The present invention relates to a friction vacuum pump comprising a fixed element bearing rows of stator blades and a rotating element bearing rows of rotor blades whereby the rows of stator blades and rotor blades are arranged concentrically with respect to the axis of rotation of the rotating element and engage with each other.
Turbomolecular vacuum pumps are a kind of friction pump, see for example U.S. Pat. No. 5,577,883. They are designed just like a turbine with rows of rotor and stator blades. Stator and rotor are substantially cylindrical in shape and are arranged coaxially with respect to the rotational axis of the rotating component. The longitudinal axes of the stator and rotor blades which engage in alternating fashion, extend radially so that a substantially axial direction for the pumping action results. One or several pairs of a row of rotor blades and a row of stator blades form a pump stage. The pumping properties (pumping capacity, compression) of a pump stage are adjusted through the design of the blades, preferably through their angle of incidence.
In the instance of turbomolecular vacuum pumps according to the state-of-the-art, there exists a minimum requirement for the number of pump stages, which can not be reduced any further. Thus turbomolecular vacuum pumps according to the state-of-the-art have to be relatively long, in particular since the drive motor contributes further to the axial length. Moreover, in the instance of the known turbomolecular vacuum pumps only one component—commonly the rotor—can be made of a single piece, whereas the other component—commonly the stator—needs consist of a multitude of components in order to be able to assemble the engaging rows of stator blades.
It is the task of the present invention to create a turbomolecular vacuum pump of the aforementioned kind which is significantly shorter in the axial direction.
This task is solved by the present invention through characterising features of the patent claims.
The present invention allows the manufacture of friction pumps, the axial length of which—disregarding the drive motor—does not significantly extend beyond the length of the stator and rotor blades. Since the blades extend axially, both rotor and stator may be made of a single part respectively.
It is expedient to operate radially pumping pumps of the kind according to the present invention, in such a manner that the pumped gases flow from outside to inside. Here the utilisation of the differing circumferential speeds of the blades offers an advantage, since corresponding to the pressure range the frictional losses can be reduced. Moreover, the losses owing to backflowing gas can be much reduced in the direction of the pumping action compared to the axial compressor, since the stator may be manufactured as a single part and since no tolerances will add owing to a multitude of components needing to be joined. Equally the losses due to backflowing gas flowing around the tips of the blades are minimised, since here too the slots can be reduced significantly by aligning the carriers.
A further advantage exists in that the detailed rotor disks can be manufactured on lathes or erosion machines. Both techniques are relatively cost-effective. With the attainable reduction in the number of parts, the present invention represents a true alternative in meeting today's pressure on prices.
Moreover, it is expedient to combine known axially compressing turbomolecular vacuum pumps with radially compressing friction vacuum pumps designed according to the present invention. Pump systems of this kind allow the placement of the drive motor on the high vacuum side without the need for the motor and the bearings to consist of high-vacuum capable materials. Finally, there result advantages relating to the bearing arrangement for the rotating component. Long rotors require, in particular when they are to be suspended in a cantilevered manner, relatively involved bearings which in the instance of the relatively short rotors in the friction vacuum pumps according to the present invention are no longer necessary.
Still further advantages of the present invention will become apparent to those of ordinary skill in the art upon reading and understanding the following detailed description of the preferred embodiments.
The invention may take form in various components and arrangements of components, and in various steps and arrangements of steps. The drawings are only for purposes of illustrating a preferred embodiment and are not to be construed as limiting the invention.
In the embodiment in accordance with
In the embodiment of
Vacuum pumps are preferably operated such that the pumping chamber decreases in the direction in which the gases are pumped. Friction vacuum pumps 1 according to the present invention offer this property already when the gases are being pumped from outside to inside (c.f. the arrows 16 drawn in to
Of course, operation of the friction pumps is possible in the reverse pumping direction. To this end only the direction of rotation for rotor 6 needs to be reversed. An example of a friction pump 1 being operated in this manner is depicted in
Depicted in
In the design example according to
Drawn in arrows 27 indicate that the connection port 9 has the function of an inlet and that the subsequent radially compressing stages (four, in all) pump from inside to outside and from outside to inside in alternating fashion. The outlet is designated as 26. It is located inside and surrounds the drive shaft 14 so that in this area no sealing agents are required. By adapting the length of the blades from the inlet to the outlet (decrease) it is again possible to influence the volume of the pump chamber.
The friction pumps 1 and 31 are located in a joint, approximately cylindrically-shaped casing 35 with an inlet 36 at the side. A shaft 39 supported by bearings at both face sides (bearings 37, 38) carries the respective rotating components of the pumping stages (rotor disk 6 of the radially compressing pump 1, rotor 41 of the turbomolecular pumping stage 32, cylinder 42 of the Holweck pumping stage 33). The side inlet 36 of the combined pump opens out between the radially compressing pumping stage 1 and the axially compressing pump 31. The outlet 44 of the combined pump is located on the delivery side of the molecular pumping stage 33. The drawn in arrows 45 and 46 indicate that the radially compressing pump stage 1 takes in the gases which are to be pumped in the area of its periphery, and that the axially compressing pump 31—as is common—takes in the gases in the area of its high-vacuum side. The gases being pumped by pump stage 1 pass via a bypass 47 directly to the intake side of the Holweck pumping stage 33.
The special characteristic of the solution in accordance with drawing
All embodiments in accordance with
In the embodiment in accordance with
If pumping of a partial flow from the inlet 36 into the area of the inlet 36′ is not desired, a further axially compressing friction vacuum pump 1′ may be provided for separating the inlets 36, 36′ (
The embodiment in accordance with
In the embodiments in accordance with
The presented examples demonstrate that the combination and the sequence of the pumping stages can be selected at will, and can be adapted to the specific application requirements. The arrangement of the pumping stages allows for more compact designs with bearings at both shaft ends. Thus the shafts can be made as stiff as needed. This results in designs which are unproblematic as to the rotor dynamics, and which also exhibit a good balancing characteristic. In that almost any number of stages can be attached to the shaft just like the components of a modular system, it is easier to implement a high-vacuum pump which compresses against the atmosphere.
The invention has been described with reference to the preferred embodiment. Obviously, modifications and alterations will occur to others upon reading and understanding the preceding detailed description. It is intended that the invention be construed as including all such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.
Number | Date | Country | Kind |
---|---|---|---|
100 04 271 | Feb 2000 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/EP01/00726 | 1/24/2001 | WO | 00 | 11/12/2002 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO01/57402 | 8/9/2001 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3947193 | Maurice | Mar 1976 | A |
5577883 | Schütz et al. | Nov 1996 | A |
5848873 | Schofield | Dec 1998 | A |
6135709 | Stones | Oct 2000 | A |
6235709 | Kodama et al. | May 2001 | B1 |
6508631 | Smith et al. | Jan 2003 | B1 |
6705844 | Englander | Mar 2004 | B1 |
Number | Date | Country |
---|---|---|
235102 | Nov 1944 | CH |
PS605902 | Nov 1934 | DE |
PS1845883 | Oct 1961 | DE |
PS107118 | Jul 1974 | DE |
2412624 | Oct 1974 | DE |
0 805 275 | Nov 1997 | EP |
2589529 | May 1987 | FR |
479427 | Jan 1938 | GB |
63-297793 | Mar 1989 | JP |
1252552 | Aug 1986 | SU |
Number | Date | Country | |
---|---|---|---|
20040013514 A1 | Jan 2004 | US |