US2654322A - Pump - Google Patents

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US2654322A
US2654322A US49403A US4940348A US2654322A US 2654322 A US2654322 A US 2654322A US 49403 A US49403 A US 49403A US 4940348 A US4940348 A US 4940348A US 2654322 A US2654322 A US 2654322A
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impellers
pump
vanes
impeller
point
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US49403A
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Horace W Olsen
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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
    • F04D11/00Other rotary non-positive-displacement pumps
    • F04D11/005Swash-type impeller pumps

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

Description

Oct. 6, 1953 H. w. OLSEN 2,654,322
I PUMP Filed Sept. 15, 1948 5 Sheets-Sheet l CO 0 O 0 C 3 o o O E 3 O o O fr uu u. H g o N I T 5) 2 &
H.-W. OLSEN I IN V EN TOR.
ATTORNEYS Oct. 6, 1953 H. w. OLSEN 2,654,322
PUMP
Filed Sept. 15, 1948 5 Sheets-Sheet 3 -H. W. OLSEN INVENTOR.
iii ,1] I NZ 7% ATTORNEYS Oct. 6, 1953 H. w. OLSEN 2,654,322
PUMP
Filed Sept. 15, 1948 5 Sheejcs-Sheet 4 fig. 6.
. 7 H. w. OLSEN NVENTOR Patented Oct. 6, 1953 UNITED STATES PATENT OFFICE.
PUMP
Horace W. Olsen, Houston; Tex. W Applicationseptember 15, 1.9 48,.S8l'ia1.NQ,49403 I 7 Claims. (01. 103-5) This. invention ie s. to im ro m n in pumps. and ater more nart tu alt y o pump employi r ta in aried im eller f r p its ne y tofluid and seal. assemb e p i adapted for such pumps.
lere qtore. P mps o th ty a included cen iu al a d. u bin t e pumps These t types. pump are a isia e y o a y urp s and; eachh s harac e is cs. that e best tted fo na tiqular ervices- F r instance, the centr fusal pumps useiul r a dl n hig umes nd hi h hea s P are n t desirable for ha dl n lu ds underqond tions h c high suction. i requi e On. th other hand, t r ne t ne pump ar ideal, qrhie u i lifts and have he hi hest ptst i al i t a t s o save: the l quid han lin umps, However, the turbine Pump. oi sm l apa en Qbiec Qithis inv n ion i to provide a pump hav ro ating rai d; imp l er wh h bi the characteristics of the turbine and centrifugal tim P11 311 enc er Qhie t is t P de a m having vaned impellers capable of pulling a high suction at the inlet and also capable of handling high olum s A. i r her o j c is to provide a pump having rotating vaned impellers which at the intake is Pr mar l a tu b ne yp p p a w c e discharge is principally but not entirely a cenrii g l PumP- Still another objectis to provide a device havng tati g a ed m l e s that y b used either as a pump or blower.
A still further object is to provide a device capable of acting as a pump or as a blower and employing two vaned impellers mounted for rotation on oblique axes whereby the vanes of one impeller mate closely with the vanes of the other impeller at one location along the peripheries thereof; and diverge from this point.
Even another o bject is to provide in pumps or blOWQ iS two impellers having a divergent mounting; wherein the vanes of one impeller mate with the-vanes of the other very closely at one location along their peripheries and the bodies of the impellei's at a point, diametrically opposed from the point of close mating of the vanes are at. their peripheries substantially two vane widths apart. Yet another object is to provide a device of the haracter described having two vaned imsubstantially divide'the spaces between the vanes of the other impeller.
Yet, a furth'erobject is to provide a device of the character described having two vaned impellers mounted divergently with their vanes, at least partially mating "and having means for maintaining the rotational relationship between the impellers such that vanes of one impeller substantially divide the spaces between the vanes of the other impeller, wherein lubricated mechanical seal assemblies are employed for providing seals about the impeller, the seal assemblies having a low component of sliding friction and a high component of rolling friction to enable the device to handle extremely high pumping fluid pressures with relatively small frictional losses due to the seal assemblies.
Other and further objects of this invention,
' Fig. 4 is a fragmentary view upon an enlarged scaleillustratihg the mounting of one f'theinn. peller discs in the pump casing,
Fig.5 is a top plan view of a modified-form of' impeller which may be used in accordance with this invention,
Fig. 6 is a view taken along the line 66 in Fig. 5 in the direction ofthe arrows,
Fig. 7 is a view taken'along the line 1'! in Fig. 6 in the direction of the arrows,
Fig. 8 is a top plan view of a modified form of impeller,
Fig. 9 is a view taken along the line 5-4 in Fig. 3 in the direction of the arrows,-
Fig. 10 is a fragmentary view on an enlarged scale illustrating the seal assembly for an impeller shaft, and
Fig. 11 is a view taken along the line ll--ll in Fig. 10 in the direction of the arrows;
Referring to the drawings, in Fig. l the pump is shown in elevation and consists of a casing made up of two parts l5 and I6 having facing flanges held together by bolts ll. In thefigures the pump is shown in a plurality or two stages but it is to be understood that the pump may be 3 constructed with a single stage or additional stages.
Fitting 18 serves as the inlet for the pump and has a flange to facilitate coupling of the pump in a fiow line. Fitting i9 is the discharge for the first stage and connects with fitting 20 which is the inlet for the second stage. Fitting 2| is the discharge of the pump.
Referring to Fig. 2 it is seen that the pump may be considered as having a driving section including shaft 22 and a pump section made up of a plurality of vaned impellers. The pump section will be first described.
The pump section of the device is made up of a plurality of vaned impellers 23 which are mounted for rotation in recesses formed in casing members l and [6. The impellers closely fit the casing recess walls which may be surface hardened. The two impellers 23 are mounted on stub shafts 25 which are journaled in recesses in the casing sections l5 and It by ball bearings including races 26 and 21. To provide a seal between the casing and shaft 25 a novel seal assembly, detailed in Figs. and 11, is used comprising a plurality of thin, wafer-like discs 28 of metal or other suitable material mounted in overlapping relation relative to each other between an inner race 29 and outer races 30. These discs are adapted to roll within the races upon relative rotationalmovement between the race rings. The outer races 30 have holes or grooves 32 to admit lubricant to the discs. Preferably these lubricant grooves 32 are equipped with Alemite fittings or the like to retain the lubricant under pressure higher than the pressures to be developed within the pump. These discs 28 may be fabricated from steel, bronze or the like with thicknesses ranging between .007" to .009". The thinner the discs the more effectively they will seal high pressures, but they are more expensive and th thicker discs are used where possible.
The mounting of impeller 24 is similar to that, of impeller 23 and the mounting of th pair of impellers is such that the two impellers are opposed. The axes of these impellers are on oblique lines relative to one another so that the vanes 23a and 24a closely mate at one position along th periphery of the impellers and the peripheral edges of the impellers diametrically opposed to the point of closest approach are substantially two vane widths apart. The vanes 23a and 24a of the impellers are preferably volute vanes as shown clearly in Fig. 3 and the vanes of impeller 23 are preferably held in the center of the spaces between vanes 24a.
The relationship between the divergence of the impellers and the position of the intake and discharge of the pump is best shown in Fig. 3. The impeller 23 is adapted to rotate clockwise as seen in this figure and the point of greatest divergence of the impellers is at the left at the meeting of the sections and it of the pump housing. The intake port 46 in section It preferably is along a volute line and extends from the point of greatest divergence in a counterclockwise direction over substantially a quadrant of. the impellers. The intake communicates directly with the peripheries of the impellers and the cross-sectional area of the intake diminishes as the divergence of the impellers increases.
The discharge port 41 of the pump unit is also formed in a volute line and extends from a point adjacent the greatest divergence of th impellers to a point adjacent the point of closest proximity between the peripheries of the impellers.
4 Th cross-sectional area of the discharge port iricreases as the distance between the impellers decreases.
Referring now to the drive for the impellers, a single prime mover not shown in th drawings may be employed to power all of the impeller units of the pump. Also it is contemplated that a plurality of power units may be employed to drive the impellers of the various pump units.
Where the drive for the pump is to be as that shown in the drawings a single drive shaft 22 extends longitudinally through the pump and resides within a longitudinal recess formed between casing sections I5 and Hi. This shaft is journalled with a plurality of ball-bearing races 34 and carries a plurality of gears 35. These gears are mounted for rotation within recesses in the casing and mesh with gears 36 carried by stub shafts 25. With this arrangement the rotation of each impeller relative to the other impellers depends upon the ratio of the gearing and for most. purposes it is preferred that this ratio be the same in each instance, and in any case the ratio should be the same for the pumps of each unit of the multi-stage pump.
The shaft 22 may be sealed at both ends of the pump casing by any suitable seal arrangement. A novel seal assembly that is especially adapted for this use is similar to that shown in conjunction with the seals for shafts 25. As shown in Fig. 2 this seal assembly includes an inner race 31 and an outer race 38 similar to race 30, a plurality of the seal wafers or discs 28 are mounted within the races and perform in the same manner as described for th seals about shafts 25. Usually the pressures to be sealed against are not great and a single annular arrangement of discs 28 is sufficient to give a satisfactory seal. Covers 39 are provided for the seal and where the shaft extends from both ends of the pump housing the two covers have central apertures to accommodate the shaft. The covers have a tight fit on the annular beveled portion 40 of the casings.
The single row seal assembly is detailed in Fig. 4 and is entirely satisfactory for sealing the journal of a rotating shaft against low pressures.
In operation the pump is connected in a flow line, the intake l8 being connected with the source of material to be pumped and the discharge 2! being connected to the discharge portion of the line. The prime mover, not shown in the drawings, is started and due to a drive connection with shaft 22 the shaft is driven and the impellers in turn are driven by the engaging gears 35 and 3E. The direction of rotation of each of the impellers 23 and 24 is the same and impeller 23 shown in Fig. 3 is rotated in a clockwise direction. It has been found that the intake of the pump need not communicate with the center of the impellers but may communicate directly with the peripheries of the impellers. The exact action which takes place within the impellers is not known but it has been found that there is suflicient suction at the periphery to draw the fluid from the intake to the space between the impellers. It is believed that this suction is the result of the vortex created between the rotating impeller blades of the impellers. At the location where the intake communicates with the peripheries of the impellers the impellers are relatively far apart and the action of the impellers impacting the fluid is very similar to that which takes place within the turbine type pumps. At any rate, it has been found that a 5 comparatively large suction head may be lifted and that the pump need not be primed inoperation. I A. centrifugal efiect ishad at the discharge ;.Q 'the, inpeed dila e l ev arrangement ofv the impeller vanes added impact is given to the fluid imparting energy thereto. Also the divergence of th'impellersis. such that as the centrifugal effect is imparted to'the fluid being pumpedthe space'between the impellers is increasingly dimmished and this imparts additional energy to the fluid.
a. relatively great suction head must belifted.
The pump imparts a very high velocity to noncompressible fluids or is capable of compressing toward the point of closest proximity of the peripheries of the impellers. The effect of this is a progressively closing wedge-shaped space formed between the vanes as the cross-sectional area of the discharge increases.
In Figs. 5 and 6 a modified type impeller is shown at 4!. This impeller has a series of volute vanes formed by the volute ribs 42. These ribs have valleys 43 therebetween which are slightly larger than ribs 42 allowing opposing impellers to mate closely at one position along the periphery of the impellers similar to the engagement of the impellers shown in Fig. 2. These modified impellers are especially adapted for use where high velocity is to be imparted to a hydraulic material or where the device is to be used as a compressor.
In the modified impellers 44 shown in Figs. 8 and 9 the vanes 44 extend radially. In this type of impeller many more vanes can be readily provided and this is an advantage in some instances. In any case it is desirable to use as high a number of vanes as possible as this increases the suction pull at the intake.
An enlarged view of the seal for shaft 26 is shown in Figs. 10 and 11. This seal includes three races 29, and 3| having opposed grooves therein forming a space substantially elliptical in cross-section. Lodged within these grooves are a plurality of seal discs which are circular and shown at 28. These discs are relatively thin and upon rotation of shaft 26 are adapted to roll along the groove with their edges contacting the wall of the groove and tend to align in the groove whereby the side surfaces of adjacent discs are held in close abutment one with the other. These discs provide a substantial seal for the journaling of the shaft.
From the foregoing it will be seen that this invention is one well adapted to obtain all of the ends and objects hereinabove set forth together with other advantages which are obvious and which are inherent to the structure.
It will be understood that certain features and sub-combinations are of utility and may be employed without reference to other features and sub-combinations. This is contemplated by and is within the scope of the claims.
As many possible embodiments may be made of the invention without departing from the scope thereof, it is to be understood that all matter herein set forth as shown in the accom panying drawings is to be interpreted as illustrative and not in a limiting sense.
Having described my invention, I claim:
1. A pump, comprising a casing, two opposed impellers'consisting, of discs having. vanes rigidly mounted on their adjacentfaces, said impellers mounted for rotation within the casing. about oblique axesand approaching each, other at one :point of their peripheries to'closely intermesh the vanes, said impellers diverging from. each other. from said one point to a, diametrically opposed point of their peripheries, said impellers beingspaced apart at their axes to provide. fluid communication between said points, an inlet opening in the casing at the peripheries of the impellers. beginning at the point of greatest divergency of the impellers and extending circumferentially over a portion of the impellers in a direction opposite to the impellers rotational direction, a discharge opening in the casing atthe peripheries of the impellersbeginning at the point of closest approach of said impellers and extending circumferentially over a portion of the impellers in a direction opposite to the impellers rotational direction, and drive means for rotating the impellers.
2. A pump as in claim 1 wherein the impeller vanes extend along convolute lines trailing the direction of rotation of the impellers.
3. A pump as in claim 1 wherein the number of vanes approximate that of a turbine impeller.
4. A pump as in claim 1 wherein the vanes are in the form of convolute corrugations.
5. A pump comprising a casing, two opposed impellers consisting of discs having vanes rigidly mounted on their adjacent faces, said impellers mounted for rotation within the casing about oblique axes and approaching each other at one point of their peripheries to closely intermesh the vanes, said impellers diverging from each other from said one point to a diametrically opposed point of their peripheries, said impellers being spaced apart at their axes to provide fluid communication between said points, an inlet opening in the casing at the peripheries of the impellers beginning at the point of greatest divergency of the impellers and extending circumferentially over a portion of the impellers in a direction opposite to the impellers rotational direction, a discharge opening in the casing at the peripheries of the impellers beginning at the point of closest approach of said impellers and extending circumferentially over a portion of the impellers in a direction opposite to the impellers rotational direction, the said inletand discharge openings formed along convolute lines, the inlet decreasing in cross-sectional area in the direction of rotation of the impellers and the discharge increasing in cross-sectional area in the direction of rotation of the impellers, and drive means for rotating the impellers.
6. A pump comprising a casing, two opposed impellers consisting of discs having vanes rigidly mounted on their adjacent faces, said impellers mounted for rotation within the casing about oblique axes and approaching each other at one point of their peripheries to closely intermesh the vanes, said impellers diverging from each other from said one point to a diametrically opposed point of their peripheries, said impellers being spaced apart at their axes to provide fluid communication between said points, the angle between the impeller axes being such that the vanes at the point of closest approach of the impellers have close tolerance with the discs portion of the opposed impeller and at the point of greatest divergence the discs portions of the impellers are substantially two vane widths apart, an inlet opening in the casing at the peripheries of the impellers beginning at the point of greatest divergency of the impellers and extending circumferentially over a portion of the impellers in a. direction opposite to the impellers rotational direction, a discharge opening in the casing at the peripheries of the impellers beginning at the point of closest approach of said impellers and extending circumferentially over a portion of the impellers in a direction opposite to the impellers rotational direction, and drive means for rotating the impellers.
7. A pump as in claim 6 wherein a plurality of the pump units recited are interconnected to provide a multi-stage pump, the inlets of all but the first unit connected to the discharge of the preceding unit of the series, the inlet of the first unit and the discharge of the last of the units being connectable to a service line.
HORACE W. OLSEN.
References Cited in the file of this patent UNITED STATES PATENTS Number Number Name Date Jones et a1 May 21, 1861 Maxson Mar. 7, 1876 Salomo Oct. 19, 1886 Kirby July 27, 1920 Woodruff Aug. 25, 1936 Montelius July 13, 1943 Walker Oct. 12, 1943 Piccardo Apr. 1, 1947 Mikulasek July 5, 1949 Davis Sept. 20, 1949 Clark Jan. 15, 1952 FOREIGN PATENTS Country Date Italy Oct. 17, 1929
US49403A 1948-09-15 1948-09-15 Pump Expired - Lifetime US2654322A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2831436A (en) * 1952-08-19 1958-04-22 Garvenswerke Maschinen Pumpen & Waagenfabrik W Garvens Pump
US2897761A (en) * 1955-12-30 1959-08-04 Virginia Burdick Roy Nutating propeller pump
US3012763A (en) * 1958-05-16 1961-12-12 Barmart Mixing machine
US3093961A (en) * 1960-02-09 1963-06-18 Pisa Pietro Ship propelling unit
US3411759A (en) * 1964-08-14 1968-11-19 Aluminum Lab Ltd Apparatus for splashing liquids
US6494698B2 (en) * 1997-08-21 2002-12-17 Felix Michael Arnold Rotary piston machine having cycloid teeth
WO2003055551A1 (en) * 2001-12-22 2003-07-10 Seleon Gmbh Radial compressor for respirators
RU2627753C2 (en) * 2015-11-02 2017-08-11 Евгений Геннадьевич Иванов Rotor hydro-pneumatic machine

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US32372A (en) * 1861-05-21 John jones
US174373A (en) * 1876-03-07 Improvement in rotary pumps and engines
US351129A (en) * 1886-10-19 Dale and john fraser
US1347512A (en) * 1919-04-10 1920-07-27 James B Kirby Pump
US2052155A (en) * 1933-06-12 1936-08-25 Frank M Strock Means for impelling and compressing gaseous fluids
US2324168A (en) * 1940-01-26 1943-07-13 Montelius Carl Oscar Josef Rotary compressor or motor
US2331641A (en) * 1941-01-21 1943-10-12 Jack E Walker Shaft sealing means for pumps
US2418194A (en) * 1944-04-19 1947-04-01 Shasta Pump Company Sealing means for submersible electric motor-pump units
US2475247A (en) * 1944-05-22 1949-07-05 Mikulasek John Planetary piston fluid displacement mechanism
US2482325A (en) * 1947-09-23 1949-09-20 Davis Oscar Newton Spherical air compressor
US2582413A (en) * 1945-07-20 1952-01-15 James M Clark Expansible chamber rotary fluid displacement device

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US32372A (en) * 1861-05-21 John jones
US174373A (en) * 1876-03-07 Improvement in rotary pumps and engines
US351129A (en) * 1886-10-19 Dale and john fraser
US1347512A (en) * 1919-04-10 1920-07-27 James B Kirby Pump
US2052155A (en) * 1933-06-12 1936-08-25 Frank M Strock Means for impelling and compressing gaseous fluids
US2324168A (en) * 1940-01-26 1943-07-13 Montelius Carl Oscar Josef Rotary compressor or motor
US2331641A (en) * 1941-01-21 1943-10-12 Jack E Walker Shaft sealing means for pumps
US2418194A (en) * 1944-04-19 1947-04-01 Shasta Pump Company Sealing means for submersible electric motor-pump units
US2475247A (en) * 1944-05-22 1949-07-05 Mikulasek John Planetary piston fluid displacement mechanism
US2582413A (en) * 1945-07-20 1952-01-15 James M Clark Expansible chamber rotary fluid displacement device
US2482325A (en) * 1947-09-23 1949-09-20 Davis Oscar Newton Spherical air compressor

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2831436A (en) * 1952-08-19 1958-04-22 Garvenswerke Maschinen Pumpen & Waagenfabrik W Garvens Pump
US2897761A (en) * 1955-12-30 1959-08-04 Virginia Burdick Roy Nutating propeller pump
US3012763A (en) * 1958-05-16 1961-12-12 Barmart Mixing machine
US3093961A (en) * 1960-02-09 1963-06-18 Pisa Pietro Ship propelling unit
US3411759A (en) * 1964-08-14 1968-11-19 Aluminum Lab Ltd Apparatus for splashing liquids
US6494698B2 (en) * 1997-08-21 2002-12-17 Felix Michael Arnold Rotary piston machine having cycloid teeth
WO2003055551A1 (en) * 2001-12-22 2003-07-10 Seleon Gmbh Radial compressor for respirators
DE10296120B4 (en) * 2001-12-22 2015-01-22 Tni Medical Ag Radial compressor for ventilators
RU2627753C2 (en) * 2015-11-02 2017-08-11 Евгений Геннадьевич Иванов Rotor hydro-pneumatic machine

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