US2628568A - High-pressure pump - Google Patents

High-pressure pump Download PDF

Info

Publication number
US2628568A
US2628568A US665268A US66526846A US2628568A US 2628568 A US2628568 A US 2628568A US 665268 A US665268 A US 665268A US 66526846 A US66526846 A US 66526846A US 2628568 A US2628568 A US 2628568A
Authority
US
United States
Prior art keywords
stator
pockets
blades
rotor
disk
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
US665268A
Inventor
Marvin L Rhine
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.)
ELLIPSE Corp
Original Assignee
ELLIPSE CORP
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=24669418&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=US2628568(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by ELLIPSE CORP filed Critical ELLIPSE CORP
Priority to US665268A priority Critical patent/US2628568A/en
Application granted granted Critical
Publication of US2628568A publication Critical patent/US2628568A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • F01C21/0809Construction of vanes or vane holders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/34Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
    • F04C2/344Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F04C2/3446Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface
    • F04C2/3447Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface the vanes having the form of rollers, slippers or the like

Definitions

  • My present invention relates to a. high pressure pump for fluids, that is, either liquid orgas.
  • One object of theinvention is to provide a pump in which a rotor rotates in a stator, the stator cavity being elliptical in shape and the rotor having pockets inwhich blades reciprocate radially with their outer ends following the wall of the stator cavity.
  • Another object is to provide, a high pressure pump including a number of rotor units in the form of disks, each surrounded by a stator unit also in the form of a disk with separator disks between the rotor andv stator disks, the stator disks being provided with inlet and outlet passageways arranged so that any number of the disks can be stacked and the. resulting assembly will constitute a hi h pressure pump when the disks are connected together between end plates and the rotor units will be in series.
  • a further object. is to, provide rotor pockets of characteristic shape and inclination, and to provide blades mounted therein of complementary shape to reciprocate in the pockets and effect intake of fluid at opposite points in the stator and displacement of fluid at intermediate opposite points whereby rotation of the rotor disks produces pumping action, the arrangement of the units in series producing high pressures unattainable by. means of single units, and a greater number of units effecting higher pressure so thatthe desired pressure may b securedby utilizing the proper number of units.
  • Still a further object is. to provide modified forms of rotor blades particularly adaptable for certain types of fluids and having certain structural details which increase their efficiency and improve the pumping action.
  • Figure l is a sectional view through a high pressure pump embodying; my present invention.
  • Figure 2 is a sectional view on the line 2-2 of the Figure 1, Figure 1 being a sectional View on,
  • Figure 3 is asectional view on the line 3.--3 of' Figure 1.
  • Figure 4 is a sectional view on the line.4+.4 of.
  • Figure 5 is an exploded perspectivev viewof' two of the stator disks and two of the separator disks to show the relation. of the passageways. and portsin them.
  • Figures 6, 7 and 8 are views similar to Figure 2 l showing modified forms of rotor blades.
  • Figure 9 is a perspective viewof another modi'- fertil form of blade.
  • Figure 16 is a sectional viewonthe line 10-40.
  • Figure 11 is a sectional View showingafurther modified form of rotor-pocket and blade shape
  • separator disks [4 with four statordisks. lfiine terposed between them, and an end plate l8.
  • A. shaft 28 is. journaled in bearings 22.and24. which bearings are carried by the, end. plates .12
  • Each stator disk has a stator cavity 31 which,
  • the stator disk has in one side face thereof, radial inlet passages 40 and in the opposite side face, radial outlet passages 42.
  • stator disks 16 have their inlet passages at 90 degrees Qr the;
  • the separator disks I4 are then providedwithi transfer passages, 44 for connecting the outlet passage 42 of onedisk to the inlet'passage 40 of,
  • The. end. plate It has. a pair or; opposite: inlet While. I have illustrated:
  • ports 46 connected with an intake boss 48 and with each other by a passageway 50 (see Figure 4), the ports 46 aligning with the passages 44 of the left hand separator disk l4 in Figure l.
  • the end plate I! is similar in construction having a pair of ports 52 connected together by a passageway 54 and with an outlet boss 56.
  • the dual arrangement of the ports 46 and 52 is not illustrated in Figure 1 because the lower half of the figure is taken on a section line at right angles to the upper half as indicated by the line l-l in Figure 2.
  • Figures 4 and however show the true arrangements on section lines directly through the pump.
  • packing 58 For sealing the shaft 20 against leakage, packing 58 is provided and suitable washers 60 and 62 are interposed between the packing and the bearing 22 and between the right hand separator disk l4 and the bearing 24 respectively.
  • the bearing 24 has a. sealed-in end and therefore requires no packing.
  • the rotor has a series of pockets each of which has a rear wall 64, a front wall 66 and an inner wall 68.
  • a blade 10 is mounted therein and is of substantially a complementary shape with respect to pocket. These blades move substantially radially in the pockets, being thrown outward by centrifugal force and by the pressure of the fluid in front of them which tend to crowd the blades back against the back walls 64 of the rotor pockets with the blades tilting so that their outer ends fit tightly against the inner face of the elliptical stator cavity 31.
  • FIG 8 illustrates a further modification in which each blade consists of two quarter circle parts 82 separated by a packing bar 84.
  • the blades of Figures 6 and 7 instead of being solid may be hollow as indicated at 86 in Figure 9, the blade of this figure being designated 88.
  • FIG 11 I show a rotor pocket and blade shape in which the blade is designated 90 and the pocket 92.
  • the portions 94 of the rotor between the pockets 92 are somewhat the shape of gear teeth and the blades 90 have a reverse shape for fitting all the way in the pockets at the minor axis of the ellipse 31.
  • This type rotor and blade are particularly adaptable for slow speed operation.
  • Fluid would enter from the inlet 48 and flow through the passageways 50 and 46 (see Figure 4) and through the openings 44 of the first separator disk [4. These openings are in alignment with the intake passageways 40 of the left hand stator disk I6 in Figure 5 so that the fluid can flow into the stator cavity from diametrically opposite points (see particularly Figure 2). At this position the blades 10 are outward in their pockets 68 thus enlarging the effective volume of the pockets and thereby drawing the fluid into the pockets.
  • my device While I have referred to my device as being a rotary pump obviously it may be a fluid driven motor or more generically a fluid displacement device as the structure is adaptable to both motors and pumps which are both fluid displacing devices.
  • the blades are so designed in shape that wear does not affect the sealing qualities of the blades in the rotor pockets. Upon wear occurring the blades merely assume a new working range farther out in the pockets without substantially changing the relationship of the blades to the pockets.
  • My stacking arrangement of the pump units obviously makes it possible to assemble from a few parts a high ressure pump having any desired operating pressure within certain limits.
  • the only modification required because of a change in size is a difierent length of tie rod 32.
  • a fluid displacement device comprising a stator having an out-of-round stator cavity, a rotor rotatable therein, said rotor having bladereceiving pockets, blades received therein for free movement relative to the pockets and radial movement relative to the stator cavity in order to contact the wall thereof, each of said blades being substantially a half-circle in cross-sectional shape, each of said pockets having a similar shaped bottom, said pockets being of substantially the same size as said blades to effect substantially complete displacement of fluid from said pockets in the seated positions of said blades.
  • a fluid displacement device comprising a stator having an out-of-round stator cavity, a rotor rotatable therein, said rotor having bladereceiving pockets, blades received therein for free movement relative to the pockets and radial movement relative to the stator cavity in order to contact the wall thereof, each of said blades being substantially a half-circle in cross-sectional shape, each of said pockets having a similar shaped bottom, said pockets being of substantially the same size as said blades to effect substantially complete displacement of fluid from said pockets in the seated positions of said blades, and a relief opening through each of said blades located between the front and rear faces of the blade and extending from the stator contactin face of the blade to the opposite face thereof to balance out excess pressure between said blade and said stator by conducting the fluid from the pocket, thus aiding said blade to follow the contour of said stator.
  • a rotary fluid displacement device comprising a stator having an out-of-round stator cavity, a rotor located therein, said rotor having blade-receiving pockets, a blade received in each of said pockets, each of said blades having contact at all times during operation with said stator and said rotor, in which the contact between the outer surface of the blade and the inner surface of the stator is area contact to prevent complete rotation of the blade in the pocket but permit it to rock therein with free movement in relation to said pocket, and the contact of a side of the blade with the rotor pocket being along a line which varies in position with respect to the blade and the pocket during operation and which acts as a pivot for the blade, the pivot action tending to keep the outer surface of the blade in said area contact with said stator during all positions of rotation of said rotor.

Landscapes

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

Description

Feb. 17, 1953 RHlNE 2,628,568
HIGH-PRESSURE PUMP Filed April 26, 1946 2 $HEETSSHEET 1 I as MARVIN L. RHINE INVENTOR.
ATT'YS Feb. 17, 1953 M. L. RHINE HIGH-PRESSURE PUMP 2 SHEETSSHEET 2 Filed April 26, 1946 Patented Feb. 17, 1953 HIGH-PRE S SURE PUMfP Marvin L. Rhine, Chicago, Ill., assignor to Ellipse Corporation, Chicago, 111., a. corporation. of
Illinois Application April 26, 1946, Serial No. 665,268"
3 Claims. 1
My present invention. relates to a. high pressure pump for fluids, that is, either liquid orgas.
One object of theinvention is to provide a pump in which a rotor rotates in a stator, the stator cavity being elliptical in shape and the rotor having pockets inwhich blades reciprocate radially with their outer ends following the wall of the stator cavity.
Another object is to provide, a high pressure pump including a number of rotor units in the form of disks, each surrounded by a stator unit also in the form of a disk with separator disks between the rotor andv stator disks, the stator disks being provided with inlet and outlet passageways arranged so that any number of the disks can be stacked and the. resulting assembly will constitute a hi h pressure pump when the disks are connected together between end plates and the rotor units will be in series.
A further object. is to, provide rotor pockets of characteristic shape and inclination, and to provide blades mounted therein of complementary shape to reciprocate in the pockets and effect intake of fluid at opposite points in the stator and displacement of fluid at intermediate opposite points whereby rotation of the rotor disks produces pumping action, the arrangement of the units in series producing high pressures unattainable by. means of single units, and a greater number of units effecting higher pressure so thatthe desired pressure may b securedby utilizing the proper number of units.
Still a further object is. to provide modified forms of rotor blades particularly adaptable for certain types of fluids and having certain structural details which increase their efficiency and improve the pumping action.
With these and other objects in view, my invention consists in the construction, arrangement and combination of the various parts of my pump whereby the objects contemplated are attained, as hereinafter more fully set forth, pointed out in my claims and illustrated in the accompanying drawings, wherein:
Figure l is a sectional view through a high pressure pump embodying; my present invention.
Figure 2 is a sectional view on the line 2-2 of the Figure 1, Figure 1 being a sectional View on,
the line-ll of Figure. 2 toshow both. inlet and outlet porting arrangements for. the series of pump units.
Figure 3 is asectional view on the line 3.--3 of'Figure 1.
Figure 4 is a sectional view on the line.4+.4 of.
Figure 2;
Figure 5 is an exploded perspectivev viewof' two of the stator disks and two of the separator disks to show the relation. of the passageways. and portsin them.
Figures 6, 7 and 8 are views similar to Figure 2 l showing modified forms of rotor blades.
Figure 9 is a perspective viewof another modi'- fled form of blade.
Figure 16 is a sectional viewonthe line 10-40.
of Figure l showing'the connectionofopposite ports with each other, and
Figure 11 is a sectional View showingafurther modified form of rotor-pocket and blade shape;
On the accompanying drawings I have 1 used the reference numeral Ill toindicate a mounting plate for my high pressure pump. Stacked against the mounting plate H] is an end plate l2,
a separator disk It, a stator disk [6, five other."
separator disks [4 with four statordisks. lfiine terposed between them, and an end plate l8.
A. shaft 28 is. journaled in bearings 22.and24. which bearings are carried by the, end. plates .12
bolts extend through openings, 36.0fthe disks l4 and l 6 (see FiguresA and 5) andiof course the end plates 12 and I8 are-similarlydrilledto-receive the tie bolts.
Each stator disk has a stator cavity 31 which,
is elliptical in outline as shown in Figure 2, its. minor diameter being substantially the same as the diameter of the rotor disk 30. The stator disk has in one side face thereof, radial inlet passages 40 and in the opposite side face, radial outlet passages 42. The passages 40-are circumferentially spaced 9G degrees from the passages.-
42 as shown in Figure 4 and alternate stator disks 16 have their inlet passages at 90 degrees Qr the;
outlet passage of one disk aligned with the inlet passage of the next adjacent disk.
The separator disks I4 are then providedwithi transfer passages, 44 for connecting the outlet passage 42 of onedisk to the inlet'passage 40 of,
the next adjacent disk and the transfer passages;
44 are therefore rotated90 de rees in, successive disks I4 as obvious from an-inspectionoillir ure 5.
The. end. plate; It has. a pair or; opposite: inlet While. I have illustrated:
ports 46 connected with an intake boss 48 and with each other by a passageway 50 (see Figure 4), the ports 46 aligning with the passages 44 of the left hand separator disk l4 in Figure l. The end plate I! is similar in construction having a pair of ports 52 connected together by a passageway 54 and with an outlet boss 56. The dual arrangement of the ports 46 and 52 is not illustrated in Figure 1 because the lower half of the figure is taken on a section line at right angles to the upper half as indicated by the line l-l in Figure 2. Figures 4 and however show the true arrangements on section lines directly through the pump.
For sealing the shaft 20 against leakage, packing 58 is provided and suitable washers 60 and 62 are interposed between the packing and the bearing 22 and between the right hand separator disk l4 and the bearing 24 respectively. The bearing 24 has a. sealed-in end and therefore requires no packing.
Referring to Figure 2, it will be noted that the rotor has a series of pockets each of which has a rear wall 64, a front wall 66 and an inner wall 68. A blade 10 is mounted therein and is of substantially a complementary shape with respect to pocket. These blades move substantially radially in the pockets, being thrown outward by centrifugal force and by the pressure of the fluid in front of them which tend to crowd the blades back against the back walls 64 of the rotor pockets with the blades tilting so that their outer ends fit tightly against the inner face of the elliptical stator cavity 31.
In pumping most liquids I find that centrifugal force and the pressure of the liquid holds the blades too tightly against the stator cavity wall and the back walls 64 of the rotor pockets. Therefore I incline the pockets from radial position so that there is a, tendency to pull the blades inwardly to counteract this pressure. The degree of inclination determines the degree of counteraction.
In the pumping of some fluids I find that blade shapes differing from those shown in Figure 2 are more desirable. For instance, in Figure 6 quarter circle blades 12 are illustrated wherein the rotor pockets have substantially fiat rear faces I4.
Where it is desirable to force the blades outwardly they may be substantially half circles as shown as IS in Figure 7.
When the pump blades (all types disclosed) are at their inward limits they drive all fluid out of the rotor pockets and to relieve the last of this fluid the blades may be provided with relief openings 18 as shown only in Figure 7. Another method is shown in Figures 8 and 9 in which relief grooves 80 are provided.
Figure 8 illustrates a further modification in which each blade consists of two quarter circle parts 82 separated by a packing bar 84. The blades of Figures 6 and 7 instead of being solid may be hollow as indicated at 86 in Figure 9, the blade of this figure being designated 88.
In Figure 11, I show a rotor pocket and blade shape in which the blade is designated 90 and the pocket 92. The portions 94 of the rotor between the pockets 92 are somewhat the shape of gear teeth and the blades 90 have a reverse shape for fitting all the way in the pockets at the minor axis of the ellipse 31. This type rotor and blade are particularly adaptable for slow speed operation.
In all forms of the blade as shown in Figures 2,
6, 7, 8, 9 and 11 there is a pocket formed ahead of the blade from which fluid is displaced in addition to being displaced from the major axis portion of the elliptical stator cavity 31. Thus the degree of eccentricity need not be very great as between the diameter of the rotor and the major axis of the stator cavity as the stator cavity is supplemented by the spaces ahead of the blades in the rotor pockets and the bottoms of the pockets. The resulting structure is a very efficient pump with considerable capacity in spite of small radial movement of the rotor blades.
Practical operation Referring specifically to the operation of my pump structure and considering particularly Figure 5 there would be first a separator disk H (in the position of the one at the left hand end of Figure 1) and this disk would be between the end plate I! of Figure 1 and the first stator disk l6, this first stator disk being the one shown at the left in Figure 5.
Fluid would enter from the inlet 48 and flow through the passageways 50 and 46 (see Figure 4) and through the openings 44 of the first separator disk [4. These openings are in alignment with the intake passageways 40 of the left hand stator disk I6 in Figure 5 so that the fluid can flow into the stator cavity from diametrically opposite points (see particularly Figure 2). At this position the blades 10 are outward in their pockets 68 thus enlarging the effective volume of the pockets and thereby drawing the fluid into the pockets.
As the rotor disk 30 in the first stator disk l8 continues to rotate the fluid will be forced out of the pockets by reason of the blades being driven back into them which causes the fluid to be expelled into the outlet passageways 42 of the first stator disk. Since these are in alignment with the openings 44 of the second separator disk [4 (second disk from the left in Figure 5) the fluid flows through them and enters the intake passageways 40 of the second stator disk I6 (third disc from the left in Figure 5).
In the stator cavity of this stator disk a similar pumping action takes place which draws fluid in alignment with the openings 44 of the third separator disk (right hand disc in Figure 5) which may now be considered as next to the end plate l8 so that the fluid discharges from the ports 44 of this separator disk to the passageways 52 and 54 of the end plate It (see Figure 10) with discharge of the fluid from the boss 56.
In order to align the ports and passageways properly alternate separator disks and alternate stator disks are rotated to each other s illustrated in Figure 5 and obviously the staging in the pump can be single (two end separator disks with one stator disk between them) or two stage (the same as the single stage with the addition of one separator disk and one stator disk as just explained in connection with Figure 5 including another separator disk to the left of the four disks there shown). In Figure 1 a five stage pump is illustrated.
While I have referred to my device as being a rotary pump obviously it may be a fluid driven motor or more generically a fluid displacement device as the structure is adaptable to both motors and pumps which are both fluid displacing devices.
The blades are so designed in shape that wear does not affect the sealing qualities of the blades in the rotor pockets. Upon wear occurring the blades merely assume a new working range farther out in the pockets without substantially changing the relationship of the blades to the pockets.
My stacking arrangement of the pump units obviously makes it possible to assemble from a few parts a high ressure pump having any desired operating pressure within certain limits. The only modification required because of a change in size is a difierent length of tie rod 32.
Some changes may be made in the construction and arrangement of the parts of my device without departing from the real spirit and purpose of my invention, and it is my intention to cover by my claims any modified forms of structure or use of mechanical equivalents which may be reasonably included within their scope.
I claim as my invention:
1. A fluid displacement device comprising a stator having an out-of-round stator cavity, a rotor rotatable therein, said rotor having bladereceiving pockets, blades received therein for free movement relative to the pockets and radial movement relative to the stator cavity in order to contact the wall thereof, each of said blades being substantially a half-circle in cross-sectional shape, each of said pockets having a similar shaped bottom, said pockets being of substantially the same size as said blades to effect substantially complete displacement of fluid from said pockets in the seated positions of said blades.
2. A fluid displacement device comprising a stator having an out-of-round stator cavity, a rotor rotatable therein, said rotor having bladereceiving pockets, blades received therein for free movement relative to the pockets and radial movement relative to the stator cavity in order to contact the wall thereof, each of said blades being substantially a half-circle in cross-sectional shape, each of said pockets having a similar shaped bottom, said pockets being of substantially the same size as said blades to effect substantially complete displacement of fluid from said pockets in the seated positions of said blades, and a relief opening through each of said blades located between the front and rear faces of the blade and extending from the stator contactin face of the blade to the opposite face thereof to balance out excess pressure between said blade and said stator by conducting the fluid from the pocket, thus aiding said blade to follow the contour of said stator.
3. A rotary fluid displacement device compris ing a stator having an out-of-round stator cavity, a rotor located therein, said rotor having blade-receiving pockets, a blade received in each of said pockets, each of said blades having contact at all times during operation with said stator and said rotor, in which the contact between the outer surface of the blade and the inner surface of the stator is area contact to prevent complete rotation of the blade in the pocket but permit it to rock therein with free movement in relation to said pocket, and the contact of a side of the blade with the rotor pocket being along a line which varies in position with respect to the blade and the pocket during operation and which acts as a pivot for the blade, the pivot action tending to keep the outer surface of the blade in said area contact with said stator during all positions of rotation of said rotor.
MARVIN L. RHINE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 395,085 Smith Dec. 25, 1888 462,708 I-Iochhausen Nov. 10, 1891 738,101 Curtis Sept. 1, 1903 901,539 Leyner Oct. 20, 1908 1,051,360 Wisdom Jan. 21, 1913 1,088,836 Nielsen Mar. 3, 1914 1,271,585 Klise July 9, 1918 1,324,260 Meyer Dec. 9, 1919 1,457,696 Ford June 5, 1923 1,495,526 Phillips May 27, 1924 1,558,696 Marion Oct. 2'7, 1925 1,651,336 Wissler Nov. 29, 1927 1,773,211 Wilsey Aug. 19, 1930 1,898,914 Vickers Feb. 21, 1933 1,989,900 Vickers Feb. 5, 1935 2,016,315 Calzoni Oct. 8, 1935 2,045,014 Kenney et al June 23, 1936 2,055,587 Pigott Sept. 29, 1936 2,149,337 Deming Mar. 7, 1939 2,312,891 Ferris Mar. 2, 1943 2,333,323 Livermore Nov. 2, 1943 2,357,333 Kendrick Sept. 5, 1944 2,367,068 Stevenson Jan. 9, 1945 2,387,761 Kendrick Oct. 30, 1945 2,423,507 Lawton July 8, 1947 2,424,285 Piccardo et a1 July 22, 1947 2,521,236 MacPherson Sept. 5, 1950 FOREIGN PATENTS Number Country Date 450,669 Great Britain July 17, 1936 590,729 France Mar. 25, 1925
US665268A 1946-04-26 1946-04-26 High-pressure pump Expired - Lifetime US2628568A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US665268A US2628568A (en) 1946-04-26 1946-04-26 High-pressure pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US665268A US2628568A (en) 1946-04-26 1946-04-26 High-pressure pump

Publications (1)

Publication Number Publication Date
US2628568A true US2628568A (en) 1953-02-17

Family

ID=24669418

Family Applications (1)

Application Number Title Priority Date Filing Date
US665268A Expired - Lifetime US2628568A (en) 1946-04-26 1946-04-26 High-pressure pump

Country Status (1)

Country Link
US (1) US2628568A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2830543A (en) * 1955-07-27 1958-04-15 Mechanisms Company Fluid pressure transducer for converting rotary force to fluid pressure, or vice-versa
US3003427A (en) * 1958-10-23 1961-10-10 James L Grupen Pump stator
US3040973A (en) * 1958-12-02 1962-06-26 Prec Scient Company Vacuum pump
US3186348A (en) * 1963-02-04 1965-06-01 Tissot Hans Rotary pump
US3189263A (en) * 1962-02-08 1965-06-15 Fichtel & Sachs Ag Packing system for rotary combustion engine and the like
US3191853A (en) * 1964-11-16 1965-06-29 Worthington Corp Rotary compressor
US3263621A (en) * 1961-11-10 1966-08-02 Eickmann Karl Rotary vane machine
US3869231A (en) * 1973-10-03 1975-03-04 Abex Corp Vane type fluid energy translating device
US4009690A (en) * 1973-05-31 1977-03-01 Moran George W Rotary internal combustion engine
EP0168268A1 (en) * 1984-05-21 1986-01-15 André Leroy Volumetric machine with rollers

Citations (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US395085A (en) * 1888-12-25 Rotary pump
US462708A (en) * 1891-11-10 Rotary pump
US738101A (en) * 1903-03-09 1903-09-01 Glynn B Stannard Rotary force-pump.
US901539A (en) * 1905-06-14 1908-10-20 John George Leyner Multiple-stage air-compressor.
US1051360A (en) * 1910-04-05 1913-01-21 William H Perry Air-pump.
US1088836A (en) * 1912-12-17 1914-03-03 Jens Nielsen Horizontal rotary engine or pump.
US1271585A (en) * 1917-12-05 1918-07-09 Blacker Rotary Pump Co Rotary pump.
US1324260A (en) * 1919-01-28 1919-12-09 Bulldog Pump Co Rotary pump.
US1457696A (en) * 1920-06-08 1923-06-05 Fordartic Refrigeration Compan Compressor
US1495526A (en) * 1923-08-13 1924-05-27 Phillips Harry Clarence Rotary prime mover, motor, compressor, pump, and the like
FR590729A (en) * 1924-02-13 1925-06-22 Emidecau Continuous rotary pusher with eclipsing scoops
US1558696A (en) * 1922-12-08 1925-10-27 Jamie E Jacobs Rotary pump
US1651336A (en) * 1927-03-29 1927-11-29 Wissler Rotary Wedge Pump Comp Rotary pump
US1773211A (en) * 1927-09-24 1930-08-19 James B Tuthill Rotary machine
US1898914A (en) * 1929-02-25 1933-02-21 Harry F Vickers Vane pump or motor
US1989900A (en) * 1931-01-15 1935-02-05 Harry F Vickers Vane type pump
US2016315A (en) * 1933-04-24 1935-10-08 Calzoni Alfredo Revolving piston machine
US2045014A (en) * 1934-07-07 1936-06-23 Gen Household Utilities Compan Compressor
GB450669A (en) * 1934-10-17 1936-07-17 Edward Ewart Guinness Improvements in or relating to rotary engines
US2055587A (en) * 1935-10-11 1936-09-29 Gulf Research Development Co Pump
US2149337A (en) * 1934-12-11 1939-03-07 Deming Rotary Pump Company Rotary pump
US2312891A (en) * 1939-05-19 1943-03-02 Oilgear Co Hydrodynamic machine
US2333323A (en) * 1940-08-10 1943-11-02 William T Livermore Pump
US2357333A (en) * 1941-03-29 1944-09-05 Manly Corp Fluid pressure device
US2367068A (en) * 1942-07-04 1945-01-09 Stevenson Engineering Corp Rotary pump
US2387761A (en) * 1942-04-17 1945-10-30 Manly Corp Fluid pressure device
US2423507A (en) * 1941-10-11 1947-07-08 S N Van Wert Planetary piston pump
US2424285A (en) * 1941-05-31 1947-07-22 Jacuzzi Bros Inc Pump and pump system
US2521236A (en) * 1945-11-21 1950-09-05 William H Macpherson Rotary pump

Patent Citations (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US395085A (en) * 1888-12-25 Rotary pump
US462708A (en) * 1891-11-10 Rotary pump
US738101A (en) * 1903-03-09 1903-09-01 Glynn B Stannard Rotary force-pump.
US901539A (en) * 1905-06-14 1908-10-20 John George Leyner Multiple-stage air-compressor.
US1051360A (en) * 1910-04-05 1913-01-21 William H Perry Air-pump.
US1088836A (en) * 1912-12-17 1914-03-03 Jens Nielsen Horizontal rotary engine or pump.
US1271585A (en) * 1917-12-05 1918-07-09 Blacker Rotary Pump Co Rotary pump.
US1324260A (en) * 1919-01-28 1919-12-09 Bulldog Pump Co Rotary pump.
US1457696A (en) * 1920-06-08 1923-06-05 Fordartic Refrigeration Compan Compressor
US1558696A (en) * 1922-12-08 1925-10-27 Jamie E Jacobs Rotary pump
US1495526A (en) * 1923-08-13 1924-05-27 Phillips Harry Clarence Rotary prime mover, motor, compressor, pump, and the like
FR590729A (en) * 1924-02-13 1925-06-22 Emidecau Continuous rotary pusher with eclipsing scoops
US1651336A (en) * 1927-03-29 1927-11-29 Wissler Rotary Wedge Pump Comp Rotary pump
US1773211A (en) * 1927-09-24 1930-08-19 James B Tuthill Rotary machine
US1898914A (en) * 1929-02-25 1933-02-21 Harry F Vickers Vane pump or motor
US1989900A (en) * 1931-01-15 1935-02-05 Harry F Vickers Vane type pump
US2016315A (en) * 1933-04-24 1935-10-08 Calzoni Alfredo Revolving piston machine
US2045014A (en) * 1934-07-07 1936-06-23 Gen Household Utilities Compan Compressor
GB450669A (en) * 1934-10-17 1936-07-17 Edward Ewart Guinness Improvements in or relating to rotary engines
US2149337A (en) * 1934-12-11 1939-03-07 Deming Rotary Pump Company Rotary pump
US2055587A (en) * 1935-10-11 1936-09-29 Gulf Research Development Co Pump
US2312891A (en) * 1939-05-19 1943-03-02 Oilgear Co Hydrodynamic machine
US2333323A (en) * 1940-08-10 1943-11-02 William T Livermore Pump
US2357333A (en) * 1941-03-29 1944-09-05 Manly Corp Fluid pressure device
US2424285A (en) * 1941-05-31 1947-07-22 Jacuzzi Bros Inc Pump and pump system
US2423507A (en) * 1941-10-11 1947-07-08 S N Van Wert Planetary piston pump
US2387761A (en) * 1942-04-17 1945-10-30 Manly Corp Fluid pressure device
US2367068A (en) * 1942-07-04 1945-01-09 Stevenson Engineering Corp Rotary pump
US2521236A (en) * 1945-11-21 1950-09-05 William H Macpherson Rotary pump

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2830543A (en) * 1955-07-27 1958-04-15 Mechanisms Company Fluid pressure transducer for converting rotary force to fluid pressure, or vice-versa
US3003427A (en) * 1958-10-23 1961-10-10 James L Grupen Pump stator
US3040973A (en) * 1958-12-02 1962-06-26 Prec Scient Company Vacuum pump
US3263621A (en) * 1961-11-10 1966-08-02 Eickmann Karl Rotary vane machine
US3189263A (en) * 1962-02-08 1965-06-15 Fichtel & Sachs Ag Packing system for rotary combustion engine and the like
US3186348A (en) * 1963-02-04 1965-06-01 Tissot Hans Rotary pump
US3191853A (en) * 1964-11-16 1965-06-29 Worthington Corp Rotary compressor
US4009690A (en) * 1973-05-31 1977-03-01 Moran George W Rotary internal combustion engine
US3869231A (en) * 1973-10-03 1975-03-04 Abex Corp Vane type fluid energy translating device
EP0168268A1 (en) * 1984-05-21 1986-01-15 André Leroy Volumetric machine with rollers

Similar Documents

Publication Publication Date Title
US6824369B2 (en) Rotary variable expansible chamber-kinetic hybrid pump
US2101051A (en) Rotary fluid displacement device
US2101428A (en) Rotary fluid displacement device
US3472445A (en) Rotary positive displacement machines
US2628568A (en) High-pressure pump
US2832293A (en) Vane pump
US2195174A (en) Pump
US5171142A (en) Rotary displacement machine with cylindrical pretension on disc-shaped partition
US1996875A (en) Fluid motor and pump
US1245691A (en) Rotary pump.
US1238731A (en) Centrifugal pump.
US2919651A (en) Power transmission
US2880677A (en) Variable volume vane pump
CA2483975C (en) Rotary pistons
US2677330A (en) Vane pump
US4021165A (en) Rotative machine for fluids with spiral-like passages and vane wheels
US2872873A (en) Power transmission
US2072482A (en) Compressor or pump
US3402669A (en) Centrifugal inertia pump
US2557427A (en) Rotary pump or hydraulic turbine
CN109404276B (en) Double-acting vane pump
US2195901A (en) Fluid clutch or transmission
US2360833A (en) Rotary pump
US3316852A (en) Pump
US2417816A (en) Fluid pump or motor