Method and arrangement for sealing off a separating gap, formed between a rotor and a stator, in a non-contacting manner

• US 6,164,655 A
• Filed: 12/17/1998
• Issued: 12/26/2000
• Est. Priority Date: 12/23/1997
• Status: Expired due to Term

• Current Assignee: ABB Schweiz AG (ABB Limited)
• Original Assignee: Asea Brown Boveri AG (ABB Limited)
• Inventors: Bremer, Joachim, Loos, Markus, Wunderwald, Dirk, Muller, Ulf Christian, Greber, Jurg, Bothien, Mihajlo
• Primary Examiner(s): Knight, Anthony
• Assistant Examiner(s): Pickard, Alison K.
• Application Number:
  US09/213,429
• Time in Patent Office: 740 Days
• Field of Search: 277/303, 277/412, 277/418, 277/419, 277/424
• US Class Current: 277/303
• CPC Class Codes: F01D 11/02 by non-contact sealings, e.g. of labyrinth type for sealing space between rotor blade tips and stator F01D11/08
• CPC Class Codes: F16J 15/447 Labyrinth packings

Abstract

The object of the invention is to provide an improved method for sealing off the separating gap, formed between a rotor and a stator, in a non-contacting manner, with which method the service life of the components involved can be increased. In addition, an arrangement for carrying out the method is to be shown. According to the invention, this is achieved in that the flow layers (35, 36), having different circumferential velocities, of the working fluid (18) are divided after the choking action into a first partial flow (35'"'"') having a high circumferential velocity and a second partial flow (36'"'"') having a low circumferential velocity, the first partial flow (35'"'"') is merely deflected, only the second partial flow (36'"'"') is swirled and is finally directed parallel to the deflected first partial flow (35'"'"') into the latter. To this end, the opposing surface (24) of the choke point (22) is designed as a flow divider for the working fluid (18). The vortex chamber (23) adjoins the flow divider (24) and is arranged further upstream than the feed duct (29) for the next sealing element (21).

Claims

1. A method for sealing off a separating gap formed between a rotor and a stator in a non-contacting manner from the throughflow of a working fluid admitted to the separating gap, comprising the steps of:

forming in the working fluid, flow layers having different circumferential velocities;

choking the working fluid in the separating gap;

dividing the flow layers of the working fluid after the choking action into a first partial flow having a high circumferential velocity and a second partial flow having a low circumferential velocity;

deflecting the first partial flow;

swirling the second partial flow; and

directing the second partial flow parallel to the deflected first partial flow and into the first partial flow.

2. The method as claimed in claim 1, wherein each of the steps are repeated at least twice.

3. An arrangement sealing off a separating gap, formed between a rotor and a stator, in a non-contacting manner from the throughflow of a working fluid admitted to the separating gap in a main flow direction, in which arrangement at least one sealing element, consisting of a choke point, an opposing surface which is located on the stator and on which the working fluid impinges downstream of the choke point, and a vortex chamber, is arranged in the separating gap, and the separating gap is designed as a feed duct upstream of each sealing element and as a discharge duct downstream of the sealing element, wherein the opposing surface is designed as a flow divider for the working fluid, the vortex chamber is arranged in the opposite direction to the main flow direction, and the feed duct or the discharge duct are arranged so as to adjoin the flow divider in the main flow direction.

4. The arrangement as claimed in claim 3, wherein the flow divider consists of at least two sectional surfaces of the stator, which have a raised contact edge projecting into the separating gap.

5. The arrangement as claimed in claim 4, wherein the vortex chamber has a larger inner surface than the separating gap adjoining the vortex chamber.

6. The arrangement as claimed in claim 5, wherein the vortex chamber is formed at an angle α

of 45°

±

20°

to the main flow direction of the working fluid.

7. The arrangement as claimed in claim 3, wherein the feed duct and the discharge duct have a gap width, and the choke point has a clearance width, the gap width being designed to be larger than the clearance width of the choke point.

8. The arrangement as claimed in claim 3, wherein the sealing element is arranged in a fluid-flow machine having a machine axis, and the choke point is formed axially, radially or diagonally to the machine axis.

9. The arrangement as claimed in claim 8, wherein the rotor is designed as a compressor impeller of a radial compressor, the stator is designed as an intermediate wall of the radial compressor, which intermediate wall closes off the compressor impeller on the machine side, the sealing element is arranged between a rear wall of the compressor impeller and the intermediate wall, and the choke point is arranged parallel to the machine axis of the radial compressor.