GB2128693A - Labyrinth seal - Google Patents
Labyrinth seal Download PDFInfo
- Publication number
- GB2128693A GB2128693A GB08327207A GB8327207A GB2128693A GB 2128693 A GB2128693 A GB 2128693A GB 08327207 A GB08327207 A GB 08327207A GB 8327207 A GB8327207 A GB 8327207A GB 2128693 A GB2128693 A GB 2128693A
- Authority
- GB
- United Kingdom
- Prior art keywords
- seal
- circumferential
- cavity
- shaft
- labyrinth seal
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/447—Labyrinth packings
- F16J15/4472—Labyrinth packings with axial path
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Abstract
In order to reduce the destabilising effects resulting from a non-uniform pressure distribution in the circumferential seal cavities (3) of a labyrinth seal (2), each cavity (3) is divided circumferentially into compartments (4) by a series of radial impeding walls (5). The compartments (4) of each cavity (3) are all connected by radial ducts (6) to an outer circumferential manifold (7). <IMAGE>
Description
SPECIFICATION
Labyrinth seal
This invention relates to a labyrinth seal in which, by the maintenance of a uniform pressure distribution in each circumferential seal cavity of the seal, there is achieved a reduction in the destabilising effects which can compromise the proper operation of, for example, high-performance turbo machines.
A labyrinth seal for a rotary shaft is known to comprise a succession of circumferential teeth which face the shaft so as to define, between them and the shaft, circumferential cavities which trap the fluid in such a manner as to limittothe maximum extent the flow offluid between the upstream side and the downstream side ofthe seal. However, rotation ofthe shaft also causes rotation of the fluid located in each circumferential cavity of the labyrinth seal, thereby creating eccentricity between the rotating part and the seal, especially if the shaft becomes displaced for any reason.The circumferential motion ofthefluid in the cavity leads to a non-uniform circumferential distribution ofthe pressure in each labyrinth cavity, which tends to amplify the shaft displacement and give rise to gradually increasing shaft vibrations. The result is therefore a self-exciting destabilising effect which car.
influence the stability of the rotary shaft to a determining extent.
According to the present invention, there is provided a labyrinth seal for a rotary shaft, comprising a succession of circumferential teeth facing the shaft
and defining between them and the shaft, circumferential cavities arranged to trap fluid in such a mannerasto limittheflowoffluid between the
upstream side and the downstream side of the seal,
there being disposed in each of the circumferential cavities ofthe seal a plurality of radial impeding walls which circumferentially divide the cavity into compartments.
In accordance with the invention, there is present, in each circumferential cavity of the labyrinth seal, a plurality of radial impeding walls which circumferentially divide the cavity into compartments. By this means, the circumferential velocity ofthefluid in each compartment is on the average very low, and therefore in practice there can be an almost symmetrical circumferential distribution ofthe circumferential velocity ofthe fluid in each seal cavity, this resulting in an analogous pressure distribution.
In orderto ensure that the pressure distribution in each labyrinth cavity is effectively circumferentially symmetrical so that no destabilising effect occurs, whatever the position of the shaft relative to the seal, according to a preferred embodiment of the invention the individual compartments of each circumferential cavity ofthe labyrinth seal are connected by radial ducts to an outer circumferential manifold.
In this respect, by connecting together all the compartments of a labyrinth seal cavity and thus balancing the pressure in the compartments, the circumferential manifold eliminates any tendency for
a non-uniform pressure distribution to arise in the
individual seal cavities as a result of any shaft
displacement, and thus makes itimpossiblefor large-amplitude damaging vibrations to be induced in the shaft by the labyrinth seal.
For a better understanding of the invention, referpence will now be made, byway of example, to the drawings in which:
Figure lisa partly-sectional side view of a labyrinth seal for a rotary shaft, in accordance with the invention;
Figure 2 is a section through the seal along the line AAofFigure 1; and
Figure 3 is a section through the seal along the line BB of Figure 1.
The Figures show a rotary shaft 1 and a labyrinth seal 2, which seal comprises a succession of circumferential cavities 3i (i= 1 n) facing the shaft 1.
Each seal cavity 3i is divided circumferentially into a numberofcompartments4i(i=1 n) by . .. n) by radial impeding walls 5i (i=l ...... n), and all the compartments 4i of each cavity are connected by correspondingradialducts6i(i=l n) to a single outer circumferential manifold 7i (i= 1 n) (see specifically Figure 3).
1. A labyrinth seal for a rotary shaft, comprising a succession of circumferential teeth facing the shaft and defining between them and the shaft, circumferential cavities arranged to trap fluid in such a manner asto limitthe flow of fluid between the upstream side and the downstream side of the seal, there being disposed in each of the circumferential cavities of the seal a plurality of radial impeding walls which circumferentially divide the cavity into compartments.
2. A labyrinth seal as claimed in claim 1, wherein the individual compartments of each circumferential seal cavity are connected by radial ducts to an outer circumferential manifold.
3. A labyrinth seal substantially as herein before described with reference to, and as shown in, the drawings.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (3)
1. A labyrinth seal for a rotary shaft, comprising a succession of circumferential teeth facing the shaft and defining between them and the shaft, circumferential cavities arranged to trap fluid in such a manner asto limitthe flow of fluid between the upstream side and the downstream side of the seal, there being disposed in each of the circumferential cavities of the seal a plurality of radial impeding walls which circumferentially divide the cavity into compartments.
2. A labyrinth seal as claimed in claim 1, wherein the individual compartments of each circumferential seal cavity are connected by radial ducts to an outer circumferential manifold.
3. A labyrinth seal substantially as herein before described with reference to, and as shown in, the drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT23811/82A IT1152732B (en) | 1982-10-19 | 1982-10-19 | PERFECTED LABYRINTH SEAL |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8327207D0 GB8327207D0 (en) | 1983-11-09 |
GB2128693A true GB2128693A (en) | 1984-05-02 |
GB2128693B GB2128693B (en) | 1986-04-30 |
Family
ID=11210151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08327207A Expired GB2128693B (en) | 1982-10-19 | 1983-10-11 | Labyrinth seal |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS5989866A (en) |
CA (1) | CA1249616A (en) |
CH (1) | CH655770A5 (en) |
DE (1) | DE3337989C2 (en) |
FR (1) | FR2534655A1 (en) |
GB (1) | GB2128693B (en) |
IT (1) | IT1152732B (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5707064A (en) * | 1993-01-08 | 1998-01-13 | The Texas A&M University System | Modulated pressure damper seal |
US5794942A (en) * | 1993-01-08 | 1998-08-18 | The Texas A&M University System | Modulated pressure damper seals |
US6155574A (en) * | 1996-11-05 | 2000-12-05 | Alfa Laval Ab | Sealing device |
US7597538B2 (en) * | 2005-11-15 | 2009-10-06 | Snecma | Thermostructural turbomachine part that is circularly symmetrical about a longitudinal axis, the part including an annular wiper, and a method of manufacture |
US20100166544A1 (en) * | 2008-06-30 | 2010-07-01 | Hitachi, Ltd. | Turbomachinery |
WO2014038951A1 (en) * | 2012-09-06 | 2014-03-13 | Dynavec As | Labyrinth packing device for a hydraulic fluid flow machine |
US9074486B2 (en) | 2011-01-31 | 2015-07-07 | General Electric Company | Method and apparatus for labyrinth seal packing ring |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19933445C2 (en) * | 1999-07-16 | 2001-12-13 | Mtu Aero Engines Gmbh | Sealing ring for non-hermetic fluid seals |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB274049A (en) * | 1927-06-09 | 1928-05-03 | Fischer Karl | Improvements relating to stuffing box packing |
GB840573A (en) * | 1958-01-20 | 1960-07-06 | Rolls Royce | Labyrinth seals |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE494348C (en) * | 1930-03-21 | Karl Fischer Dipl Ing | Labyrinth stuffing box | |
DE884593C (en) * | 1940-05-12 | 1953-09-14 | Harry Kuhrmeier Dipl Ing | Sealing ring for high pressures |
US2886351A (en) * | 1956-01-03 | 1959-05-12 | Orenda Engines Ltd | Elements for labyrinth seals |
-
1982
- 1982-10-19 IT IT23811/82A patent/IT1152732B/en active
-
1983
- 1983-10-11 GB GB08327207A patent/GB2128693B/en not_active Expired
- 1983-10-18 FR FR8316578A patent/FR2534655A1/en active Pending
- 1983-10-18 JP JP58193577A patent/JPS5989866A/en active Granted
- 1983-10-18 CA CA000439209A patent/CA1249616A/en not_active Expired
- 1983-10-19 DE DE3337989A patent/DE3337989C2/en not_active Expired
- 1983-10-19 CH CH5692/83A patent/CH655770A5/en not_active IP Right Cessation
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB274049A (en) * | 1927-06-09 | 1928-05-03 | Fischer Karl | Improvements relating to stuffing box packing |
GB840573A (en) * | 1958-01-20 | 1960-07-06 | Rolls Royce | Labyrinth seals |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5707064A (en) * | 1993-01-08 | 1998-01-13 | The Texas A&M University System | Modulated pressure damper seal |
US5794942A (en) * | 1993-01-08 | 1998-08-18 | The Texas A&M University System | Modulated pressure damper seals |
US6155574A (en) * | 1996-11-05 | 2000-12-05 | Alfa Laval Ab | Sealing device |
US7597538B2 (en) * | 2005-11-15 | 2009-10-06 | Snecma | Thermostructural turbomachine part that is circularly symmetrical about a longitudinal axis, the part including an annular wiper, and a method of manufacture |
US20100166544A1 (en) * | 2008-06-30 | 2010-07-01 | Hitachi, Ltd. | Turbomachinery |
EP2141363A3 (en) * | 2008-06-30 | 2010-11-03 | Hitachi, Ltd. | Seal for turbomachine |
US8388311B2 (en) | 2008-06-30 | 2013-03-05 | Hitachi, Ltd. | Turbomachinery |
US9074486B2 (en) | 2011-01-31 | 2015-07-07 | General Electric Company | Method and apparatus for labyrinth seal packing ring |
WO2014038951A1 (en) * | 2012-09-06 | 2014-03-13 | Dynavec As | Labyrinth packing device for a hydraulic fluid flow machine |
Also Published As
Publication number | Publication date |
---|---|
IT8223811A0 (en) | 1982-10-19 |
FR2534655A1 (en) | 1984-04-20 |
GB8327207D0 (en) | 1983-11-09 |
CH655770A5 (en) | 1986-05-15 |
JPS5989866A (en) | 1984-05-24 |
GB2128693B (en) | 1986-04-30 |
DE3337989C2 (en) | 1985-12-05 |
JPH0319424B2 (en) | 1991-03-15 |
CA1249616A (en) | 1989-01-31 |
IT1152732B (en) | 1987-01-07 |
DE3337989A1 (en) | 1984-04-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PE20 | Patent expired after termination of 20 years |
Effective date: 20031010 |