formed between them withan scribed my name this 12th day of July integral hub enlargement having axially ex- A. D., 1911.
tending nndercut slots in its periphery and CHARLES HEAD SMOOT. impeller blades having ribbed bases anchored Witnesses: in said slots and extending into said Wheel GEORGE I. JOHNSTON,
chamber. L. BA'I'IIE.
US63824211A 1911-07-13 1911-07-13 Centrifugal blower-wheel. Expired - Lifetime US1052291A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US63824211A US1052291A (en) 1911-07-13 1911-07-13 Centrifugal blower-wheel.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US63824211A US1052291A (en) 1911-07-13 1911-07-13 Centrifugal blower-wheel.

Publications (1)

Publication Number Publication Date
US1052291A true US1052291A (en) 1913-02-04

Family

ID=3120552

Family Applications (1)

Application Number Title Priority Date Filing Date
US63824211A Expired - Lifetime US1052291A (en) 1911-07-13 1911-07-13 Centrifugal blower-wheel.

Country Status (1)

Country Link
US (1) US1052291A (en)

Cited By (4)

* 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
US4333278A (en) * 1979-09-24 1982-06-08 Wheelabrator-Frye Inc. Bladed centrifugal blasting wheel
US4480413A (en) * 1979-09-24 1984-11-06 Wheelabrator-Frye Inc. Bladed centrifugal blasting wheel
US20080286136A1 (en) * 2007-05-17 2008-11-20 Purvines Stephen H Fan housing

Cited By (4)

* 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
US4333278A (en) * 1979-09-24 1982-06-08 Wheelabrator-Frye Inc. Bladed centrifugal blasting wheel
US4480413A (en) * 1979-09-24 1984-11-06 Wheelabrator-Frye Inc. Bladed centrifugal blasting wheel
US20080286136A1 (en) * 2007-05-17 2008-11-20 Purvines Stephen H Fan housing

Similar Documents

Publication Publication Date Title
JPH0262717B2 (en)
US2641191A (en) Guide means on impeller for centrifugal pumps or blowers
US2233825A (en) Pump
GB712051A (en) Improvements in or relating to axial-flow fluid machines
US3394876A (en) Drum motor blade construction
US1663998A (en) Means for minimizing fluid pulsations
CN108930666A (en) Screw ventilation
US3876328A (en) Compressor with improved performance diffuser
US1614091A (en) Fan and fan blower
US1052291A (en) Centrifugal blower-wheel.
US1036627A (en) Rotary compressor.
US2362514A (en) Centrifugal compressor
US10077778B2 (en) Multistage centrifugal compressor
US1029554A (en) Centrifugal pump or blower.
US1629141A (en) Hydraulic pump
US984189A (en) Centrifugal and turbine pump and the like.
US2962206A (en) Centrifugal compressor for a gas turbine engine
US2372518A (en) Centrifugal type compressor
US1287367A (en) Centrifugal compressor.
US2423634A (en) Compressor
US1125118A (en) Compound blower.
US827750A (en) Blowing machinery.
US1041511A (en) Centrifugal compressor and pump.
GB191307783A (en) Turbine-pump or Compressor.
US874377A (en) Pump.