WO2001070451A1 - Verfahren zum entfernen eines dichtmittels - Google Patents
Verfahren zum entfernen eines dichtmittels Download PDFInfo
- Publication number
- WO2001070451A1 WO2001070451A1 PCT/EP2001/002579 EP0102579W WO0170451A1 WO 2001070451 A1 WO2001070451 A1 WO 2001070451A1 EP 0102579 W EP0102579 W EP 0102579W WO 0170451 A1 WO0170451 A1 WO 0170451A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- groove
- clamping means
- housing
- liquid
- sealant
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
- B23P19/047—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts for flexible profiles, e.g. sealing or decorating strips in grooves or on other profiles by devices moving along the flexible profile
-
- 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
- F16J15/3268—Mounting of sealing rings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
- Y10T29/49719—Seal or element thereof
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49718—Repairing
- Y10T29/49721—Repairing with disassembling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49815—Disassembling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49815—Disassembling
- Y10T29/49822—Disassembling by applying force
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/53—Means to assemble or disassemble
- Y10T29/53657—Means to assemble or disassemble to apply or remove a resilient article [e.g., tube, sleeve, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/53—Means to assemble or disassemble
- Y10T29/53796—Puller or pusher means, contained force multiplying operator
- Y10T29/5383—Puller or pusher means, contained force multiplying operator having fluid operator
Definitions
- Such a sealant is, for example, a sealing tape which is fastened to a housing or to a rotor of a turbine machine, around the gap between the shaft of the rotor and a guide vane fastened to the housing or between the housing and a rotor blade against a flowing through
- a sealing tape is alternately arranged on the housing or the guide vane and a sealing tape on the shaft or the rotor blade, one speaks of a so-called labyrinth seal.
- the action medium hardly penetrates through this labyrinth of seals, so that the performance of the turbomachine is only slightly reduced due to this loss of action medium.
- the following refers to the housing of the turbomachine when the housing is referred to as such or from a guide vane fixedly connected to the housing, and from the rotor when the rotor as such or from a fixed to the rotor connected Laufschaufei is the speech.
- the sealing tape protruding into the gap between the housing and the rotor is generally L-shaped on its fastening side.
- the L-shaped fastening side of the sealing tape is inserted into a groove on the housing or on the rotor.
- a clamping device is then inserted into the groove.
- clamping means also flaring ge ⁇ Nannt, a calking wire is inscribed in the groove.
- the sealing tape holds firmly in the groove due to the high frictional forces developed by the caulking wire.
- caulking wire is usually also used for a metallic caulking element.
- sealing tapes in turbomachinery usually show such wear after a few 10,000 hours that they can no longer fulfill their sealing function.
- the sealing tapes must be replaced from time to time.
- the object of the invention is to provide a method for removing a sealant, which is held in a groove of a component, which takes less time compared to methods of the prior art and is therefore less expensive.
- This object is achieved according to the invention by a method for removing a sealant which is held in a groove of a component with a clamping means, a liquid jet being directed under high pressure into the groove between the sealant and the clamping means or between the clamping means and the component , whereby at least the clamping means is released from the groove.
- turbomachinery Although there has previously been talk of rotationally symmetrical components of turbomachinery, it should in principle be noted that the invention is suitable in principle for removing any sealant held with a clamping means in a groove in a simple manner. Whether the component is part of a compressor, a gas turbine, a steam turbine, a pump, a generator or another device is irrelevant for the application of the invention.
- a sealing tape is removed from a groove in a component, for example a rotor or a housing of a turbomachine, in particular a steam or gas turbine.
- a sealing tape is held in a groove of the component by means of a clamping means.
- the liquid jet is directed to remove such a sealant between the sealant and the component, whereby the sealant is released from the groove.
- the liquid jet can be directed between the sealant and the clamping means, whereby at least the clamping means is released from the groove and the sealant is then easily removed from the groove, for example manually.
- the liquid jet is advantageously guided along the groove. As a result, the sealant or the clamping means is continuously released from the groove.
- both the wire and the material from which the groove is made can be made of high-alloy or high-temperature steel.
- the material of the groove can also be cast steel, for example gray cast iron, while the wire is made of a steel that is still alloyed.
- the process can also be used with advantage in cases in which the material of the clamping means is mechanically more resistant than the mate
- a metallic caulking element for holding the sealant designed as a sealant is removed from the groove of a rotor or a housing of a turbomachine, in particular a turbo compressor, a steam turbine or a gas turbine, as the clamping means.
- the liquid jet is advantageously expelled at a pressure between 750 and 4000 bar.
- the choice of pressure depends on the material of the clamping means, the sealant and the material of the component.
- a metallic clamping means in the form of a metallic caulking wire for holding a sealing tape in a turbomachine it has proven to be advantageous if the liquid jet is expelled at a pressure between 2000 and 3000 bar.
- the clamping means is easily removed from the groove without causing mechanical damage to the component.
- water is used as the liquid. When using water, no complex measures are required to meet environmental requirements.
- a liquid jet is expediently used, the width of which at the point of impact in the groove is 0.5 to 1.5 times as large as the width of the groove.
- the success in releasing a clamping means which is very firmly m-aligned in the groove largely depends on the pressure which the liquid jet develops under the clamping means in the groove. This pressure is dependent on the amount of liquid that is introduced under time as an agent and the speed at which the liquid hits the groove. The more liquid m is introduced into the groove per time, the greater the pressure developed under the clamping means. If a narrow flow jet is used, the pressure which may be necessary can only be achieved by a very high speed of the liquid. However, this allows the groove to be washed out, ie to change its shape, which is not desired.
- the sealant and / or the clamping means is kept taut during the removal from the groove.
- the element under which the liquid jet is directed is expediently kept taut. Without such a tight hold, the respective element would flutter in the liquid jet or be bent away from the liquid and possibly break off. However, breaking off the element to be removed has a negative effect, since the liquid below the one in the Groove that holds the groove can develop less pressure than under an element intact in the area of the beam.
- FIG. 1 shows a part of a housing of a steam turbine in a personal representation, a series of sealing tapes being inserted into the housing;
- FIG. 3 shows a schematic illustration of the removal of the sealing tape shown in FIG. 1 by means of a directed liquid jet.
- FIG. 1 shows a perspective view of part of a housing 2 made of gray cast iron of a steam turbine.
- the part shown is half of a hollow cylinder, inside which the rotor of the steam turbine, not shown, rotates.
- a series of sealing tapes 3 are inserted one behind the other on the housing 2 and each protrude into the gap. To simplify the illustration, only three of these sealing tapes 3 are shown. Sealing tapes, which are arranged on the rotor, each engage between two adjacent sealing tapes 3 of the housing 2. It is a so-called labyrinth seal of the gap between the rotor and the housing 2.
- Each sealing tape 3 is fastened to the housing 2 in a groove 6 m by means of a metallic clamping means 4.
- the clamping means is a caulking wire made of an alloyed steel.
- the sealing tape 3 is L-shaped on its fastening side. The fastening side of the sealing tape 3 is inserted into the groove 6 of the housing 2 and then mechanically firmly pressed or caulked into the groove 6 with the gill means 4. This creates a permanent and mechanically stable connection between the sealing tape 3 and the housing 2. The same naturally also applies to the runner.
- Figure 3 now shows how the sealing tape 3 is removed from the groove 6 of the housing, e.g. if it can no longer guarantee its sealing function due to mechanical wear.
- a high-pressure unit not shown in detail, liquid is brought to a pressure of between 2000 bar and 3000 bar. Water is used as the liquid.
- a liquid jet 9 is directed under high pressure between the clamping means 4 and the sealing tape 3.
- the clamping means 4 in the groove 6 detaches from the sealing tape 3 and is pressed out of the groove 6 due to the high pressure of the liquid.
- the process is started at the point shown.
- the liquid jet 9 is then guided along the groove 6 by means of the nozzle 1, as a result of which the clamping means 4 is gradually released from the groove 6.
- the clamping means 4 is kept continuously taut by a suitable device.
- the nozzle 8 can continuously follow the rounding of the groove 6 and in this respect always direct the liquid jet 9 between the sealing tape 3 and the clamping means 4.
- the width of the liquid jet at the point of impact in the groove is approximately 1 mm, the groove 6 having a width of 1.5 mm and the clamping means 4 having a width of 1.25 mm.
- the liquid jet 9 is thus 0.67 times as wide as the groove 6 and 0.8 times as wide as the clamping means 4.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Sealing Devices (AREA)
- Automatic Assembly (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP01933667A EP1265726B1 (de) | 2000-03-22 | 2001-03-07 | Verfahren zum entfernen eines dichtmittels |
US10/239,295 US6779239B2 (en) | 2000-03-22 | 2001-03-07 | Method for removing a seal |
DE50113413T DE50113413D1 (de) | 2000-03-22 | 2001-03-07 | Verfahren zum entfernen eines dichtmittels |
JP2001568692A JP2003527973A (ja) | 2000-03-22 | 2001-03-07 | シール手段の除去方法 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP00106226 | 2000-03-22 | ||
EP00106226.4 | 2000-03-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2001070451A1 true WO2001070451A1 (de) | 2001-09-27 |
Family
ID=8168196
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2001/002579 WO2001070451A1 (de) | 2000-03-22 | 2001-03-07 | Verfahren zum entfernen eines dichtmittels |
Country Status (11)
Country | Link |
---|---|
US (1) | US6779239B2 (de) |
EP (1) | EP1265726B1 (de) |
JP (1) | JP2003527973A (de) |
CN (1) | CN1172772C (de) |
AR (1) | AR027683A1 (de) |
AT (1) | ATE381977T1 (de) |
DE (1) | DE50113413D1 (de) |
ES (1) | ES2295164T3 (de) |
RU (1) | RU2246651C2 (de) |
TW (1) | TW504435B (de) |
WO (1) | WO2001070451A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2169184A2 (de) * | 2008-09-24 | 2010-03-31 | General Electric Company | Vorrichtung und Verfahren zur Entfernung von Gasturbinenkompressor-Leitschaufelsegmenten mit dem Rotor vor Ort |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7827665B2 (en) * | 2004-07-08 | 2010-11-09 | Press-Seal Gasket Corporation | Gasket and mandrel assembly for pipe joints |
US20060228209A1 (en) * | 2005-04-12 | 2006-10-12 | General Electric Company | Abradable seal between a turbine rotor and a stationary component |
US7996971B2 (en) * | 2007-09-26 | 2011-08-16 | The Boeing Company | Seal removal apparatus |
DE102008005606B3 (de) * | 2008-01-22 | 2010-04-15 | Khs Ag | Vorrichtung zur Abdichtung von Vertikalfugen zwischen plattenförmigen Wandelementen |
WO2013060663A2 (de) * | 2011-10-24 | 2013-05-02 | Alstom Technology Ltd | Gasturbine |
US9429041B2 (en) | 2014-05-14 | 2016-08-30 | General Electric Company | Turbomachine component displacement apparatus and method of use |
WO2016084663A1 (ja) * | 2014-11-25 | 2016-06-02 | イーグル工業株式会社 | 容量制御弁 |
US10786927B2 (en) | 2017-02-20 | 2020-09-29 | Press-Seal Corporation | Hole former with gasket locating features for cast manhole structures |
US11285571B1 (en) * | 2021-01-25 | 2022-03-29 | Delavan Inc. | Fuel nozzle seal removal tool |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2197580A (en) * | 1986-11-21 | 1988-05-25 | Jet Stream Systems Limited | Band removal |
EP0430856A1 (de) * | 1989-11-27 | 1991-06-05 | United Technologies Corporation | Ablösung von plasmagespritzten oder gesinterten Beschichtungen mittels eines Wasserstrahls |
EP0753376A1 (de) * | 1995-07-10 | 1997-01-15 | United Technologies Corporation | Reparaturverfahren für eine abschleifbare Dichtung |
US5738730A (en) * | 1995-07-12 | 1998-04-14 | Honda Giken Kogyo Kabushiki Kaisha | Process for peeling off temporarily protecting coating film |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3915739A (en) * | 1974-07-12 | 1975-10-28 | Montreal | Method of cleaning foreign matter from a cavity in a semiconductor |
US3969813A (en) * | 1975-08-15 | 1976-07-20 | Bell Telephone Laboratories, Incorporated | Method and apparatus for removal of semiconductor chips from hybrid circuits |
US4081892A (en) * | 1976-11-01 | 1978-04-04 | Flow Industries, Inc. | Method of making composite structure |
US5078161A (en) * | 1989-05-31 | 1992-01-07 | Flow International Corporation | Airport runway cleaning method |
US5499639A (en) * | 1995-05-01 | 1996-03-19 | Williams, Jr.; Robert V. | Apparatus and method for cleaning exchanger tubes |
PL196800B1 (pl) * | 1997-10-20 | 2008-01-31 | Florianer Bahn Forschungs & Errichtungsgesellschaft Mbh | Sposób i urządzenie do oczyszczania rowków szyn, zwłaszcza kolejowych i tramwajowych |
-
2001
- 2001-03-07 EP EP01933667A patent/EP1265726B1/de not_active Expired - Lifetime
- 2001-03-07 RU RU2002128140/06A patent/RU2246651C2/ru active
- 2001-03-07 ES ES01933667T patent/ES2295164T3/es not_active Expired - Lifetime
- 2001-03-07 CN CNB018067875A patent/CN1172772C/zh not_active Expired - Fee Related
- 2001-03-07 US US10/239,295 patent/US6779239B2/en not_active Expired - Fee Related
- 2001-03-07 JP JP2001568692A patent/JP2003527973A/ja not_active Abandoned
- 2001-03-07 DE DE50113413T patent/DE50113413D1/de not_active Expired - Fee Related
- 2001-03-07 WO PCT/EP2001/002579 patent/WO2001070451A1/de active IP Right Grant
- 2001-03-07 AT AT01933667T patent/ATE381977T1/de not_active IP Right Cessation
- 2001-03-20 AR ARP010101282A patent/AR027683A1/es active IP Right Grant
- 2001-03-29 TW TW090107496A patent/TW504435B/zh active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2197580A (en) * | 1986-11-21 | 1988-05-25 | Jet Stream Systems Limited | Band removal |
EP0430856A1 (de) * | 1989-11-27 | 1991-06-05 | United Technologies Corporation | Ablösung von plasmagespritzten oder gesinterten Beschichtungen mittels eines Wasserstrahls |
EP0753376A1 (de) * | 1995-07-10 | 1997-01-15 | United Technologies Corporation | Reparaturverfahren für eine abschleifbare Dichtung |
US5738730A (en) * | 1995-07-12 | 1998-04-14 | Honda Giken Kogyo Kabushiki Kaisha | Process for peeling off temporarily protecting coating film |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2169184A2 (de) * | 2008-09-24 | 2010-03-31 | General Electric Company | Vorrichtung und Verfahren zur Entfernung von Gasturbinenkompressor-Leitschaufelsegmenten mit dem Rotor vor Ort |
EP2169184A3 (de) * | 2008-09-24 | 2013-04-24 | General Electric Company | Vorrichtung und Verfahren zur Entfernung von Gasturbinenkompressor-Leitschaufelsegmenten mit dem Rotor vor Ort |
Also Published As
Publication number | Publication date |
---|---|
EP1265726A1 (de) | 2002-12-18 |
DE50113413D1 (de) | 2008-02-07 |
TW504435B (en) | 2002-10-01 |
CN1418142A (zh) | 2003-05-14 |
AR027683A1 (es) | 2003-04-09 |
EP1265726B1 (de) | 2007-12-26 |
CN1172772C (zh) | 2004-10-27 |
ES2295164T3 (es) | 2008-04-16 |
RU2246651C2 (ru) | 2005-02-20 |
US6779239B2 (en) | 2004-08-24 |
US20030101561A1 (en) | 2003-06-05 |
JP2003527973A (ja) | 2003-09-24 |
ATE381977T1 (de) | 2008-01-15 |
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