GB2401400A - Pump with screw pitch less than 1.6 times the diameter - Google Patents

Pump with screw pitch less than 1.6 times the diameter Download PDF

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Publication number
GB2401400A
GB2401400A GB0310591A GB0310591A GB2401400A GB 2401400 A GB2401400 A GB 2401400A GB 0310591 A GB0310591 A GB 0310591A GB 0310591 A GB0310591 A GB 0310591A GB 2401400 A GB2401400 A GB 2401400A
Authority
GB
United Kingdom
Prior art keywords
rotor
pump
threads
rotors
outer diameter
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.)
Withdrawn
Application number
GB0310591A
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GB0310591D0 (en
Inventor
Michael John Werson
Robert William Beaven
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.)
Automotive Motion Technology Ltd
Original Assignee
Automotive Motion Technology Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Automotive Motion Technology Ltd filed Critical Automotive Motion Technology Ltd
Priority to GB0310591A priority Critical patent/GB2401400A/en
Publication of GB0310591D0 publication Critical patent/GB0310591D0/en
Priority to US10/839,992 priority patent/US7232297B2/en
Priority to DE602004004309T priority patent/DE602004004309T2/en
Priority to PT04010909T priority patent/PT1475537E/en
Priority to ES04010909T priority patent/ES2283899T3/en
Priority to AT04010909T priority patent/ATE351981T1/en
Priority to EP04010909A priority patent/EP1475537B1/en
Publication of GB2401400A publication Critical patent/GB2401400A/en
Priority to US11/657,502 priority patent/US7452194B2/en
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F04C2/08Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C2/082Details specially related to intermeshing engagement type machines or pumps
    • F04C2/084Toothed wheels
    • 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
    • F04C2/08Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C2/12Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C2/14Rotary-piston machines or pumps 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
    • F04C2/16Rotary-piston machines or pumps 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
    • F04C2/165Rotary-piston machines or pumps 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 having more than two rotary pistons with parallel axes

Abstract

A pump 10 including at least two rotors 12, 14a, 14b each being provided with a generally helical screw thread 20, 20', 26a, 26a', 26b 26b', one rotor 12 having a larger outer diameter than the others. The rotors are mounted for rotation in a housing (16 Fig. 1) such that the screw threads mesh and rotation of one rotor causes rotation of the others, The pitch P of the threads is less than 1.6 times and greater than 0.5 times the outer diameter (OD) of the larger diameter rotor. A pitch/diameter ratio of less than 1.6 allows a greater number of fluid chambers for a given length than conventional rotors having a ratio of 2 to 2.4. The depth of the threads may be less than 0.2 times the outer diameter of the larger rotor to reduce leakage, cost and increase volumetric efficience over deeper threads.

Description

À À - :. : : . PATENTS ACT 1977 A 1 0868GB/DJL/ACL Title: Pump
Description of Invention
The present invention relates to a pump, more particularly to a pump in which pumping is effected by means of at least two intermeshing screw threads, i.e. an intermeshing screw pump.
Pumps in which the pumped fluid is carried between the screw threads on one or more rotors such that the liquid is displaced in a direction generally parallel to the axis of rotation of the or each rotor, are known, and are generally referred to as screw pumps.
Where more than one rotor is provided, the pump is generally known as an intermeshing screw pump. In this case, one rotor is provided with one or more helical grooves and another rotor is provided with one or more corresponding helical ridges. Typically one of the rotors (the power rotor) is driven by motor, which when activated causes the power rotor to rotate along its longitudinal axis. The rotors are mounted in a housing such that their helical screw threads mesh and rotation of the power rotor causes the other rotor or rotors (the idler rotor or rotors) to rotate about its/their longitudinal axis or axes.
Fluid is drawn into the pump at an inlet or suction end of the pump between the counter-rotating screw threads. As the rotors turn the meshing of the threads produces fluid chambers bounded by the threads and the pump housing. Fluid becomes trapped in the fluid chambers and continued rotation of the screws causes the fluid chambers to move from the inlet end of the pump to the high pressure outlet end of the pump. Fluid is ejected from the pump at the outlet end as fluid is displaced from the fluid chambers.
It is known to increase the pressure of the fluid output from such a pump by increasing the length of the screws, and as a consequence known high . c. À c: pressure screw pumps tend to be relatively long and are thus unsuitable for use in applications where high output pressure and a compact pump is required, for example in automotive applications where space in an engine compartment is limited.
According to a first aspect of the invention, we provide a pump including at least two rotors each being provided with a generally helical screw thread, one rotor having a larger outer diameter than the other, the rotors being mounted for rotation in a housing such that the screw threads of the rotors mesh and rotation of one rotor causes rotation of the other rotor, wherein the pitch of the threads is less than 1.6 times the outer diameter of the larger diameter rotor.
In known intermeshing screw pumps, the pitch of the threads, i.e. the axial distance between corresponding points on adjacent turns of the thread, is typically twice the outer diameter of the larger diameter rotor, and may be up to 2.4 times the outer diameter of the larger diameter rotor. Thus, for a given pump length, more fluid chambers are formed in a pump according to the invention than in a conventional pump, i.e. for a given number of fluid chambers, a pump according to the invention is shorter than a conventional pump. Since the pressure of fluid output from anintermeshing screw pump depends, in part, on the number of fluid chambers formed by the screw threads of the rotors, for a given pressure, a pump according to the invention may be shorter than a conventional pump. Thus, by virtue of the invention, a screw pump may be produced which is capable of delivering high pressure fluid and which is more suitable for use in confined spaces such as those found-within an engine compartment of an automotive vehicle.
Preferably the pitch of the threads is less than 1.2 times the outer diameter of the larger diameter rotor.
The pitch of the threads may be less than the outer diameter of the larger diameter rotor, and may, for example, be 0.75 times the outer diameter of the larger diameter rotor.
:: age: À. .e.' .e Preferably the pitch of the threads is at least 0.5 times the outer diameter of the larger diameter rotor.
Preferably the thread depth of the screw threads is less than 0.2 times the outer diameter of the larger diameter rotor.
In conventional screw pumps, the thread depth of the screw threads is greater than 0.2 times the diameter of the larger diameter rotor. Whilst, decreasing the thread depth decreases the volume of each fluid chamber, and thus tends to decrease the volume output of the pump, use of a reduced thread depth has particular advantages. I One advantage of reducing the thread depth is that decreasing the thread depth also decreases the area of leakage paths which permit leakage of fluid from the fluid chambers, and thus reduces leakage from the fluid chambers and hence increases the volumetric efficiency of the pump. In addition, for a given rotor root diameter (the rotor outer diameter minus twice the thread depth), the overall diameter of a pump according to the invention may be reduced. Rotors with threads of lower depth are also easier and thus less expensive to machine.
Thus, a more compact and more efficient pump may be produced at reduced manufacturing cost.
Any reduction in output volume may be compensated for by increasing the speed of rotation of the rotors.
Preferably the thread depth of the screw threads is less than 0.175 times the outer diameter of the power rotor.
The thread depth of the screw threads may be less than 0.15 times the outer diameter of the power rotor.
Preferably the thread depth of the screw threads is at least 0.1 times the outer diameter of the power rotor.
Preferably each rotor is provided with two generally helical interposed screw threads. '
:e:. .:e:e À . Preferably the pump includes a power rotor and two idler rotors, the power rotor being arranged between the two idler rotors.
According to a second aspect of the invention we provide a rotor for a pump, the rotor being provided with a generally helical screw thread, wherein the pitch of the thread is less than 1.6 times the outer diameter of the rotor.
Embodiments of the invention will now be described with reference to the accompanying drawings in which: FIGURE 1 is a side sectional illustrative view of a pump according to the invention; FIGURE 2 is an enlarged illustrative view of the rotors of the pump of Figure l, the rotors being arranged in an inoperative position, side by side, FIGURE 3 is an illustrative end cross-sectional view through the rotors and housing of the pump shown in Figure 1.
Referring now to the figures, there is shown a pump 10 including a central power rotor 12 and two idler rotors 14a, 14b, all mounted for rotation about their longitudinal axes in a housing 16. The power rotor 12 is connected to a driving means by means of a drive shaft 18, in this case an electric motor (not shown) which when activated, causes the power rotors 12 to rotate about its longitudinal axis A. The drive shaft 18 is supported in a bearing assembly 28.
The power rotor 12 has a larger outside diameter than the two idler rotors 14a, 14b.
Each rotor 12, 14a, 14b is provided with a generally helical screw thread, and the rotors 12, 14a, 14b are arranged in the housing 16, with the power rotor 12 between the two idler rotors 14a, 14b, such that the screw threads mesh.
The longitudinal axes A, B and C of the rotors 12, 14a are generally parallel, and thus rotation of the power screw about axis A causes the idler rotors 14a, 14b to rotate about their longitudinal axes, B and C respectively.
In this example, the rotors 12, 14a, 14b are all provided with two generally helical threads or flights which each extend along substantially the e t'.
entire length of the rotor 12, 14a, 14b, and which are interposed such that when the rotor 12, 14a, 14b is viewed in transverse cross-section, as shown in Figure 3, one thread is diametrically opposite the other. The power rotor 12 has the shape of a generally cylindrical shaft 22 with the threads 20, 20', two generally helical ridges, extending radially outwardly around the shaft 22. The idler rotors 14a, 14b each have the shape of a generally cylindrical shaft 24a, 24b with the threads 26a, 26a', 26b, 26b', two generally helical grooves, extending radially inwardly into each shaft 24a, 24b.
An inlet port (not shown) is provided in the pump housing 16 adjacent a first end of the rotors 12, 14a, 14b and an outlet port 30 is provided in the pump housing 16 adjacent a second, opposite end ofthe rotors 12, 14a, 14b.
The pump is operated as follows.
The motor is activated to cause rotation of the power rotor 12 about axis A, which in turn causes rotation of the idler rotors 14a, 14b in the housing 16 about axes B and C respectively. Fluid is drawn into the inlet 28 between the threads 20, 20', 26a, 26a', 26b, 26b' at the first ends of the rotors. As the rotors turn, the meshing of the threads produces fluid chambers bounded by the thread roots loathe thread flanks F and the pump housing 16. Fluid becomes trapped in the fluid chambers and continued rotation of the screws causes the fluid chambers to move from the first end of the rotors 12, 14a, 14b to the second end of the rotors 12, 14a, 14b. Fluid is ejected from the pump 10 via the outlet port 30 as a consequence of fluid being displaced from the fluid chamber as the screw threads at the second end of the rotors 12, 14a, 14b mesh.
The pitch of each thread 20, 20', 26a, 26a', 26b, 26b', i.e. the distance between corresponding points on adjacent loops of the thread, marked as P on Figure 2, is less than 1.6 times the outer diameter of the power rotor, marked as OD in Figure 3, and is preferably less than the outer diameter OD of the power rotor 12, but at least 0.5 times the outer diameter OD ofthe power rotor 12.
::t Be.: lo:.
|.. l. : : 44: À . For example, for a power rotor outer diameter OD of between 1 Omm and 12mm, and idler rotor outer diameters OD of around 7.2 mm, the pitch P of the threads 20, 20', 26a, 26a', 26b, 26b' is typically from 7 up to 9mm.
The depth of each thread 20, 20', 26a, 26a', 26b, 26b', marked on Figure 3 as TD, is less than 0.2 times the outer diameter of the power rotor 12. In this example, the outer diameter OD of the power rotor 12 is between 10mm and 12mm and the thread depth TD is between 1.4 and 1.7mm inclusive.
In known intermeshing screw pumps, the pitch P of the threads 20, 20', 26a, 26a', 26b, 26b' is typically twice the outer diameter OD of the power rotor 12, and may be up to 2.4 times the outer diameter OD of the power rotor 12, whereas the thread depth TD is 0.2 times the outer diameter OD of the power rotor 12.
Thus, for a given pump length, more fluid chambers are formed in a pump 10 according to the invention than in a conventional pump, or, put another way, for a given number of fluid chambers, the pump 10 is shorter than a conventional pump. Since the pressure of fluid output from an intermeshing screw pump 10 depends on the number of fluid chambers formed by the screw threads 20, 20', 26a, 26a', 26b, 26b' of the rotors 12, 14a, 14b, for a given pressure output, the pump 10 may be shorter than a conventional pump.
Moreover, since the thread depth TD is lower than for a conventional pump, for a given power rotor 12 root diameter RD, the overall pump diameter may be smaller than for a conventional pump.
Thus the pump 10 can be used where space is restricted such as in automotive applications, for example in an electrically operated power pack in which the pump is activated to produce pressurised fluid and the pressurised fluid is used to move an actuator member. Such an electrically powered power pack may be required for applications such as power steering.
It is advantageous to use a screw pump in such applications as screw pumps are relatively quiet compared with vane and gear pumps, for examples, r l l: Be: :: tl: and require only a relatively small motor in order to run at the high speeds, e.g. over 7,500 rpm, required to produce the fluid volume output needed for such applications.
The reduction in thread depth TD described above does have a consequence of reducing the volume of each fluid chamber in the pump 10, which in turn reduces the volume output of the pump when operating at a particular speed, but this can be compensated for by increasing the speed of rotation of the pump.
Use of the screw thread form described above also improves the efficiency of the pump 10. A screw pump using a conventional thread form which was scaled down to produce a pump of the same dimensions as a pump according to the invention, operated at under 20% efficiency, whereas a relatively high efficiency (over 60%) has been achieved using the screw thread form described above.
During operation of the pump 10 leakage of fluid from the fluid chambers occurs along leakage paths between the flanks F of the meshing threads 20, 20', 26a, 26a', 26b, 26b', and between the exterior surfaces of the rotors 20, 14a, 14b and the housing 16 or the thread roots R. Such leakage reduces the efficiency of the pump 10.
Reduction of the thread depth TD reduces the size of the leakage path between the flanks F of meshing threads 20, 20', 26a, 26a', 26b, 26b', and reduction of the pitch reduces the size of the leakage paths between the outer surfaces and the root surfaces R of the rotors 12, 14a, 14b, and it is understood that this contributes towards the improved efficiency of the pump 10.
Use of the above described screw thread form also decreases the costs of manufacturing the pump 10.
The rotors 12, 14a, 14b are typically made by machining the thread forms into a cylindrical metal rod, and the tolerances must be tight in order to ensure that the threads mesh properly without leaving large fluid leakage paths , , À À 1 ::' :e l:. :e and without the meshing threads becoming jammed during rotation of the rotors 12, 14a, 14b. The longer the rotor, the more difficult it becomes accurately to control a machine tool to produce a tight tolerance thread over the entire rotor length. Thus, for a given number of thread turns, it is easier, and hence less expensive, to manufacture a tight tolerance thread on the rotors 12, 14a, 14b, of the present invention than it would be to manufacture a longer rotor with a conventional thread form.
In addition, the complexity and hence cost of machining a tight tolerance thread form decreases with a reduced thread depth. This is at least partly because a reduction in root diameter RD increases the likelihood of the rotor 12, 14a, 14b bending during machining, and thus more care must be taken to produce a thread form of the required low tolerance. For a given rotor outer diameter OD, the root diameter RD of the rotors 12, 14a, 14b of the present invention is correspondingly larger than the root diameter RD of rotors of conventional design.
Various modifications may be made to the pump 10 within the scope of the invention.
For example, the rotors 12, 14a, 14b may be provided with fewer or more than two threads or flights per rotor. It would be possible, for example to provide three interposed threads on each rotor 12, 14a, 14b each having a pitch and thread depth as described above.
It is also possible to provide only a single idler rotor, or to provide more than two idler rotors. Moreover, where two or more idler rotors are provided, it is not necessary for the central rotor to be connected to the driving means - one of the outer rotors may be connected to the driving means, or both the central rotor and at least one of the outer rotors may be connected to the driving means.
It is also possible that the central rotor may be fixed relative to the driving means, and rotation of the rotors achieved by rotation of the pump ' :: 'c: c.e.. se e' t housing about the longitudinal axis of the central rotor, for example by incorporating the pump housing in the rotor of an electric motor.
Finally, it is not necessary for the threads 20, 20' on the power rotor 12 each to have the form of a ridge, and the threads 26a, 26a', 26b, 26b' in the idler rotors 1 4a, 1 4b to each have the form of a groove. It is possible to reverse this and provide the threads of the power rotor 12 as grooves, and the threads of the idler rotors 14a, 14b as ridges.
The features disclosed in the foregoing description, or the following claims, or the accompanying drawings, expressed in their specific forms or in terms of a means for performing the disclosed function, or a method or process for attaining the disclosed result, as appropriate, may, separately, or in any combination of such features, be utilised for realising the invention in diverse forms thereof.

Claims (15)

e el.' .e t:: .. e. rrIc CLAIMS
1. A pump including at least two rotors each being provided with a generally helical screw thread, one rotor having a larger outer diameter than the other, the rotors being mounted for rotation in a housing such that the screw threads of the rotors mesh and rotation of one rotor causes rotation of the other rotor, wherein the pitch of the threads is less than 1.6 times the outer diameter of the larger diameter rotor.
2. A pump according to claim 1 wherein the pitch of the threads is less than 1.2 times the outer diameter of the larger diameter rotor.
3. A pump according to claim 2 wherein the pitch of the threads is less than the outer diameter of the larger diameter rotor.
4. A pump according to claim 3 wherein the pitch of the threads is 0.75 times the outer diameter of the larger diameter rotor.
5. A pump according to any preceding claim wherein the pitch of the threads is at least 0.5 times the outer diameter of the larger diameter rotor.
6. A pump according to any preceding claim wherein the thread depth of the screw threads is less than 0.2 times the outer diameter of the larger diameter rotor.
7. A pump wherein the thread depth of the screw threads is less than 0. 175 times the outer diameter of the power rotor.
::.' te. :: seeedIt:
8. A pump according to claim 7 wherein the thread depth of the screw threads is less than 0.15 times the outer diameter of the power rotor.
9. A pump according to claim 8 wherein the thread depth of the screw threads is at least 0.1 times the outer diameter of the power rotor.
10. A pump according to any preceding claim wherein each rotor is provided with two generally helical interposed screw threads.
11. A pump according to any preceding claim wherein the pump includes a power rotor and two idler rotors, the power rotor being arranged between the two idler rotors.
12. A pump substantially as hereinbefore described with reference to and/or as shown in the accompanying drawings.
13. A rotor for a pump, the rotor being provided with a generally helical screw thread, wherein the pitch of the thread is less than 1.6 times the outer diameter of the rotor.
14. A rotor substantially as hereinbefore described with reference to and/or as shown in the accompanying drawings.
15. Any novel feature or novel combination of features as hereinbefore described and/or shown in the accompanying drawings.
GB0310591A 2003-05-08 2003-05-08 Pump with screw pitch less than 1.6 times the diameter Withdrawn GB2401400A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
GB0310591A GB2401400A (en) 2003-05-08 2003-05-08 Pump with screw pitch less than 1.6 times the diameter
US10/839,992 US7232297B2 (en) 2003-05-08 2004-05-06 Screw pump
DE602004004309T DE602004004309T2 (en) 2003-05-08 2004-05-07 screw pump
PT04010909T PT1475537E (en) 2003-05-08 2004-05-07 Screw pump
ES04010909T ES2283899T3 (en) 2003-05-08 2004-05-07 SCREW PUMP.
AT04010909T ATE351981T1 (en) 2003-05-08 2004-05-07 SCREW PUMP
EP04010909A EP1475537B1 (en) 2003-05-08 2004-05-07 Screw pump
US11/657,502 US7452194B2 (en) 2003-05-08 2007-01-24 Screw pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0310591A GB2401400A (en) 2003-05-08 2003-05-08 Pump with screw pitch less than 1.6 times the diameter

Publications (2)

Publication Number Publication Date
GB0310591D0 GB0310591D0 (en) 2003-06-11
GB2401400A true GB2401400A (en) 2004-11-10

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB0310591A Withdrawn GB2401400A (en) 2003-05-08 2003-05-08 Pump with screw pitch less than 1.6 times the diameter

Country Status (1)

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110397588A (en) * 2019-07-29 2019-11-01 山东劳伦斯流体科技有限公司 A kind of high-pressure heavy-load Quimby pump

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693763A (en) * 1951-10-25 1954-11-09 Laval Steam Turbine Co Nonpositive screw pump or motor
DE1004930B (en) * 1951-10-25 1957-03-21 Imo Industri Ab Screw pump
US6158996A (en) * 1996-09-12 2000-12-12 Ateliers Busch S.A. Screw rotor set
GB2352777A (en) * 1999-05-07 2001-02-07 Ind Tech Res Inst Double screw rotor assembly
US6312242B1 (en) * 2000-05-12 2001-11-06 Industrial Technology Research Institute Asymmetric double screw rotor assembly

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693763A (en) * 1951-10-25 1954-11-09 Laval Steam Turbine Co Nonpositive screw pump or motor
DE1004930B (en) * 1951-10-25 1957-03-21 Imo Industri Ab Screw pump
US6158996A (en) * 1996-09-12 2000-12-12 Ateliers Busch S.A. Screw rotor set
GB2352777A (en) * 1999-05-07 2001-02-07 Ind Tech Res Inst Double screw rotor assembly
US6312242B1 (en) * 2000-05-12 2001-11-06 Industrial Technology Research Institute Asymmetric double screw rotor assembly

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