US2460310A - Screw pump - Google Patents

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US2460310A
US2460310A US511083A US51108343A US2460310A US 2460310 A US2460310 A US 2460310A US 511083 A US511083 A US 511083A US 51108343 A US51108343 A US 51108343A US 2460310 A US2460310 A US 2460310A
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rotors
casing
shaft
rotor
air
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US511083A
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Rathman Gilbert
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ROOTS CONNERSVILLE BLOWER CORP
ROOTS-CONNERSVILLE BLOWER Corp
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ROOTS CONNERSVILLE BLOWER CORP
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    • 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
    • F01C1/00Rotary-piston machines or engines
    • F01C1/08Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/12Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type
    • F01C1/14Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F01C1/16Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type

Definitions

  • Thejnvention relates in general to an apparatus for propelling, or for being propelled by a compressibie or expansible medium and, specifically, relates to an improved technic in the opera tion of displacement apparatus of the type which includes two helically ribbed rotors in meshed engagement for compressing air or gas as it flows through a conduit.
  • displacement apparatus of the type which includes two helically ribbed rotors in meshed engagement for compressing air or gas as it flows through a conduit.
  • the low pressure air is caught at the intake end of the intermeshcd rotors, is advanced along the same to the opposite ends where a reduction in cross sectional area of the groove, or grooves as the case may be, places the air under compressison at its point of discharge from the rotors. 1t has been found in actual practice with such air compressors that the air is discharged not in a continuous stream but periodically surging, or pulsating, bach and forth in the discharge conduit.
  • the primary object of the invention is to provide a gaseous i'luid conducting or compression pump capable of maintaining a constant flow of the gaseous medium without this objectionable surging or variable pressure condition at the discharge end of the pump and more broadly considered the invention features a method for handling the compressed alr or other gaseous bodies as they are discharged from such'a pump in such way as will avoid such objectionable surging and maintain the desired continuity of iiow.
  • this objective is attained by positioning at the discharge end or ends of the rotors a valve operatively related to the rotors to maintain the air groove or grooves closed up to the point where the maximum compression is reached or almost reached and then 'to automatically open the discharge end of the groove or grooves to the discharge port of the apparatus so that at each rotation of the rotors the air will be discharged at or adjacent its point of maximum compression.
  • invention is to provide a simple form of appa-V ratus for translating the expansive force of the actuating medium into rotative mechanical force with a high degree of eiclency.
  • Fig. 3 is a horizontal sectional View taken on the plane indicated by the line 3 3 of Fig. l looking in the direction indicated by the arrows when the rotors have advanced the passageways in the valves to a closed position;
  • Fig. 4 is an exploded view in perspective showing details ,of the double rotary disc valve demounted from the shafts.
  • air pumping apparatus l0 comprising a rotor containing casing ii having at one end a gear box i2 and at the opposite end an antifriction bearing box i3.
  • a rotor containing casing ii having at one end a gear box i2 and at the opposite end an antifriction bearing box i3.
  • the casing li is provided adjacent opposite ends with inlet ports I9 and 2@ which may be supplied from a manifold 2l having a single intake port 22.
  • the casing is provided at its center and on the side opposite the ports I9 and 20 with a discharge port 23, as more particularly shown in Fig. 3.
  • the shaft Id is provided with a pair of rotors 2li and 25 eachprovided with a helical groove 26 and keyed to the shaft and secured against outward endwise movement by nuts 27.
  • the shaft i5 is provided with a pair of rotors 28 and 29 keyed to the shaft and each provided with a helical rib 30 andy similarly held against outward movement by nuts 3
  • Each of the rotors of one shaft is in intermeshed engagement with its companion rotor of the other shaft and the rotors follow conventional practices in this respect.
  • Shaft l5 projects to the outside of the appaof all four rotors.
  • the spacer block provides a centrally positioned bearing for the two shafts I4 and I3 passed therethrough as shown in Fig. 1.
  • is provided in the portion thereof exteriorly of its shaft receiving hole 44 with an opening 45 extending therethrough.
  • the opening 43 is illustrated as being of an elliptical form and in its length dimension is less than the length of the arc a-b formed at the bottom of the closure cylinder 33.
  • the cylinder 31 is providedin the portion faced 30 by the bearings 33 and 39 with a passageway 43 extending therethrough in offset relation Ito the opening 41 which receives the shaft l5.
  • This transverse passageway extends clrcumferentially and in the instant case for a distance of about 165 with its outer edge 48 aligned with the outer edge 43 of the opening 45, when the openings 43- and 43 are in registration as shown in Fig. 2.
  • 'I'he cylinder 31 is provided in the side thereof facing the outlet 23 with a passageway 50.
  • the passageway 45 is so located relative to the discharge end of the grooves or channels 23 that the passageway 45 is brought into registry with the passageway 43 as the air reaches its point of maximum compression as the result of the compressive action
  • the air so compressed is passed through passageways 43 and 50 and moves through the outlet 23 as indicated by the arrows in Fig. 2.
  • the gases are .periodically admitted to the inner ends of the rotors and in expanding react on the helical ribs 30 to rotate the rotors and in this way drive the shaft 32.
  • the port 22 constitutes an exhaust for the expanded gases.
  • a rotor casing having inlets adjacent its opposite ends and an outlet adjacent its center, two parallel shafts journalled in tht casing.
  • means for driving one shaft from the other each shaft provided with a pair of helically ribbed rotors fitted in the casing and with each of the rotors of' one shaft in intermeshed engagement with its companion rotor on the other shaft, a spacing block secured to the casing providing a rugged internal brace for the same and fitting between the rotors of one shaft to limit their approach towards each other and to provide a wall defining and closing the adjacent ends of the channels of said one shaft, and coacting with the adjacent ends of the channels thereof to form on each side of the spacing block a pair of tapered air compressing spaces, each pair of compression spacesl being open at al1 times to the discharge end of the groove in its associated rotor of the other shaft.
  • each flange provided with a slot extending therethrough and in open communication with the groove in its associated rotor and a channeled block secured to the casing at the outlet, fitted between the flanges and provided with a passagelway leading to the outlet from the sides thereof and periodically discharged as herein featured.
  • eachV auel shafts extending portion of the shafts' extend, each shaft provided on yopposite sides of the block with ahelical rib,with the rib on one shaft meshing into the helical groove of the adjacent rib of the other shaft, opposite sides of the block in the area surrounding one of the shafts recessed to provide bearings of flat circular form, said last named yshaft having keyed thereto a pair of disk-like flanges, one for each bearing and rotatably fitted therein, said block having ineach of the sides provided with the bearings an arcfshaped opening, each flange provided withthe portion thereof exteriorlyI of its associated shaft with an opening of less arc length than the arc length of the opening in the block and of approximateellip-v tical form, and said block provided
  • a device for-moving a uid the combina tion of a housing having at least two openings therein, one forming an inlet and the other forming an outlet for the iiuid, and a pair of intermeshing and cooperating screwlike rotors in said housing coacting to pass the fluid through the housing from the inlet through the outlet, a partition in the form of an 8-shaped casting tted in the casing and located between one of the openings and the adjacent ends of the pair of rotors, said partition provided with an opening having a dimension considered circumferentially materially less than 180 and facing one of the rotors and said partition in the area thereof facing the other rotor bein'g imperforated and thus acting at all times to close the channel at the adjacent end ofthe other rotor, the ends )f the ⁇ channels of both rotors coacting with the partition to form compartments tapering in cross sectional area to permit the fluid to expand or to Vbecome compressed as it passes therethrough,
  • a casing provided with inlet and outlet ports, a pair of rotors located between the ports, means connecting the rotors to drive one from the other, the rotors provided with coacting ribs in interengaging relation to compress iiuid in the grooves of both rotors as the uid reaches the discharge ends of the grooves, one of the rotors constituting a driving rotor and the other a driven rotor, an ,element fixed to the casing and forming a stop Aengaged by the adjacent ends of both rotors, said element provided with a conduit leading to the discharge port and the intake end of said conduit forming an opening facing the adjacent end of the driving rotor and confined to the space within the axially projected cross sectional area of said driving rotor, said driving rotor and opening related to periodically open the adjacent end of the groove in the driving rotor once for a part of each rotation of the same, and said element extending
  • a fluid propelling pump vcomprising pump-l ing mechanism having its elements duplicated in balanced relation on opposite sides of a transverse medial plane and comprising on each side of the plane two helicallyribbed rotatable elements inintermeshlng engagement and adapted to advance a fluid there-through, and to place it under compression, said elements intergeared to drive one from the other, a casing surrounding said elements and provided with an inlet for the Aiiuid open to the receiving ends of said elements "said block and head provided with means coacting to form a valve of the rotary disc type, said block and head being each. provided with passage-ways extending there-through and adapted as each head is rotated with its associated ribbed element to register with the passage-way through theblock to discharge the uid advanced between the four ribbed elements periodically once for each rotation of the elements.
  • a screw pump including a casing having inlet and outlet ports, a pair of rotors journalled in the casing and intergeared to drive one from the other, each rotor provided with a spiral ribbed part, with one of said spiral ribbed parts intermeshing with the other to force fluids from the inlet through the casing and out-through the outlet and to place them under compression at the discharge ends of said spiral ribbed parts, a member fixed relative to the casing, extending across the interior of the same and located between the discharge ends of the spiral ribbed parts of the rotors and the outlet, said member provided with a passage-way facing the discharge end of one of said spiral rib parts, confined to the axially projected cross section of the spiral ribbed part which it faces, said passage-way arci shaped I crosssection.
  • a casing provided with inlet ports at opposite ends thereof and a discharge port ad'- jacent its mid-length, a pair oi' rotors journalled in the casing, means for driving one rotor from the other, each rotor provided with two helicaliy ribbed portions disposed on opposite sides 'of the mid-length of the casing, a partition i'itted inthe casing for closing the inner ends of both of said helically ribbed portions to cause the inner ends of all of the channels in said helically ribbed portions to be oi' reduced cross sectional area towards the partition, said partition provided with a passage-way leading to the discharge port and adapted to receive fluids discharged from the inner ends of the helically ribbed portions oi' one of the rotors, the discharge ends of all channels being otherwise closed.
  • a device ofthe class described the combination of a casing provided with an inlet port and an outlet port, a pair o! interxneshing screws fitted for free rotary movement in the casing and coacting to advance a fluid from the inlet port through the casing and out through the outlet port, means for driving one screw from the other. at a one-to-one ratio, a partition xed in the 8 casing against movement axially of the screws and against which the discharge ends of both screws abut. the opposite or intake ends of they screws being wide open to the. inlet port, said partition forming a barrier to close completely Athe discharge end of one of the screws and means controlled by the rotation oi the other screw for opening communication between the discharge end of the said other screw and the outlet port once for each rotation of the screws.

Description

Feb. l, E949. G. RATHMAN 2,460,3l0
SCREW PUMP Fild'nov. 2o, 194s 2 sheets-sheet 1 lll Patented Fe. ll, l@
I aient SCREW PUMP Application November 20, 1943, SerialNo. 511,083
. 9 Claims. l
Thejnvention relates in general to an apparatus for propelling, or for being propelled by a compressibie or expansible medium and, specifically, relates to an improved technic in the opera tion of displacement apparatus of the type which includes two helically ribbed rotors in meshed engagement for compressing air or gas as it flows through a conduit. In such air compressors as are now known, the low pressure air is caught at the intake end of the intermeshcd rotors, is advanced along the same to the opposite ends where a reduction in cross sectional area of the groove, or grooves as the case may be, places the air under compressison at its point of discharge from the rotors. 1t has been found in actual practice with such air compressors that the air is discharged not in a continuous stream but periodically surging, or pulsating, bach and forth in the discharge conduit.
The primary object of the invention is to provide a gaseous i'luid conducting or compression pump capable of maintaining a constant flow of the gaseous medium without this objectionable surging or variable pressure condition at the discharge end of the pump and more broadly considered the invention features a method for handling the compressed alr or other gaseous bodies as they are discharged from such'a pump in such way as will avoid such objectionable surging and maintain the desired continuity of iiow.
Broadly, this objective is attained by positioning at the discharge end or ends of the rotors a valve operatively related to the rotors to maintain the air groove or grooves closed up to the point where the maximum compression is reached or almost reached and then 'to automatically open the discharge end of the groove or grooves to the discharge port of the apparatus so that at each rotation of the rotors the air will be discharged at or adjacent its point of maximum compression. 4
Considering the situation where the apparatus is used as a prime mover such, for instance, as
invention is to provide a simple form of appa-V ratus for translating the expansive force of the actuating medium into rotative mechanical force with a high degree of eiclency.
Various other objects and advantages of the invention will be in part obvious from an inspec- (Cl. 23o-M3) tion of the accompanying drawings and in part will be more fully set forth in the following particular description of one form of mechanism vembodying the invention, and theinvention also consists in certain new and novel features of construction and combination of parts hereinafter Fig. 3 is a horizontal sectional View taken on the plane indicated by the line 3 3 of Fig. l looking in the direction indicated by the arrows when the rotors have advanced the passageways in the valves to a closed position; and
Fig. 4 is an exploded view in perspective showing details ,of the double rotary disc valve demounted from the shafts.
In the drawings' there is disclosed air pumping apparatus l0 comprising a rotor containing casing ii having at one end a gear box i2 and at the opposite end an antifriction bearing box i3. Mounted in the apparatus are two shafts Id and l5 disposed in parallel relation having antifric tion bearings it at opposite ends of each shaft and with the shafts connected by a pair of gears l l-IB in gear box l2 to drive one shaft from the other. The casing li is provided adjacent opposite ends with inlet ports I9 and 2@ which may be supplied from a manifold 2l having a single intake port 22. The casing is provided at its center and on the side opposite the ports I9 and 20 with a discharge port 23, as more particularly shown in Fig. 3.
The shaft Id is provided with a pair of rotors 2li and 25 eachprovided with a helical groove 26 and keyed to the shaft and secured against outward endwise movement by nuts 27. Similarly,
the shaft i5 is provided with a pair of rotors 28 and 29 keyed to the shaft and each provided with a helical rib 30 andy similarly held against outward movement by nuts 3|. Each of the rotors of one shaft is in intermeshed engagement with its companion rotor of the other shaft and the rotors follow conventional practices in this respect. A
Shaft l5 projects to the outside of the appaof all four rotors.
8-shaped internal brace for the midlength pori0 tion of the casing. The spacer block provides a centrally positioned bearing for the two shafts I4 and I3 passed therethrough as shown in Fig. 1.
Opposite sides of the block in the portion 31 thereof which faces the helical ribs are rel5 respective bearings 33 and 39 andare keyed to 20 the shaft respectively by keys 42 and.43. l Each disc-like flange 40 and 4| is provided in the portion thereof exteriorly of its shaft receiving hole 44 with an opening 45 extending therethrough.
In order to obtain maximum time delay in which 25 the valve is open, the opening 43 is illustrated as being of an elliptical form and in its length dimension is less than the length of the arc a-b formed at the bottom of the closure cylinder 33.
The cylinder 31 is providedin the portion faced 30 by the bearings 33 and 39 with a passageway 43 extending therethrough in offset relation Ito the opening 41 which receives the shaft l5. This transverse passageway extends clrcumferentially and in the instant case for a distance of about 165 with its outer edge 48 aligned with the outer edge 43 of the opening 45, when the openings 43- and 43 are in registration as shown in Fig. 2. 'I'he cylinder 31 is provided in the side thereof facing the outlet 23 with a passageway 50.
In operation and assuming that air is being admitted through the intake ports I9 and 20 and that the rotors are being driven from a source of power supplied through the shaft 32 and in a it will be understood that air admitted to the grooves 23 will be advanced by the ribs 30 towards the center of the apparatus. As the channels 23 taper in cross sectional area at their discharge direction to turn their ribs towards the center, 45
ends, the air trapped therein is placed under pressure at least momentarily. It is noted that the discharge ends of the helical grooves 26 in both of the rotors 24 and 25; that is the ends where the air is finally compressed, are never open directly to the outlet valves and thus are never open to the outside air. If this were not so and air. accumulating in the discharge ends of the grooves 23 in rotors 24 and 23 were permitted to escape a back pressure would develop in the grooves oi' the rotors 23 and 24. The air 00 ycompressed in the terminal portions of the the channels of the rotors 28 and 29 that the air compressed in the rotors 24 and 23 is eventually 4 charge flow, of course no air can escape from the compression chamber found at the discharge ends of the rotors 23 and 29. The passageway 45 is so located relative to the discharge end of the grooves or channels 23 that the passageway 45 is brought into registry with the passageway 43 as the air reaches its point of maximum compression as the result of the compressive action The air so compressed is passed through passageways 43 and 50 and moves through the outlet 23 as indicated by the arrows in Fig. 2.
It has been foundv that this method of delaying the escape of the air until it reaches or at least approaches its point of maximum compression, and then releasing it at this point, has the effect of avoiding the surging, or pulsating action, which takes place in devices of this character where such a periodically opening and closingr valve so timed in its action is not used.
Considering the use of the apparatus wherera v flowing or expanding gas is utilized to rotate-the shaft 32 as in those cases where the port 23 is connected with the firing chamber of an internal combustion engine supplied with a carburetor, the gases are .periodically admitted to the inner ends of the rotors and in expanding react on the helical ribs 30 to rotate the rotors and in this way drive the shaft 32. It is understood, 'of course, that in this case the port 22 constitutes an exhaust for the expanded gases.
I claim:
1. In a device of the class described, the combination of a rotor casing having inlets adjacent its opposite ends and an outlet adjacent its center, two parallel shafts journalled in tht casing. means for driving one shaft from the other, each shaft provided with a pair of helically ribbed rotors fitted in the casing and with each of the rotors of' one shaft in intermeshed engagement with its companion rotor on the other shaft, a spacing block secured to the casing providing a rugged internal brace for the same and fitting between the rotors of one shaft to limit their approach towards each other and to provide a wall defining and closing the adjacent ends of the channels of said one shaft, and coacting with the adjacent ends of the channels thereof to form on each side of the spacing block a pair of tapered air compressing spaces, each pair of compression spacesl being open at al1 times to the discharge end of the groove in its associated rotor of the other shaft. the inner ends of the rotors of the other shaft each provided with an outstanding flange in rotative sliding engagement with the adjacent side of the block, each flange provided with a slot extending therethrough and in open communication with the groove in its associated rotor and a channeled block secured to the casing at the outlet, fitted between the flanges and provided with a passagelway leading to the outlet from the sides thereof and periodically discharged as herein featured.
ing the time while the valves interrupt the disadjacent the flanges said slots. being each of less circumferential length than that of the passageway whereby the passageway is closed once for each rotation ofthe flanges, the slots in eachV auel shafts extending portion of the shafts' extend, each shaft provided on yopposite sides of the block with ahelical rib,with the rib on one shaft meshing into the helical groove of the adjacent rib of the other shaft, opposite sides of the block in the area surrounding one of the shafts recessed to provide bearings of flat circular form, said last named yshaft having keyed thereto a pair of disk-like flanges, one for each bearing and rotatably fitted therein, said block having ineach of the sides provided with the bearings an arcfshaped opening, each flange provided withthe portion thereof exteriorlyI of its associated shaft with an opening of less arc length than the arc length of the opening in the block and of approximateellip-v tical form, and said block provided with a passageway open at one end to the outlet port, and the other end of the passageway being alter-` nately opened and closed from the two pairs of meshed helical ribsby the rotation of said shaft and its associated flanges.
3. In a device for-moving a uid, the combina tion of a housing having at least two openings therein, one forming an inlet and the other forming an outlet for the iiuid, and a pair of intermeshing and cooperating screwlike rotors in said housing coacting to pass the fluid through the housing from the inlet through the outlet, a partition in the form of an 8-shaped casting tted in the casing and located between one of the openings and the adjacent ends of the pair of rotors, said partition provided with an opening having a dimension considered circumferentially materially less than 180 and facing one of the rotors and said partition in the area thereof facing the other rotor bein'g imperforated and thus acting at all times to close the channel at the adjacent end ofthe other rotor, the ends )f the` channels of both rotors coacting with the partition to form compartments tapering in cross sectional area to permit the fluid to expand or to Vbecome compressed as it passes therethrough, depending on the direction of movement of the fluid therethrough, with said compartments being at all times in intercommunication, and one of said compartments periodically exposed through said opening to the outlet during a portion of each rotation of the rotors.
4. In a device of the class described, the combination of a casing provided with inlet and outlet ports, a pair of rotors located between the ports, means connecting the rotors to drive one from the other, the rotors provided with coacting ribs in interengaging relation to compress iiuid in the grooves of both rotors as the uid reaches the discharge ends of the grooves, one of the rotors constituting a driving rotor and the other a driven rotor, an ,element fixed to the casing and forming a stop Aengaged by the adjacent ends of both rotors, said element provided with a conduit leading to the discharge port and the intake end of said conduit forming an opening facing the adjacent end of the driving rotor and confined to the space within the axially projected cross sectional area of said driving rotor, said driving rotor and opening related to periodically open the adjacent end of the groove in the driving rotor once for a part of each rotation of the same, and said element extending solidly in overlapping relation to the adjacent end of the driven rotor to close the adjacent end of its groove and thus intercept direct iiuid communication between the outlet port and the groove in said driven rotor while permitting the air compressed in the grooveof the driven rotor to by-'pass therefrom into the groove of the driving rotor from which it is discharged through said opening when the discharge end of the groove in the driving element registers with said opening.
5. A fluid propelling pump vcomprising pump-l ing mechanism having its elements duplicated in balanced relation on opposite sides of a transverse medial plane and comprising on each side of the plane two helicallyribbed rotatable elements inintermeshlng engagement and adapted to advance a fluid there-through, and to place it under compression, said elements intergeared to drive one from the other, a casing surrounding said elements and provided with an inlet for the Aiiuid open to the receiving ends of said elements "said block and head provided with means coacting to form a valve of the rotary disc type, said block and head being each. provided with passage-ways extending there-through and adapted as each head is rotated with its associated ribbed element to register with the passage-way through theblock to discharge the uid advanced between the four ribbed elements periodically once for each rotation of the elements.
6. In a device of the class described, the combination of the casing'provided with inlet and outlet ports, a pair of intermeshing helically ribbed rotors for advancing fluid from the inlet to the outlet ports and for placing the fluid under pressure as it is discharged, an element fixed relative to the casing, provided with an opening facing the discharge high pressure end of one of the rotors, and confined to the space within the axially projected cross sectional area of said rotor and said element acting asa barrier for closing the discharge end of the other rotor, said rst named rotor and its associated opening being related to open the adjacent end ofthe first named rotor periodically once for each rotation of the same and only at that lpoint where the rotors reach their point of maximum compression.
'7. A screw pump including a casing having inlet and outlet ports, a pair of rotors journalled in the casing and intergeared to drive one from the other, each rotor provided with a spiral ribbed part, with one of said spiral ribbed parts intermeshing with the other to force fluids from the inlet through the casing and out-through the outlet and to place them under compression at the discharge ends of said spiral ribbed parts, a member fixed relative to the casing, extending across the interior of the same and located between the discharge ends of the spiral ribbed parts of the rotors and the outlet, said member provided with a passage-way facing the discharge end of one of said spiral rib parts, confined to the axially projected cross section of the spiral ribbed part which it faces, said passage-way arci shaped I crosssection. and another portion ot said me ber extending entirely across`the axially projected cross section of the other spiral Y 8. In a device of the class described, the combination of a casing provided with inlet ports at opposite ends thereof and a discharge port ad'- jacent its mid-length, a pair oi' rotors journalled in the casing, means for driving one rotor from the other, each rotor provided with two helicaliy ribbed portions disposed on opposite sides 'of the mid-length of the casing, a partition i'itted inthe casing for closing the inner ends of both of said helically ribbed portions to cause the inner ends of all of the channels in said helically ribbed portions to be oi' reduced cross sectional area towards the partition, said partition provided with a passage-way leading to the discharge port and adapted to receive fluids discharged from the inner ends of the helically ribbed portions oi' one of the rotors, the discharge ends of all channels being otherwise closed.
9. In a device ofthe class described. the combination of a casing provided with an inlet port and an outlet port, a pair o! interxneshing screws fitted for free rotary movement in the casing and coacting to advance a fluid from the inlet port through the casing and out through the outlet port, means for driving one screw from the other. at a one-to-one ratio, a partition xed in the 8 casing against movement axially of the screws and against which the discharge ends of both screws abut. the opposite or intake ends of they screws being wide open to the. inlet port, said partition forming a barrier to close completely Athe discharge end of one of the screws and means controlled by the rotation oi the other screw for opening communication between the discharge end of the said other screw and the outlet port once for each rotation of the screws.
GILBERT RATHMAN.
nnrnnnNcEs crrnn The following references are of record in the file oi' this' patent: l
I UNITED STATE@ PATENTS Number. Name Date f 165,805 Disston J 20. 1875 514.559 Morgan Feb. 18, 1894 y 960,992 Motsinger June 7, 1910 960,994 Motsinger June 7; 1910 1,430,894 Fay Oct. 8. 1922 1,701,188 Tiit Feb. 5, 1929 41,991,041 Cannizzaro Feb. 19, 1935 2,130,054 Whitfield Sept. 18, 1938 2,287,716 Whitfield ..---.-....1... June 23, 19412 FOREIGN lPAW-'NTB Number Country j Date 384,355 Great Britain Dec. 8. 1982 591,679 France Apr. 18, 1925
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511878A (en) * 1950-06-20 Rathman
US2578196A (en) * 1946-11-30 1951-12-11 Imo Industri Ab Screw compressor
US2580006A (en) * 1948-04-07 1951-12-25 Wade Engineering Ltd Compressor
US2655309A (en) * 1950-05-01 1953-10-13 J F Nevins Dual rotor compressor
US2656972A (en) * 1949-01-31 1953-10-27 Dresser Ind Adjustable port arrangement for the high-pressure ends of fluid pumps and motors of the rotary screw type
US2804260A (en) * 1949-07-11 1957-08-27 Svenska Rotor Maskiner Ab Engines of screw rotor type
US3011447A (en) * 1956-10-01 1961-12-05 Robert W Brundage Hydraulic pump or motor
US3074624A (en) * 1960-03-11 1963-01-22 Svenska Rotor Maskiner Ab Rotary machine
US3112869A (en) * 1960-10-17 1963-12-03 Willis A Aschoff High vacuum pump
US3275226A (en) * 1965-02-23 1966-09-27 Joseph E Whitfield Thrust balancing and entrapment control means for screw type compressors and similardevices
US20090288648A1 (en) * 2008-05-21 2009-11-26 Gm Global Technology Operations, Inc. Superchargers with dual integral rotors

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US165805A (en) * 1875-07-20 Improvement m rotary blowers
US514659A (en) * 1894-02-13 Suction and force apparatus for pumping fluids
FR591679A (en) * 1900-01-01
US960994A (en) * 1909-12-20 1910-06-07 Newell H Motsinger Rotary engine.
US960992A (en) * 1909-12-20 1910-06-07 Newell H Motsinger Rotary engine.
US1430894A (en) * 1920-04-13 1922-10-03 William E Quimby Inc Screw pump
US1701166A (en) * 1927-06-07 1929-02-05 Sinclair Refining Co Hot-oil pump
GB384355A (en) * 1931-08-05 1932-12-08 Frederick Charles Greenfield Improvements in and relating to rotary machines for the compression and propulsion of
US1991541A (en) * 1933-09-19 1935-02-19 Cannizzaro Joseph Combined velocity and displacement pump or compressor
US2130054A (en) * 1935-07-02 1938-09-13 Joseph E Whitfield Blower
US2287716A (en) * 1941-04-22 1942-06-23 Joseph E Whitfield Fluid device

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US165805A (en) * 1875-07-20 Improvement m rotary blowers
US514659A (en) * 1894-02-13 Suction and force apparatus for pumping fluids
FR591679A (en) * 1900-01-01
US960994A (en) * 1909-12-20 1910-06-07 Newell H Motsinger Rotary engine.
US960992A (en) * 1909-12-20 1910-06-07 Newell H Motsinger Rotary engine.
US1430894A (en) * 1920-04-13 1922-10-03 William E Quimby Inc Screw pump
US1701166A (en) * 1927-06-07 1929-02-05 Sinclair Refining Co Hot-oil pump
GB384355A (en) * 1931-08-05 1932-12-08 Frederick Charles Greenfield Improvements in and relating to rotary machines for the compression and propulsion of
US1991541A (en) * 1933-09-19 1935-02-19 Cannizzaro Joseph Combined velocity and displacement pump or compressor
US2130054A (en) * 1935-07-02 1938-09-13 Joseph E Whitfield Blower
US2287716A (en) * 1941-04-22 1942-06-23 Joseph E Whitfield Fluid device

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511878A (en) * 1950-06-20 Rathman
US2578196A (en) * 1946-11-30 1951-12-11 Imo Industri Ab Screw compressor
US2580006A (en) * 1948-04-07 1951-12-25 Wade Engineering Ltd Compressor
US2656972A (en) * 1949-01-31 1953-10-27 Dresser Ind Adjustable port arrangement for the high-pressure ends of fluid pumps and motors of the rotary screw type
US2804260A (en) * 1949-07-11 1957-08-27 Svenska Rotor Maskiner Ab Engines of screw rotor type
US2655309A (en) * 1950-05-01 1953-10-13 J F Nevins Dual rotor compressor
US3011447A (en) * 1956-10-01 1961-12-05 Robert W Brundage Hydraulic pump or motor
US3074624A (en) * 1960-03-11 1963-01-22 Svenska Rotor Maskiner Ab Rotary machine
US3112869A (en) * 1960-10-17 1963-12-03 Willis A Aschoff High vacuum pump
US3275226A (en) * 1965-02-23 1966-09-27 Joseph E Whitfield Thrust balancing and entrapment control means for screw type compressors and similardevices
US20090288648A1 (en) * 2008-05-21 2009-11-26 Gm Global Technology Operations, Inc. Superchargers with dual integral rotors

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