DRY PUMP FOR GAS AND SET OF A PLURALITY OF DRY PUMPS FOR GAS

Abstract

A dry pump for gases comprises a first rotor (1) comprising a first lobe portion (1A) and a first screw (16), as well as a second rotor (2) comprising a second lobe portion (2A) and a second screw (2B). A casing delimits an internal volume in which are located together the first and second screws (1B, 2B) and the first and second lobe portions (1A, 2A). Each of the first and second screws (1B, 2B) comprises a threading invariable along its length. The first and second rotors (1, 2) turn in opposite directions and are located in successive configurations. In a first configuration of the rotors, the first and second lobe portions (1A, 2A), a portion of the first screw (16), a portion of the second screw (2B) and the casing together delimit a chamber (30) which is closed. In a second configuration of the rotors, the chamber (30) has a smaller capacity than in the first configuration. In a third configuration of the rotors, the chamber (30) is displaced entirely at the first and second screws (1B, 2B) and isolated from the lobe portions.

Claims

1. Dry pump for gases, comprising: a first rotor comprising a first lobe portion and a first screw, a second rotor comprising a second lobe portion and a second screw, and a casing in which the first and second rotors are mounted and rotatable in such a way that the first and second screws mesh and the first and second lobe portions engage one with the other, the casing delimiting an internal volume in which are located together the first and second screws and the first and second lobe portions, at least one inlet coming out into the internal volume at the first and second lobe portions, at least one outlet from the internal volume being located opposite the inlet relative to the first and second screws, each of the first and second screws comprising a threading invariable along its length, the first and second rotors being rotatable in opposite directions in such a way as to be able to be located successively in: a first configuration in which the first and second lobe portions, a portion of the first screw, a portion of the second screw and the casing together delimit a chamber which is closed, a second configuration in which the chamber is always delimited by the first and second lobe portions, a portion of the first screw, a portion of the second screw and the casing in such a way as to be closed and have a smaller capacity than in the first configuration, a third configuration in which the chamber is displaced entirely at the first and second screws and isolated from the lobe portions at least by a helical thread of the threading of the first screw, a helical thread of the threading of the second screw and a blocking made by an intersection of the helical thread of the first screw and of the helical thread of the second screw, and a fourth configuration in which the chamber is displaced at a downstream end of the first and second screws and is in communication with the outlet.

2. Dry pump for gases according to claim 1, wherein the first and second lobe portions comprise lobes each of which extends by one of the helical threads of the threadings of the first and second screws.

3. Dry pump for gases according to claim 2, wherein a number of lobes of the first lobe portion is equal to a number of helical threads of the threading of the first screw, a number of lobes of the second lobe portion being equal to a number of helical threads of the threading of the second screw.

4. Dry pump for gases according to claim 1, wherein the outlet is located at a distance from the first and second screws.

5. Dry pump for gases according to claim 1, wherein the chamber is one of a plurality of successive chambers that the first and second rotors and the casing together delimit.

6. Dry pump for gases according to claim 5, wherein regardless of respective angular positions of the first and second rotors, there are always two closed chambers among the successive chambers.

7. Dry pump for gases according to claim 5, wherein one of the successive chambers is a collecting chamber which has the outlet from the internal volume.

8. Dry pump for gases according to claim 7, wherein the threading of the first screw and the threading of the second screw delimit helical grooves, downstream ends of these helical grooves being open and coming out into the collecting chamber regardless of respective angular positions of the first and second rotors.

9. Dry pump for gases according to claim 1, wherein the first rotor is a male rotor, the second rotor being a female rotor.

10. Dry pump for gases according to claim 1, wherein the second rotor comprises one more lobe than the first rotor.

11. Dry pump for gases according to claim 1, wherein the first rotor comprises a plurality of lobes which number two, the second rotor comprising a plurality of lobes which number three.

12. Dry pump for gases according to claim 1, wherein the first rotor has a cross section which is the same at the first lobe portion and at the first screw, apart from its angular orientation, while the second rotor has a cross section which is the same at the second lobe portion and at the second screw, apart from its angular orientation.

13. Dry pump for gases according to claim 1, wherein the first rotor comprises at least two monobloc elements, kept together, which are a first monobloc element comprising at least the first screw and a second monobloc element comprising at least one part of the first lobe portion.

14. Set of a plurality of dry pumps for gases according to claim 1, wherein the first screws of a first dry pump for gases of the set and of a second dry pump for gases of the set are identical, the second screws of the first dry pump for gases and of the second dry pump for gases being identical, the first and second lobe portions of the first dry pump for gases having an axial dimension which is a first axial dimension, the first and second lobe portions of the second dry pump for gases having an axial dimension which is a second axial dimension different from the first axial dimension.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0029] Other advantages and features will emerge more clearly from the description which follows of a particular embodiment of the invention, given by way of non-limiting example, and represented in the annexed drawings of which:

[0030] FIG. 1 is a schematic view and axial section of a dry pump for gases according to one embodiment of the invention;

[0031] FIG. 2 is a view in perspective which represents two constituent rotors of the pump of FIG. 1 and which is simplified in that the shafts of these rotors are omitted;

[0032] FIG. 3 is a lateral and exploded view, which represents a single one of the two rotors of the pump of FIG. 1 and which is simplified in that the shaft of the rotor represented is omitted;

[0033] FIG. 4 is a view which is simplified like FIGS. 2 and 3, which represents the same rotors as FIG. 2, as well as chambers partially delimited by these rotors in the pump of FIG. 1, and where the rotors are seen from one end;

[0034] FIG. 5 is a view in perspective which is simplified like FIGS. 2 and 3 and which represents the same rotors as FIG. 2, as well as chambers partially delimited by these rotors in the pump of FIG. 1;

[0035] FIG. 6 is a view in perspective representing one chamber from among the chambers visible in FIGS. 4 and 5;

[0036] FIG. 7 is a view in perspective which represents the same chamber as FIG. 6 but later, that is to say at a moment after the moment at which this chamber is such as represented in FIG. 6;

[0037] FIG. 8 is a view in perspective which represents the same chamber as FIGS. 6 and 7 but later, that is to say at a moment after that moment at which this chamber is such as represented in FIG. 7; and

[0038] FIG. 9 is a graph which represents the evolution of the capacity of the chamber of FIGS. 6 to 8 in the course of time.

DESCRIPTION OF A PREFERRED EMBODIMENT OF THE INVENTION

[0039] In FIG. 1, a dry pump for gases according to one embodiment of the invention comprises a first rotor 1 and a second rotor 2, which are mounted in a casing 3 in several parts kept assembled.

[0040] A plurality of bearings 5 support a shaft 6 of the first rotor 1 in such a way that this first rotor 1 is rotational on an axis of rotation X.sub.1-X′.sub.1. A plurality of bearings 7 support a shaft 8 of the second rotor 2 in such a way that this second rotor 2 is rotational on an axis of rotation X.sub.2-X′.sub.2 parallel to the axis of rotation X.sub.1-X′.sub.1. In the sense intended here and in the annexed claims, the axial direction is the direction parallel to the axes of rotation X.sub.1-X′.sub.1, and X.sub.2-X′.sub.2, while an axial dimension is a dimension in the direction parallel to the axes of rotation X.sub.1-X′.sub.1, and X.sub.2-X′.sub.2.

[0041] One end of the shaft 8 is coupled to a motor 10 for driving the first and second rotors 1 and 2. Opposite the motor 10, the shaft 8 of the second rotor 2 bears a toothed wheel 11 which meshes with a toothed wheel 12 borne by the shaft 6 of the first rotor 1. The toothed wheels 11 and 12 form a gearing whose gear ratio equal to 3/2 is such that the first rotor 1 turns faster than the second rotor 2.

[0042] The first rotor 1 comprises a first lobe portion 1A and a first screw 1B which follow one another axially without distance between them. The second rotor 2 comprises a second lobe portion 2A and a second screw 2B which follow one another axially without distance between them. The first lobe portion 1A, the first screw 1B, the second lobe portion 2A and the second screw 2B are all in a same internal volume 14, which the casing 3 delimits without compartmentalizing it.

[0043] An inlet 15 for gas intake passes through the casing 3 and comes out into the internal volume 14, at the first and second lobe portions 2A and 2B, of one side of the plane passing through the axes of rotation X.sub.1-X′.sub.1 and X.sub.2-X′.sub.2. An outlet 16 for the discharge of gases passes through the casing 3 and communicates with the internal volume 14, at a collecting chamber 18, which is constituted by a downstream portion of this internal volume 14 and which is located at the outlet of the first and second screws 1B and 2B, that is to say opposite the first and second lobe portions 1A and 2A in relation to these first and second screws 1B and 2B.

[0044] The internal volume 14 is cylindrical at least at the first and second screws 1B and 2B, by being constituted by the union of two interpenetrating cylinders of revolution, the respective axes of which are the axes of rotation X.sub.1-X′.sub.1 and X.sub.2-X′.sub.2. At the first and second lobe portions 1A and 2A, the internal volume 14 is cylindrical in an identical way, at least on the side opposite the inlet 15 in relation to the plane containing the axes of rotation X.sub.1-X′.sub.1 and X.sub.2-X′.sub.2. At the inlet 15, a downstream and lateral portion of the internal volume 14 can constitute an intake chamber where the internal volume 14 is enlarged laterally and where the inlet 15 comes out.

[0045] The reference numerals 17 designate devices, each of which achieves a tightness between the casing 3 and one of the shafts 6 and 8.

[0046] As can be seen in FIG. 2, the first rotor 1 is a male rotor. The first lobe portion 1A comprises a plurality of lobes 20 which are identical and which number two in the embodiment represented. The screw 1B comprises a threading made up of as many helical threads 21 as there are lobes 20. This threading is invariable on the entire length of the screw 1B. Its pitch, its average diameter and its profile, that is to say the shape and the dimensions of its section along an axial plane passing through the axis of rotation X.sub.1-X′.sub.1, are invariable on the entire length of the screw 1B. Each lobe 20 is extended by one of the two helical threads 21, which are identical. The number of lobes 20 can be different from two. The same applies to the number of helical threads 21.

[0047] The second rotor 2 is a female rotor. The second lobe portion 2A comprises a plurality of lobes 22 which are identical and which number three in the embodiment represented. The screw 2B comprises a threading made up of as many helical threads 23 as there are lobes 22. This threading is invariable on the entire length of the screw 2B. Its pitch, its average diameter and its profile, that is to say the shape and the dimensions its section along an axial plane passing through the axis of rotation X.sub.2-X′.sub.2, are invariable on the entire length of the screw 2B. Each lobe 22 is extended by one of the three helical threads 23, which are identical. The number of lobes 22 can be different from two. The same applies to the number helical threads 23.

[0048] The first lobe portion 1A meshes with the second lobe portion 2A. The first and second screws 1B and 2B interlock.

[0049] The first rotor 1 has a cross section which is the same at the first lobe portion 1A and at the first screw 1B, apart from its angular orientation. In an identical way, the second rotor 2 has a cross section which is the same at the second lobe portion 2A and at the second screw 2B, apart from its angular orientation.

[0050] As can be seen well in FIG. 3, the first rotor 1 results from the assembly of a plurality of monobloc elements, of which a first comprises the first lobe portion 1A and of which a second comprises the first screw 1B. The shaft 6 can be part of the first monobloc element of the first rotor 1 or of the second monobloc element of the first rotor 1. Likewise, a third monobloc element of the first rotor 1 can constitute the shaft 6. The second rotor 2 results from the assembly of a plurality of monobloc elements, of which a first comprises the second lobe portion 2A and of which a second comprises the second screw 2B. The shaft 8 can be part of either of the first and second monobloc elements of the second rotor 2. Likewise, a monobloc element distinct from the first and second monobloc elements of the second rotor 2 can constitute the shaft 8.

[0051] At all times, the first rotor 1, the second rotor 2 and the casing 3 delimit jointly a plurality of successive chambers which are visible in FIG. 4, for certain ones, and in FIG. 5, for all. Among these successive chambers are the collecting chamber 18, the intake chamber mentioned above and designated by reference numeral 25 in FIGS. 4 and 5, as well as the chambers 30, 31, 32 and 33.

[0052] When the first and second rotors 1 and 2 are located in the configuration represented in FIGS. 4 and 5, the chambers 30, 31, 32 and 33 are closed. When the dry pump for gases of FIG. 1 operates, the first and second rotors 1 turn in opposite directions, as indicated by the arrows in FIG. 4. Therefore the chambers 30, 31, 32 and 33 evolve, which is illustrated by FIGS. 6 to 8, representing the single chamber 30 at successive moments.

[0053] When the first and second rotors 1 and 2 are located in the configuration represented in FIGS. 4 and 5, the chamber 30 is as shown in FIG. 6. After the first rotor 1 and the second rotor 2 have turned respectively by half a turn and by a third of a turn starting from positions which they have in FIGS. 3 and 4, the chamber 30 is as shown in FIG. 7. When it is as shown in FIG. 7, the chamber 30 has the shape and the position which the chamber 31 has in FIGS. 3 and 4. After the first rotor 1 and the second rotor 2 have turned respectively by one turn and by 2/3 of a turn starting from the positions that they have in FIGS. 3 and 4, the chamber 30 is as shown in FIG. 8. When it is as shown in FIG. 8, the chamber 30 has the shape and the position which the chamber 32 has in FIGS. 3 and 4.

[0054] Described now will be the evolution of the chamber 30 in the course of time, while the first and second rotors turn continuously in opposite directions.

[0055] In FIG. 6, the chamber 30 is closed by being blocked, at its downstream end, that is to say at P1, by the intersection of a helical thread 21 and a helical thread 23. Still in FIG. 6, the first and second lobe portions 1A and 2A, a portion of the first screw 1B, a portion of the second screw 2B and the casing 3 together delimit the chamber 30, which has almost reached its maximum capacity.

[0056] The rotations of the first and second rotors 1 and 2 in opposite directions continue continuously starting from their positions in FIGS. 4 and 5. Therefore, the first and second lobe portions 1A and 2A arrive at a configuration starting from which they together reduce the capacity of the chamber 30 of which the downstream end is still blocked at P1 by the intersection of a helical thread 21 and a helical thread 23. In FIG. 7, the chamber 30 is represented at a selected moment while the first and second lobe portions 1A and 2A reduce together the capacity of the chamber 30. At the same time that the first and second lobe portions 1A and 2A reduce together the capacity of the chamber 30, a compression of the gas present in this chamber 30 occurs.

[0057] While the rotations of the first and second rotors 1 and 2 in opposite directions continue, the compression in the chamber 30 is followed by a blocking of the upstream end of this chamber 30, by the intersection of a helical thread 21 and a helical thread 23. After the blocking of its upstream end occurs, the chamber 30 is as shown in FIG. 8. The blocking of the upstream end of the chamber 30 is located at P2 in this FIG. 8.

[0058] Once the blocking at P2 occurs, the continuation of the rotations of the first and second rotors 1 and 2 in opposite directions causes the chamber 30 to be displaced in axial direction, downstream, but without changing capacity. In other words, there is no compression in the chamber 30 after the blocking at P2 has taken place.

[0059] When the chamber 30 reaches the downstream end of the first and second screws 1B and 2B, there is no compression there again in this chamber 30, since the outlet 16 is at a distance from the first and second screws 1B and 2B.

[0060] The curve C in FIG. 9 is the graphic representation of the capacity V of the chamber 30 as a function of time t.

[0061] It can be seen from the foregoing that the role of the first and second screws 1B and 2B is not to bring about a reduction of the capacity and thus a compression. The first and second screws have as their role to carry out a succession of identical blockages at the blocking point at P1, which retains gas when, in the chamber 30, this gas is compressed by the first and second lobe portions 1A and 2A. The first and second screws also have as a role to carry out a succession of identical blockages at the blocking point at P2, which isolates the gas present in the chamber 30 of the first and second lobe portions 1A and 2A after the compression of this gas.

[0062] As the compression has taken place essentially at the first and second lobe portions 1A and 2A, the heating up due to this compression occurs also essentially at the first and second lobe portions 1A and 2A. Thanks to this, a low temperature rise of the first and second screws 1B and 2B can be obtained, bringing about an efficient cooling of the internal volume 14 at the first and second lobe portions 1A and 2A. Moreover, a low temperature rise of the first and second screws 1B and 2B is advantageous insofar as it is rather complicated to master the consequences of expansions in screws owing to the fact that such screws have complex shapes.