Dynamic seal

Information

  • Patent Grant
  • 6705844
  • Patent Number
    6,705,844
  • Date Filed
    Wednesday, July 31, 2002
    22 years ago
  • Date Issued
    Tuesday, March 16, 2004
    20 years ago
Abstract
A seal is disposed between a rotating part and a stationary part. At least one of the parts is provided with projections which protrude into the seal gap. The seal gap (5) extends approximately radially so that both parts are provided with projections which extend in an axial direction, which are located concentrically in relation to the axis of rotation of the rotating parts and which engage with each other. Said projections are configured in the form of rows of blade-like elements. This effectively seals approximately radially extending seal gaps.
Description




BACKGROUND OF THE INVENTION




The present invention relates to a dynamic seal between a rotating part and a stationary part where at least one of the parts is provided with projections which protrude into the seal gap.




In particular in the instance of vacuum pumps there frequently exists the requirement of having to seal shafts which penetrate a separating wall between two chambers at different pressures. Commonly, labyrinth seals are employed to this end, as is also known from U.S. Pat. No. 3,399,827, for example.




In the instances of seals for gaps extending approximately radially it is known (c.f. U.S. Pat. No. 5,165,872, gap seal


43


in

FIG. 5

) to employ purge gases (nitrogen, argon or alike) to protect, for example, a bearing/motor chamber against the ingress of detrimental gases. The purge gas is admitted into the bearing/motor chamber and passes through the seal for the gap into the pump chamber so that it is ensured that gases can not pass from the pump chamber into the motor chamber.




SUMMARY OF THE INVENTION




It is the task of the present invention to create an effective dynamic seal for gaps extending approximately radially between a rotating and a stationary component. This task is solved through the characterizing features of the patent claims.




Through the employment of projections designed by way of engaging rows of blades, not only can the desired sealing effect be improved; moreover, there exists the possibility of assigning to the seal pumping properties beneficial to the application in each instance. If, for example, a chamber is to be protected against the ingress of gases, the rows of blades, respectively the angle of incidence for the blades forming the rows of blades, may be so selected that the seal provides a pumping action in a direction opposed to the direction of the flow of the detrimental gases.




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.











BRIEF DESCRIPTION OF THE DRAWINGS




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.





FIGS. 1 and 2

are sectional views through an embodiment of the seal in accordance with the present invention;





FIGS. 3 and 4

are section al views through a double flow embodiment;





FIGS. 5 and 6

are embodiments where the rotors are cantilevered;





FIGS. 7

to


9


are embodiments of vacuum pumps equipped with a rotor system having bearings at both face sides.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS





FIGS. 1 and 2

depict a seal


1


in accordance with the present invention with stationary rows of rotor blades


2


and rotating rows of rotor blades


3


, the longitudinal axes of which extend in parallel to the rotational axis


4


of the rotating component. They are arranged in concentric rows about the rotational axis


4


and extend into the gap


5


which is to be sealed. The chambers which are to be mutually sealed off against each other and which are separated by the sealing gap


5


are generally designated as


8


and


9


. The rows of the rotor blades


2


and the rows of stator blades


3


are arranged in alternating fashion. In the area of the gap


5


which is to be sealed they engage and have if a pumping action is desired in a manner basically known changing angles of incidence in the direction of the flow. From

FIG. 2

it is apparent that the blades


2


,


3


are components of the neighboring rotating resp. stationary components


6


and


7


respectively, between which there is located the gap


5


which is to be sealed.




Depicted in

FIGS. 3 and 4

is a double flow embodiment of a seal


1


in accordance with the present invention. An inner group of rows of blades pumps the gases radially towards the inside (arrow


11


), an outer group of rows of blades from inside to outside (arrow


12


). Thus an equally effective separation of the chambers


8


and


9


which are to be sealed is achieved. This arrangement offers the benefit that in the chamber which is to be protected (e.g.


8


) the vapor pressures of components in said chamber will not drop to inadmissibly low levels. In addition, this separation may be supported by the admission of inert gas between the two groups. The inert gas supply is effected through the stationary component


6


. An inlet bore is depicted (also several may be provided) and designated as


14


.




Depicted in

FIG. 5

is the way in which the present invention is applied in a blower


20


. It consists of a drive section


21


in which the drive motor, not depicted, is accommodated, and the gas pumping section


22


. The drive motor drives a shaft


23


which is guided as gas-tight as possible (labyrinth seal


24


) through the flange


25


of the drive's housing. Affixed to the unoccupied end of the shaft


23


is blower wheel


26


. To support the labyrinth seal


24


, a seal


1


in accordance with the present invention has been implemented in the gap


5


between the bottom side of blower wheel


26


and the flange


25


. The flange


25


carries the rows of stator blades


2


, the blower's wheel


26


carries rotating rows of blades


3


arranged concentrically about the shaft


23


and which engage in the area of gap


5


. If the seal


1


shall have the effect of preventing the entry of gases pumped by blower wheel


26


into the motor chamber, then it is expedient to design the seal in such a manner that it exhibits a pumping action directed radially towards the outside.




Depicted in

FIG. 6

is a partial section through a turbomolecular pump


31


, the base section of which is designated as


32


. In the base section


32


with the drive motor


33


, the shaft


34


is supported by bearing


35


. The shaft


34


carries the rotor


36


with its rotor blades


37


, which are located together with the stator blades


38


in the pump chamber


39


. In order to effectively separate this pump chamber


39


from the motor and bearing chamber


41


, a sealing system


1


designed in accordance with the present invention is provided. It comprises stator blades


2


arranged on two levels carried by a ring-shaped component


42


, said component being L-shaped in its sectional view and encompassing the shaft


34


. The rotor


36


is equipped with a recess


43


matching the contour of the ring-shaped component


42


. The rotor blades


3


related to the stator blades


2


are affixed to the rotor


36


. If in an embodiment of this kind a reliable separation of the chambers


39


and


41


is to be achieved for example, then it is expedient to design seal


1


in such a manner that the inner (upper) group of rows of blades


2


,


3


has a pumping action directed towards the motor chamber


41


and the outer (lower) group of rows of blades


2


,


3


has a pumping action directed towards the pump chamber


39


. By admitting and inert gas between the two groups of rows of blades, the separating effect can even be improved. Both the ingress of hydrocarbons from the motor and bearing chamber


41


into the pump chamber


39


, and also the ingress of detrimental (for example, corrosive or toxic) gases from the pump chamber


39


into the motor chamber


41


can be reliably avoided. The benefit also mentioned in connection with

FIGS. 3 and 4

exists.




Depicted in

FIG. 7

is the application of a seal in accordance with the present invention in an axially compressing friction pump


51


according to the state-of-the-art. The friction pump


51


consists of a turbomolecular pumping stage


52


arranged on the suction side and a molecular pumping stage


53


arranged on the delivery side which may be designed as a Holweck pump (as depicted) or as a Gaede, Siegbahn, Englander or side channel pump. The seal


1


and the friction pump


51


are located in a joint housing


55


approximately cylindrical in shape with a side inlet


56


. A shaft


59


supported by bearings (bearings


57


,


58


) at both face sides carries the rotating components in each instance (rotor disk


6


of the seal


1


, rotor


61


of the turbomolecular pumping stage


52


, cylinder


62


of the Holweck pumping stage


53


). The side inlet


56


of the pump


51


opens between the seal


1


and the axially compressing pumping stages


52


,


53


. The outlet


64


of the pump


51


is located on the delivery side of the molecular pumping stage


53


.




The special feature of the solution in accordance with

FIG. 7

is, that the drive motor


68


is located on the high vacuum side of the axially pumping pump


51


(and not, as is common, on the delivery side of the Holweck pumping stage


53


). In that the seal


1


is located between the inlet


56


and the drive motor


68


, a relatively high pressure (for example 1×10


−2


mbar) can be maintained in motor chamber


41


. The usage of high vacuum capable materials in motor chamber


41


is not required.




The embodiment in accordance with

FIG. 8

differs from that in accordance with

FIG. 7

in that the seal


1


has a pumping action directed radially from the outside to the inside. Moreover, a bypass


67


is connected to the motor chamber


41


said bypass being linked to the suction side of the molecular pumping stage


62


. In line with the entered arrows


69


, the gases pumped by the seal


1


enter through the motor chamber


41


into the bypass


67


and from there into molecular pumping stage


53


. In this way, maintaining of a forevacuum pressure in the motor chamber


41


is ensured. Moreover, the seal


1


supports the pumping capacity of the turbomolecular pumping stage


52


without significantly increasing the total length of the pump


51


.




Depicted in

FIG. 9

is an embodiment of a pump


51


for deployment in multi-chamber systems, two chamber systems in this instance. Such systems are, for example, analytical instruments having several chambers which need to be evacuated down to different pressures. Thus the distance from the intake ports is given, often resulting in state-of-the-art systems in the necessity for relatively long cantilevered rotor systems requiring involved bearing arrangements.




The embodiment in accordance with

FIG. 9

has two side inlets


56


,


56


′. These are separated from each other by at least one seal


1


. The seal


1


is so designed that it has a pumping action from outside to inside. The inlet


56


“sees” the inlet area of the axially pumping friction pump


51


as well as the periphery of the seal


1


pumping from outside to inside. The outlet of the radially pumping seal


1


opens into the inlet area of a second turbomolecular pumping stage


52


′ to which the second inlet


56


′ is connected. The seal


1


effects a lower pressure at inlet


56


compared to that at inlet


56


′. The drive motor


68


is located on the delivery side of the turbomolecular pumping stage


52


′. This delivery side is linked via the bypass


67


to the suction side of the molecular pumping stage


53


.




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.



Claims
  • 1. A seal between a rotating part and a stationary part in which at least one of the parts is provided with projections which protrude into a radially extending seal gap so that both parts are provided with engaging projections which extend in an axial direction, which projections are located concentrically in relation to an axis of rotation of the rotating part and are designed as rows of blades.
  • 2. The seal according to claim 1, wherein the rows of blades provide a pumping action.
  • 3. The seal according to claim 2, wherein the seal is of the double flow type.
  • 4. The seal according to claim 3, wherein the properties of the rows of blades of the double flow seal are selected in such a manner that a direction of the pumping action of the outer rows of blades is opposed to a direction of the pumping action of the inner rows of blades.
  • 5. The seal according to claim 4, wherein an inert gas inlet is defined between the inner and outer rows of blades forming the double flow seal.
  • 6. The seal according to claim 1, wherein the seal is part of a blower or a pump and is located between a pump chamber and a motor chamber.
  • 7. The seal according to claim 6, wherein the seal has a pumping action directed towards the pump chamber.
  • 8. The seal according to claim 6, wherein the seal is part of a turbomolecular pump, said seal having a pumping action directed towards the motor chamber, the motor chamber being linked through a bypass to a forevacuum pumping stage.
  • 9. The seal according to claim 8, wherein the motor chamber is located at a suction side of the turbomolecular vacuum pump.
  • 10. The seal according to claim 1, wherein the seal is part of a turbomolecular vacuum pump having at least two inlets, said seal being located between the inlets.
  • 11. The seal according to claim 10, wherein the seal has a pumping action, a periphery of the seal being linked with a first inlet area and its center with a second inlet area.
  • 12. A seal assembly comprising:first and second parts which define a gap therebetween, the first and second parts being rotatable relative to each other about an axis of rotation; a first ring of blades projecting from the first part into the seal gap in a direction parallel to the axis of rotation; a second ring of blades projecting into the seal gap in a direction parallel to the axis of rotation, the first and second rings of blades being disposed contiguous to each other; at least one of the rows of blades being skewed relative to a circumferential direction such that the skewed blades provide a pumping action within the seal gap.
Priority Claims (1)
Number Date Country Kind
100 04 263 Feb 2000 DE
PCT Information
Filing Document Filing Date Country Kind
PCT/EP00/12469 WO 00
Publishing Document Publishing Date Country Kind
WO01/57403 8/9/2001 WO A
US Referenced Citations (16)
Number Name Date Kind
1715597 Haug Jun 1929 A
2127865 Goddard Aug 1938 A
3109658 Barrett et al. Nov 1963 A
3399827 Schwartzman Sep 1968 A
3466052 Ludwig Sep 1969 A
3957277 Margnelli May 1976 A
4199154 Mueller Apr 1980 A
4460180 Koistinen Jul 1984 A
4512725 Saulgeot Apr 1985 A
4655681 Mori et al. Apr 1987 A
4734018 Taniyama et al. Mar 1988 A
5165872 Fleischmann et al. Nov 1992 A
5222742 Roberts Jun 1993 A
5499902 Rockwood Mar 1996 A
6152452 Wang Nov 2000 A
6419461 Okada Jul 2002 B2
Foreign Referenced Citations (6)
Number Date Country
32 21 380 Jul 1923 DE
491 159 Feb 1930 DE
23 221 May 1952 DE
24 40 141 Apr 1975 DE
0 408 791 Jan 1991 EP
2602834 Feb 1988 FR
Non-Patent Literature Citations (1)
Entry
Wood, et al., “Performance of Centrifugal Shaft Seals For High-Temperature, High-Pressure Liquids”, Machine Design, Jan. 30, 1964, p. 129-136.