GB2228976A - Helical gear pump - Google Patents

Helical gear pump Download PDF

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Publication number
GB2228976A
GB2228976A GB8902230A GB8902230A GB2228976A GB 2228976 A GB2228976 A GB 2228976A GB 8902230 A GB8902230 A GB 8902230A GB 8902230 A GB8902230 A GB 8902230A GB 2228976 A GB2228976 A GB 2228976A
Authority
GB
United Kingdom
Prior art keywords
rotor
locations
stator
coating
interference
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.)
Granted
Application number
GB8902230A
Other versions
GB8902230D0 (en
GB2228976B (en
Inventor
Lindsay Thomas Mathewson
Geoffrey Harold May
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.)
NOV Process and Flow Technologies UK Ltd
Original Assignee
Mono Pumps 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 Mono Pumps Ltd filed Critical Mono Pumps Ltd
Priority to GB8902230A priority Critical patent/GB2228976B/en
Publication of GB8902230D0 publication Critical patent/GB8902230D0/en
Priority to EP19900300894 priority patent/EP0381413A3/en
Priority to NO900446A priority patent/NO172200C/en
Priority to FI900500A priority patent/FI900500A0/en
Publication of GB2228976A publication Critical patent/GB2228976A/en
Priority to US07/746,174 priority patent/US5120204A/en
Application granted granted Critical
Publication of GB2228976B publication Critical patent/GB2228976B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F04C2/10Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member
    • F04C2/107Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member with helical teeth
    • F04C2/1071Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member with helical teeth the inner and outer member having a different number of threads and one of the two being made of elastic materials, e.g. Moineau type
    • F04C2/1073Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member with helical teeth the inner and outer member having a different number of threads and one of the two being made of elastic materials, e.g. Moineau type where one member is stationary while the other member rotates and orbits

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

i 1 HELICAL GEAR PUMP The present invention relates to helical gear pumps.
These comprise an outer stator member with a helical female gear formation of n starts, an inner rotor rotatable within said stator having a helical male gear formation of the same pitch of ntl starts, means being provided to cause the rotor to rotate and orbit relative to the stator.
Usually the rotor has n-1 starts.
Traditionally the outer stator member is formed of a resilient, rubber like material and the rotor is formed of metal, usually steel. Fcr the pump to operate satisfactorily, there must be a good seal at all times formed between the rotor and the stator so that the cavities formed therein, which progress through the pump, are effectively sealed between suction and discharge pressure. The seal is improved if the interference between the rotor and stator is increased, but this causes problems of requiring a greater drive power, heat generation and of wear on the two parts, particularly the stator.
The helical gear formation of the rotor is such as to provide peaks and troughs in the rotor and experience has shown that wear on the rotor is normally initiated close to the rotor major diameter or peak. In order to reduce the amount of wear, it has been proposed to use a coating on the rotor of modified chromium oxide, this being applied by plasma coating. The use of modified chromium oxide as a coating medium results in a thicker deposition of the chromium oxide at the minor diameter or trough i.e. where it is least required. This is due to the complexity of the rotor geometry associated with the coating process which involves rotating the rotor about its normal axis, while applying the chromium oxide coating by means of a gun which traverses the length of the rotor parallel to the axis of rotation. As the rotor is rotated, the peripheral speed at 0 2 the peaks will be higher than at the troughs. Furthermore, as the plasma torch or gun traverses along the length of the rotor, the distance or "gun gap" g between the gun and the rotor varies between g and g+2e, where e is the eccentricity of the rotor.
The combination of varying peripheral speed and varying "gun gap" g lead to an uneven distribution of the coating. Consequently, it has been found that with a conventional rotor, in which the ratio d/e = 5 and P/e 12.5, (where d is the minor diameter, e is the eccentricity and P is the rotor pitch), the coating thickness ratio between the minor diameter and the major diameter (the trough and the peak) has been found to be in excess of 1.5:1. This has two disadvantages. Firstly there is an unnecessary coating of the rotor at the minor diameter and secondly there is a risk of overcoating at the minor diameter, bearing in mind chromium oxide has a maximum thickness after which it peels off, that is its integrity of coating is reduced.
It is now proposed, according to the present invention, to provide a helical gear pump comprising an outer stator member with a helical female gear formation of n starts, an inner rotor rotatable within said stator and having a helical male gear formation of the same pitch of ntl starts, and means to cause said rotor to rotate and orbit relative to said stator, the rotor having a major diameter D, a minor diameter d, a pitch P and an eccentricity e, wherein the interference between the rotor and the stator is arranged to be such that the interference is significantly more at the locations of the minor diameter d than at the locations of the major diameter D.
It has been found that if there is too much interference at the major diameter the capacity of the pump is reduced, largely because the size of the cavities formed between the rotor and stator is reduced by the larger L) 3 diameter rotor. Equally important, however, if there is too much interference at the major diameter the power requirement is increased. The provision of a greater interference at the minor diameter has less effect in both of these connections and ensures that a good seal is produced thereby improving the efficiency of the pump.
In a preferred construction, the interference at the location of the minor diameter d is considerably greater than the interference at the locations of the major diameter and the ratio d/e of the minor diameter d to eccentricity e is at least 8.
-ch P Advantageously the ratio P/e of the rotor pit to the eccentricity e is at least 17.5.
As indicated earlier, improved results can be achieved in pumps of this type if the metal of the rotor is plasma coated with a coating of modified chromium oxide. Advantageously with the structure of the present invention, the base metal of the rotor, prior to plasma coating, is machined so that in the region of the location of majOr diameter D, the thickness of the plasma coating is less and in the region of the locations of minor diameter d, the thickness of the plasma coating is greater than in the remainder of the rotor, while allowing the interference to be significantly more at the locations of the minor diameter d than at the locations of the major diameter D.
In order that the present invention may be more readily understood, the following description is given, merely by way of example, reference being made to the accompanying drawing in which:-
Figure 1A is a cross sectional schematic view showing the stator form and rotor path of one embodiment of helical gear pump according to the invention; Figure 1B is a similar view of a conventional pump; 4 Figure 2 is a schematic side elevation showing the coating of a rotor according to the invention; and Figure 3 is a graph showing the relationship between capacity and pressure of the convention pump and a pump according to the present invention.
Referring first to Figure 1A and 1B, the stator form is shown in full lines and the path of the rotor is shown in dotted lines. In the conventional structure of Figure 1B, the rotor path is substantially coterminous with the stator form shown in full line. The stator form consists of two substantial semi-circular zones 10,12 and, on each side, two sets of straight line portions 14,14,16,16, the sets 14,16 meeting at the horizontal centre line 18 of the stator form. At the junction of the semi circular portions 10,12 with the straight line portions 14,16, experience has shown that there tends to be a leak path as is shown in the enlarged encircled portion in Figure 1B.
With the structure according to the present invention, the stator form is modified slightly so that the portions 14,16 essentially form a straight line. Also the dimensions of the rotor are chosen so that there is a significant interference as can be seen by the fact that the chain dotted indication of the rotor path 20 is shown, at least along the straight line portions 14,16, and a significant part of the semi-circular portions 10,12 of the stator forms, to be outside the stator form.
On the other hand, however, the interference at the locations of the major diameter are not significantly changed so that the interference at the locations at the minor diameter is significantly greater than the interference at the locations of the major diameter.
If reference is now made to Figure 2 of the drawings it will be seen that the rotor 22 is shown as being sprayed with a coating, such as modified chromium oxide, by a plasma gun 24. At the vicinities of the peaks of 26 of the rotor the gap of the rotor from the plasma gun is shown as a distance 9. It will be appreciated that the gap at the troughs 28 of the rotor will be g + 2e. This tends to produce a greater thickness of coating at the troughs 28 than at the peaks 26. Therefore the base metal of the rotor is machined, with a construction according to the invention, so that in the region of the locations of major diameter, that is at the peaks 26, the thickness of the plasma coating is less and in the region of the locations of minor diameter, that is in the troughs, the thickness of the plasma coating is greater than in the remainder of the rotor, while allowing the interference to be significantly more at the locations of the minor diameter than at the locations of the major diameter.
In this way optimum coating can be achieved without there being any fear of the integrity of the coating with the base metal being broken down and yet the desired interference which is greater at the locations of minor diameter than at the locations of the major diameter can also be arrived at.
In a preferred arrangement, the ratio d/e of the minor diameter d to the eccentricity e is at least 8 and the ratio P/e of the pitch P to the eccentricity e is at least 17.5.
If one now looks at Figure 3, one will see that the pressure/capacity curve of the pump according to the invention is shown in full lihe and the corresponding curve for a conventional pump of the same rating is shown in chained dotted lines. It will be seen that firstly there is a greater capacity at all times for the same pressure throughout the whole range of pressure both at the minimum rated speed of the pump and at the maximum rated speed and 6 that there is a lesser drop off in the capacity as the pressure increases from minimum to maximum throughout the speed range of the pump. As can be seen from the comparison of the stator forms, the new form has eliminated the leak paths and this improves the performance of the rotor/stator combination and also prevents abrasive particles becoming trapped in the seal line where they potentially can cause more damage to the rotor.
Wear tests with chromium oxide coated rotors having d/e ratio of 8 and P/e ratio of 17.5 have been extensively tested alongside hard chrome plated rotors having a more orthodox geometry. These wear tests have shown a significant increase in life in favour of chromium oxide coated rotors.
-ry, With a conventional rotor geomet i.e. d/e = 5 and P/e = 12.5, the coating thickness ratio of the minor:major (trough:peak) has been found to be in excess of 1.5:1. The geometry has according to the invention, in which d/e = 8 and P/e = 17.5 substantially reduces this ratio to 1.3:1 this results in the two advantages that it reduces the unnecessary coating at the minor diameter and reduces the risk of over coating at the major diameter which would result in the coating peeling off.
7

Claims (6)

1. A helical gear pump comprising an outer stator member with a helical female gear formation of n starts, an inner rotor rotatable within said stator and having a helical male gear formation of the same pitch of ntl starts and means to cause said rotor to rotate and orbit relative to said stator, the rotor having a major diameter D, a minor diameter d, a pitch P and an eccentricity e, wherein the interference between the rotor and stator is arranged to be such that the interference is significantly more at the -er d than at the locations of locations of the minor diamet the major diameter D.
2. A pump according to Claim 1, wherein the ratio d/e,of the minor diameter d to eccentricity e is at least 8.
3. A pump according to Claim 1 or 2, wherein the ratio P/e of the pitch P to the eccentricity e is at least 20 17.5.
4. A pump according to any preceding Claim, wherein the metal of the rotor is plasma coated with a coating of modified chromium oxide.
5.
A pump according to Claim 4, wherein the base metal of the rotor, prior to plasma coating, is machined, so that in the region of the locations of major diameter D, the thickness of the plasma coating is less and, in the region of the locations of minor diameter d, the thickness of the plasma coating is greater than in the remainder of the rotor, while allowing the interference to be significantly more at the locations of the minor diameter d than the locations of the major diameter D.
-11 8
6. A helical gear pump substantially as herein before described with reference to as illustrated in the accompanying drawing.
4 Published 1990 at The Patent Office. State House.66"7a High Holborn. London WClR 4TP. FLL-.hercopiesmaybeobtainedfrom The fttoentOffic e Sales Branch, St Mary Cray. Orpington, Kent BRS 3RD. Printed by Multiplex techniques ltd, St Mary Cray, Kent, Con. 2,,87
GB8902230A 1989-02-01 1989-02-01 Helical gear pump Expired - Fee Related GB2228976B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB8902230A GB2228976B (en) 1989-02-01 1989-02-01 Helical gear pump
EP19900300894 EP0381413A3 (en) 1989-02-01 1990-01-29 Helical gear pump
NO900446A NO172200C (en) 1989-02-01 1990-01-31 TURN GEAR PUMP
FI900500A FI900500A0 (en) 1989-02-01 1990-01-31 SKRUVPUMP.
US07/746,174 US5120204A (en) 1989-02-01 1991-08-15 Helical gear pump with progressive interference between rotor and stator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8902230A GB2228976B (en) 1989-02-01 1989-02-01 Helical gear pump

Publications (3)

Publication Number Publication Date
GB8902230D0 GB8902230D0 (en) 1989-03-22
GB2228976A true GB2228976A (en) 1990-09-12
GB2228976B GB2228976B (en) 1993-08-11

Family

ID=10650971

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8902230A Expired - Fee Related GB2228976B (en) 1989-02-01 1989-02-01 Helical gear pump

Country Status (4)

Country Link
EP (1) EP0381413A3 (en)
FI (1) FI900500A0 (en)
GB (1) GB2228976B (en)
NO (1) NO172200C (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5498142A (en) * 1995-05-30 1996-03-12 Kudu Industries, Inc. Hardfacing for progressing cavity pump rotors
GB2341423A (en) * 1998-09-09 2000-03-15 Mono Pumps Ltd Progressing cavity pump
CN105240269A (en) * 2014-06-26 2016-01-13 水利部科技推广中心 Double-end U-type thread divided spiral micro-nano bubble device

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5395221A (en) * 1993-03-18 1995-03-07 Praxair S.T. Technology, Inc. Carbide or boride coated rotor for a positive displacement motor or pump
RU2228443C1 (en) * 2003-03-11 2004-05-10 Общество с ограниченной ответственностью фирма "Радиус-Сервис" Rotor of screw hydraulic machine
DE102017104768A1 (en) 2017-03-07 2018-09-13 Seepex Gmbh Cavity Pump

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB629454A (en) * 1947-11-04 1949-09-20 Fmc Corp Improvements in gear type pumps
GB1001336A (en) * 1963-07-25 1965-08-18 Mono Pumps Ltd Helical gear pump
GB1542786A (en) * 1976-03-09 1979-03-28 Mec Et De Metallurg Sa Soc Gen Moineau-type screw pump stators
US4773834A (en) * 1983-08-16 1988-09-27 Patrick J. Quinn Progressive cavity pump

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1553146A1 (en) * 1965-09-16 1970-02-05 Netzsch Maschinenfabrik Runner for screw pumps
DE1553148A1 (en) * 1966-03-12 1969-07-03 Netzsch Maschinenfabrik Runner for screw pumps
DE2017620C3 (en) * 1970-04-13 1981-07-16 Gummi-Jäger KG GmbH & Cie, 3000 Hannover Eccentric screw pump

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB629454A (en) * 1947-11-04 1949-09-20 Fmc Corp Improvements in gear type pumps
GB1001336A (en) * 1963-07-25 1965-08-18 Mono Pumps Ltd Helical gear pump
GB1542786A (en) * 1976-03-09 1979-03-28 Mec Et De Metallurg Sa Soc Gen Moineau-type screw pump stators
US4773834A (en) * 1983-08-16 1988-09-27 Patrick J. Quinn Progressive cavity pump

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5498142A (en) * 1995-05-30 1996-03-12 Kudu Industries, Inc. Hardfacing for progressing cavity pump rotors
US5645896A (en) * 1995-05-30 1997-07-08 Kudu Industries Inc. Method of applying a filled in metal carbide hard facing to the rotor of a progressing cavity pump
GB2341423A (en) * 1998-09-09 2000-03-15 Mono Pumps Ltd Progressing cavity pump
GB2341423B (en) * 1998-09-09 2002-04-24 Mono Pumps Ltd Progressing cavity pump
CN105240269A (en) * 2014-06-26 2016-01-13 水利部科技推广中心 Double-end U-type thread divided spiral micro-nano bubble device

Also Published As

Publication number Publication date
EP0381413A3 (en) 1990-12-05
NO900446D0 (en) 1990-01-31
NO900446L (en) 1990-08-02
EP0381413A2 (en) 1990-08-08
NO172200C (en) 1993-06-16
GB8902230D0 (en) 1989-03-22
FI900500A0 (en) 1990-01-31
GB2228976B (en) 1993-08-11
NO172200B (en) 1993-03-08

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940201