GB2128693A - Labyrinth seal - Google Patents

Labyrinth seal Download PDF

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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
Application number
GB08327207A
Other versions
GB8327207D0 (en
GB2128693B (en
Inventor
Luciano Bonciani
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nuovo Pignone SpA
Original Assignee
Nuovo Pignone SpA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Nuovo Pignone SpA filed Critical Nuovo Pignone SpA
Publication of GB8327207D0 publication Critical patent/GB8327207D0/en
Publication of GB2128693A publication Critical patent/GB2128693A/en
Application granted granted Critical
Publication of GB2128693B publication Critical patent/GB2128693B/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/44Free-space packings
    • F16J15/447Labyrinth packings
    • F16J15/4472Labyrinth packings with axial path

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)

**WARNING** start of CLMS field may overlap end of DESC **. 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). CLAIMS
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.
GB08327207A 1982-10-19 1983-10-11 Labyrinth seal Expired GB2128693B (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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
GB8327207D0 (en) 1983-11-09
JPS5989866A (en) 1984-05-24
CA1249616A (en) 1989-01-31
DE3337989C2 (en) 1985-12-05
DE3337989A1 (en) 1984-04-19
CH655770A5 (en) 1986-05-15
IT1152732B (en) 1987-01-07
IT8223811A0 (en) 1982-10-19
FR2534655A1 (en) 1984-04-20
GB2128693B (en) 1986-04-30
JPH0319424B2 (en) 1991-03-15

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PE20 Patent expired after termination of 20 years

Effective date: 20031010