WO2004001257A1 - Dichtungsanordnung zum abdichten eines spaltes zwischen zwei relativ zueinander um eine gemeinsame drehachse drehbeweglichen bauteilen - Google Patents
Dichtungsanordnung zum abdichten eines spaltes zwischen zwei relativ zueinander um eine gemeinsame drehachse drehbeweglichen bauteilen Download PDFInfo
- Publication number
- WO2004001257A1 WO2004001257A1 PCT/DE2003/001973 DE0301973W WO2004001257A1 WO 2004001257 A1 WO2004001257 A1 WO 2004001257A1 DE 0301973 W DE0301973 W DE 0301973W WO 2004001257 A1 WO2004001257 A1 WO 2004001257A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- component
- sealing
- gap
- components
- brush seal
- Prior art date
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
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
- F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
- F16J15/3288—Filamentary structures, e.g. brush seals
Definitions
- Sealing arrangement for sealing a gap between two components which are rotatable relative to one another about a common axis of rotation
- the invention relates to a sealing arrangement for sealing a gap between two components which are rotatable relative to one another about a common axis of rotation according to the type specified in the preamble of claim 1.
- the use of brush seals for sealing two components that are rotatable relative to one another is well known.
- the brush seal essentially comprises a brush housing, which is mounted in the first component, and a plurality of bristles, which are introduced into the brush housing and whose free ends are aligned with a sealing surface of the second component.
- brush seals are used to seal an annular gap between the rotor and stator.
- Such a brush seal is disclosed for example in DE 100 18 273 A1.
- this object is achieved according to the invention in that the first component, in which the brush housing is mounted, is axially displaceable along the axis of rotation and is adjustable, and that the sealing surface of the second component, to which the bristles of the brush seal are aligned, is conical.
- the sealing arrangement according to the invention leads to significant advantages.
- the axial displacement of the first component allows the brush seal to be optimally adjusted during commissioning.
- a simplified assembly of the brush seal is ensured by the design of the seal arrangement according to the invention.
- the brush seal wears, it can be "adjusted".
- the readjustment is carried out by axially displacing the first component in the direction of the second component.
- the conical design of the sealing surface according to the invention results in a gap reduction between the two components, which increases the sealing function of the brush seal. This also means an optimization of the leakage, which among other things an extension of life means.
- the means for axially displacing and adjusting comprise an adjusting nut which is introduced into the housing and engages with a displacement thread cut into the first component, and a sliding seat formed between the housing and the first component.
- Fig. 1 is a sectional view of the sealing arrangement according to the invention, the one
- Fig. 2 shows the sealing arrangement of Fig. 1 after an adjustment process.
- a seal arrangement designated overall by reference number 10 in FIG. 1, for sealing a gap between two components which can be rotated relative to one another in a turbomachine (not shown further), e.g. Steam turbine or gas turbine comprises a first component 12, which is surrounded by a housing 14, and a second component 16.
- the two components 12, 16 have a common axis of rotation 18.
- the second component 16 is rotatably supported relative to the first component 12 about the axis of rotation 18.
- the rotational mobility of the second component 16 is indicated by the arrow 20.
- a brush seal 22 is introduced into the annular gap between the components 12, 16 in order, for example, to seal an area 24 with high pressure from an area 26 with lower pressure.
- the brush seal 22 comprises a brush housing 28 and a plurality of bristles 30 inserted in the brush housing 28. While the brush housing 28 is firmly in the first th component 12 is mounted, the free ends of the bristles 30 are aligned with a conical sealing surface 32 of the second component 16.
- a simple axial displacement and adjustment of the first component 12 in the housing 14 along the axis of rotation 18 is ensured via an adjustment nut 34 which is introduced into the housing 14 and engages with a displacement thread 36 cut into the first component 12.
- a sliding seat 38 is provided between the first component 12 and the housing 14.
- the gap between the two components 12, 16 is reduced in the event of an axial displacement 40 of the first component 12 in the direction of the second component 16.
- a gap reduction means that the sealing effect of the brush seal 22 is increased.
- FIG. 2 shows the sealing arrangement 10 from FIG. 1 after the sealing effect has been adjusted by axial displacement.
- the gap between the first component 12 and the second component 16 has been reduced.
- the brush seal 22 which has been introduced can remain installed for a longer period of time, that is to say has a longer service life, which in turn results in cost savings.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sealing Devices (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/518,483 US7523943B2 (en) | 2002-06-21 | 2003-06-13 | Sealing arrangement for sealing a gap between two components which can rotate in relation to each other about a common rotational axis |
JP2004514557A JP4391934B2 (ja) | 2002-06-21 | 2003-06-13 | 共通回転軸の周りで相対的に回転運動可能な2つの構成部材間の隙間を密封するための密封構造 |
EP03760561A EP1516137A1 (de) | 2002-06-21 | 2003-06-13 | Dichtungsanordnung zum abdichten eines spaltes zwischen zwei relativ zueinander um eine gemeinsame drehachse drehbeweglichen bauteilen |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10227630A DE10227630A1 (de) | 2002-06-21 | 2002-06-21 | Dichtungsanordnung zum Abdichten eines Spaltes zwischen zwei relativ zueinender um eine gemeinsame Drehachse drehbeweglichen Bauteilen |
DE10227630.7 | 2002-06-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2004001257A1 true WO2004001257A1 (de) | 2003-12-31 |
Family
ID=29723329
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE2003/001973 WO2004001257A1 (de) | 2002-06-21 | 2003-06-13 | Dichtungsanordnung zum abdichten eines spaltes zwischen zwei relativ zueinander um eine gemeinsame drehachse drehbeweglichen bauteilen |
Country Status (5)
Country | Link |
---|---|
US (1) | US7523943B2 (de) |
EP (1) | EP1516137A1 (de) |
JP (1) | JP4391934B2 (de) |
DE (1) | DE10227630A1 (de) |
WO (1) | WO2004001257A1 (de) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2944559B1 (de) * | 2014-05-13 | 2019-05-08 | ABB Oy | Schwenkdichtungsanordnung für eine Antriebseinheit |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0561565A1 (de) * | 1992-03-14 | 1993-09-22 | McCoy, Ronald Geoffrey | Wellenabdichtung |
EP1046841A2 (de) * | 1999-04-23 | 2000-10-25 | Carl Freudenberg | Wellenabdichtung für rotierende Wellen |
DE10018273A1 (de) | 2000-04-13 | 2001-10-25 | Mtu Aero Engines Gmbh | Bürstendichtung |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3345035A (en) * | 1965-04-30 | 1967-10-03 | Gen Motors Corp | Turbine wheel |
PL76196B1 (de) * | 1970-06-10 | 1975-02-28 | ||
GB2042646B (en) * | 1979-02-20 | 1982-09-22 | Rolls Royce | Rotor blade tip clearance control for gas turbine engine |
DE3507638C2 (de) | 1985-03-05 | 1987-04-30 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Bürstendichtung |
US4595207A (en) * | 1985-07-09 | 1986-06-17 | Mtu Motoren-Und Turbinen-Union Munchen Gmbh | Brush seal labyrinth sealing means between two machine parts |
US5029875A (en) | 1989-07-07 | 1991-07-09 | Textron Inc. | Fluid seal structure |
US5074748A (en) * | 1990-07-30 | 1991-12-24 | General Electric Company | Seal assembly for segmented turbine engine structures |
US5310319A (en) * | 1993-01-12 | 1994-05-10 | United Technologies Corporation | Free standing turbine disk sideplate assembly |
FR2742837B1 (fr) * | 1995-12-21 | 1998-02-20 | Eurocopter France | Dispositif d'etancheite pour arbre tournant |
US5961279A (en) * | 1996-05-31 | 1999-10-05 | Atlantic Richfield Company | Turbine power plant having minimal-contact brush seal augmented labyrinth seal |
DE19641375C1 (de) * | 1996-10-08 | 1997-12-04 | Mtu Muenchen Gmbh | Herstellungsverfahren für und Vorrichtung zum Herstellen von Bürstendichtungen |
US7226054B2 (en) * | 2004-12-14 | 2007-06-05 | United Technologies Corporation | Clamp lock brush seal assembly |
-
2002
- 2002-06-21 DE DE10227630A patent/DE10227630A1/de not_active Ceased
-
2003
- 2003-06-13 JP JP2004514557A patent/JP4391934B2/ja not_active Expired - Fee Related
- 2003-06-13 US US10/518,483 patent/US7523943B2/en not_active Expired - Fee Related
- 2003-06-13 EP EP03760561A patent/EP1516137A1/de not_active Withdrawn
- 2003-06-13 WO PCT/DE2003/001973 patent/WO2004001257A1/de active Application Filing
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0561565A1 (de) * | 1992-03-14 | 1993-09-22 | McCoy, Ronald Geoffrey | Wellenabdichtung |
EP1046841A2 (de) * | 1999-04-23 | 2000-10-25 | Carl Freudenberg | Wellenabdichtung für rotierende Wellen |
DE10018273A1 (de) | 2000-04-13 | 2001-10-25 | Mtu Aero Engines Gmbh | Bürstendichtung |
Also Published As
Publication number | Publication date |
---|---|
JP2005530117A (ja) | 2005-10-06 |
JP4391934B2 (ja) | 2009-12-24 |
DE10227630A1 (de) | 2004-01-15 |
US7523943B2 (en) | 2009-04-28 |
US20060131814A1 (en) | 2006-06-22 |
EP1516137A1 (de) | 2005-03-23 |
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