DE19719770A1 - Turbine machine - Google Patents
Turbine machineInfo
- Publication number
- DE19719770A1 DE19719770A1 DE1997119770 DE19719770A DE19719770A1 DE 19719770 A1 DE19719770 A1 DE 19719770A1 DE 1997119770 DE1997119770 DE 1997119770 DE 19719770 A DE19719770 A DE 19719770A DE 19719770 A1 DE19719770 A1 DE 19719770A1
- Authority
- DE
- Germany
- Prior art keywords
- housing
- support structure
- annular support
- turbomachine
- turbo machine
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/70—Disassembly methods
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Hydraulic Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Die Erfindung betrifft eine Turbomaschine nach dem Oberbegriff des Patent anspruchs 1.The invention relates to a turbomachine according to the preamble of the patent claim 1.
Bei Turbomaschinen müssen regelmäßig im Zusammenhang mit Wartungsar beiten Baugruppen kontrolliert oder ausgebaut und ersetzt werden. Dazu ist es erforderlich, daß im allgemeinen das Oberteil, die obere Halbschale des Gehäuses der Turbomaschine abgenommen wird, um Zugang zu diesen Bau gruppen zu erhalten. Solche Teildemontagen sind sehr aufwendig und zeit raubend, daher teuer. Insbesondere um vielfach nur festzustellen, daß die über prüften Baugruppen weiterhin funktionstüchtig sind. Außerdem erfordert eine solche Teildemontage unverhältnismäßig viel Montagezeit gegenüber der eigentlichen Prüfzeit.For turbomachinery, they must be regularly related to maintenance be checked or removed and replaced. It is for that required that in general the upper part, the upper half-shell of the Housing of the turbomachine is removed to give access to this construction groups. Such partial disassembly is very complex and time consuming, therefore expensive. In particular, in order to determine that the over tested modules are still functional. It also requires one such partial disassembly disproportionate time compared to the actual test time.
Die Erfindung versucht, diese Nachteile zu vermeiden. Es liegt ihr die Aufgabe zugrunde, eine Turbomaschine anzugeben, bei welcher zur Überprüfung oder zum Austausch von Baugruppen Teildemontagen im bisherigen Umfang nicht erforderlich sind. The invention tries to avoid these disadvantages. It is her job based on specifying a turbomachine for which to check or not for the replacement of assemblies required are.
Die Lösung dieser Aufgabe wird mit den Merkmalen des Kennzeichens von Patentanspruch 1 umschrieben. Vorteilhafte Ausführungsformen einer Tur bomaschine sind durch die Merkmale der abhängigen Ansprüche angegeben.The solution to this problem is with the characteristics of the indicator of Claim 1 circumscribed. Advantageous embodiments of a door bomaschine are indicated by the features of the dependent claims.
Weitere Merkmale und Vorteile ergeben sich aus der Beschreibung einer beispielsweisen Ausführungsform anhand der Zeichnung. In dieser zeigt:Further features and advantages result from the description of a exemplary embodiment with reference to the drawing. In this shows:
Fig. 1 schematisch einen Teil des Gehäuses einer Turbomaschine, teilweise aufgeschnitten, Fig. 1 shows diagrammatically, partially cut away part of the casing of a turbomachine,
Fig. 2 schematisch einen teilweisen Schnitt (AA) durch die Turbomaschine senkrecht zu ihrer Achse. Fig. 2 shows schematically a partial section (AA) through the turbo machine perpendicular to its axis.
Es sind nur die für das Verständnis der Erfindung wesentlichen Elemente gezeigt; insbesondere ist nicht der an sich bekannte und unveränderte Teil der Turbomaschine oder andere ihrer Details etc. dargestellt.They are only the elements essential for understanding the invention shown; in particular, the part of the Turbomachine or other of its details etc. shown.
Bei einer Turbomaschine 1 mit einem Gehäuse 2, in welchem ein Rotor 4 gelagert ist und das die Peripheriebaugruppen, wie Brennkammern, Kühlsys teme, etc. enthält, ist eine ringförmige Tragstruktur 3 im Gehäuse 2 vorgesehen. Diese ringförmige Tragstruktur 3 ist im Gehäuse drehbar gelagert und in wenig stens einer Position verriegelbar. Auf ihr sind alle periodisch zu überprüfenden oder auszuwechselnden Baugruppen 5 montiert. Um die ringförmige Tragstruktur 3 bei Bedarf anläßlich einer Revision der Turbomaschine 1 in verschiedene Montage oder Revisionspositionen drehen zu können, ist sie mit einer Einrich tung verbunden, welche einerseits die ringförmige Tragstruktur 3 in der Betriebs stellung verriegelt und andererseits sie in die erforderlichen Montage oder Revisionspositionen bewegt. Diese Einrichtung zum Drehen der ringförmigen Tragstruktur 3 ist zwischen dem Gehäuse 2 und der ringförmigen Tragstruktur 3 oder zwischen dieser und dem Rotor 4 angeordnet. Das Gehäuse 2 der Turbo maschine 1 weist wenigstens eine verschließbare Montageöffnung 6 auf, welche eine solche Größe und Form hat, daß die zu kontrollierenden oder zu ersetzenden Baugruppen 5 der Turbomaschine 1 leicht zugänglich sind bzw. ausgebaut und entfernt werden können. Insbesondere sind bei mehreren Montageöffnungen 6 diese im wesentlichen in zwei achsnormalen Ebenen angeordnet, welche den im Innern des Gehäuses 2 vorhandenen Baugruppen 5 entsprechen. Damit ist gewährleistet, daß die Baugruppen 5 der Turbomaschine zugänglich sind, wodurch sich die Stillstandszeit wesentlich verringert. Zudem muß bei einer solcherweise ausgebildeten Turbomaschine nicht mehr das Gehäuse teilweise demontiert werden, um zu den zu ersetzenden oder zu kontrollierenden Baugruppen 5 Zugang zu erhalten. Dies bewirkt wesentliche Einsparungen bei der Revision.In a turbomachine 1 with a housing 2 , in which a rotor 4 is mounted and which contains the peripheral assemblies, such as combustion chambers, cooling systems, etc., an annular support structure 3 is provided in the housing 2 . This annular support structure 3 is rotatably mounted in the housing and can be locked in at least one position. All modules 5 to be checked or replaced periodically are mounted on it. In order to be able to rotate the ring-shaped support structure 3 when required during a revision of the turbomachine 1 into different assembly or revision positions, it is connected to a device which, on the one hand, locks the ring-shaped support structure 3 in the operating position and, on the other hand, it into the required assembly or revision positions emotional. This device for rotating the annular support structure 3 is arranged between the housing 2 and the annular support structure 3 or between the latter and the rotor 4 . The housing 2 of the turbo machine 1 has at least one lockable mounting opening 6 , which has such a size and shape that the assemblies 5 to be checked or replaced of the turbomachine 1 are easily accessible or can be removed and removed. In particular, in the case of a plurality of assembly openings 6, these are arranged essentially in two axially normal planes, which correspond to the assemblies 5 present in the interior of the housing 2 . This ensures that the assemblies 5 of the turbomachine are accessible, which significantly reduces the downtime. In addition, in the case of a turbomachine designed in this way, the housing no longer has to be partially dismantled in order to gain access to the assemblies 5 to be replaced or checked. This leads to significant savings in the revision.
11
Turbomaschine
Turbo machine
22nd
Gehäuse
casing
33rd
ringförmige Tragstruktur
annular support structure
44th
Rotor
rotor
55
Baugruppen (für Revision)
Assemblies (for revision)
66
Montageöffnung
Assembly opening
Claims (5)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1997119770 DE19719770A1 (en) | 1997-05-10 | 1997-05-10 | Turbine machine |
GB9808224A GB2328477A (en) | 1997-05-10 | 1998-04-17 | Access to subassemblies of a turbomachine |
CN 98107968 CN1199132A (en) | 1997-05-10 | 1998-05-08 | Turbomachine |
JP12590898A JPH10317913A (en) | 1997-05-10 | 1998-05-08 | Turbine machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1997119770 DE19719770A1 (en) | 1997-05-10 | 1997-05-10 | Turbine machine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE19719770A1 true DE19719770A1 (en) | 1998-11-12 |
Family
ID=7829186
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1997119770 Withdrawn DE19719770A1 (en) | 1997-05-10 | 1997-05-10 | Turbine machine |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPH10317913A (en) |
CN (1) | CN1199132A (en) |
DE (1) | DE19719770A1 (en) |
GB (1) | GB2328477A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009045391A1 (en) | 2009-10-06 | 2011-04-07 | Robert Bosch Gmbh | Micromechanical structure and method for producing a micromechanical structure |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012202466B3 (en) * | 2012-02-17 | 2013-07-11 | Siemens Aktiengesellschaft | Assembly of a turbomachine |
US10502057B2 (en) * | 2015-05-20 | 2019-12-10 | General Electric Company | System and method for blade access in turbomachinery |
US20190234310A1 (en) * | 2018-01-29 | 2019-08-01 | Pratt & Whitney Canada Corp. | Segmented internal fuel manifold |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3214101C2 (en) * | 1981-04-17 | 1984-01-26 | Nuovo Pignone S.p.A., Firenze | Gas turbine plant |
DD253851A1 (en) * | 1986-11-20 | 1988-02-03 | Orgreb Inst Kraftwerke | ARRANGEMENT FOR CONTROLLING TURBINES, ESPECIALLY STEAM TURBINES |
GB2244047A (en) * | 1990-05-17 | 1991-11-20 | Rolls Royce Plc | Inspection aperture plug assembly |
US5473883A (en) * | 1993-11-03 | 1995-12-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Compressor turbojet engine whose rotor has a movable upstream stage |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3493212A (en) * | 1968-06-24 | 1970-02-03 | Westinghouse Electric Corp | Rotary machine apparatus |
GB1265717A (en) * | 1969-06-10 | 1972-03-08 | ||
US4222708A (en) * | 1978-06-26 | 1980-09-16 | General Electric Company | Method and apparatus for reducing eccentricity in a turbomachine |
US4856968A (en) * | 1988-02-02 | 1989-08-15 | Armbruster Joseph M | Air circulation device |
US4925363A (en) * | 1989-02-13 | 1990-05-15 | Westinghouse Electric Corp. | Blade ring rollout roller |
US5233822A (en) * | 1991-01-31 | 1993-08-10 | General Electric Company | Method and system for the disassembly of an annular combustor |
US5249417A (en) * | 1991-09-25 | 1993-10-05 | United Technologies Corporation | Method and apparatus to install and remove heavy components |
-
1997
- 1997-05-10 DE DE1997119770 patent/DE19719770A1/en not_active Withdrawn
-
1998
- 1998-04-17 GB GB9808224A patent/GB2328477A/en not_active Withdrawn
- 1998-05-08 JP JP12590898A patent/JPH10317913A/en active Pending
- 1998-05-08 CN CN 98107968 patent/CN1199132A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3214101C2 (en) * | 1981-04-17 | 1984-01-26 | Nuovo Pignone S.p.A., Firenze | Gas turbine plant |
DD253851A1 (en) * | 1986-11-20 | 1988-02-03 | Orgreb Inst Kraftwerke | ARRANGEMENT FOR CONTROLLING TURBINES, ESPECIALLY STEAM TURBINES |
GB2244047A (en) * | 1990-05-17 | 1991-11-20 | Rolls Royce Plc | Inspection aperture plug assembly |
US5473883A (en) * | 1993-11-03 | 1995-12-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Compressor turbojet engine whose rotor has a movable upstream stage |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009045391A1 (en) | 2009-10-06 | 2011-04-07 | Robert Bosch Gmbh | Micromechanical structure and method for producing a micromechanical structure |
US8443671B2 (en) | 2009-10-06 | 2013-05-21 | Robert Bosch Gmbh | Micromechanical structure and method for manufacturing a micromechanical structure |
Also Published As
Publication number | Publication date |
---|---|
CN1199132A (en) | 1998-11-18 |
GB9808224D0 (en) | 1998-06-17 |
GB2328477A (en) | 1999-02-24 |
JPH10317913A (en) | 1998-12-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE3538599A1 (en) | SHOVEL MOUNTING DEVICE | |
DE2627702A1 (en) | AXIAL FLOW MACHINE | |
DE102010053141B4 (en) | Turbine aggregate with possible over-rotation of the foot of a blade to the installation of a last blade | |
DE4110244A1 (en) | INTERMEDIATE SEALING ARRANGEMENT FOR BLADE LEVELS OF CONTINUOUS TURBINE ENGINE ROTORS | |
DE102014118021A1 (en) | Turbomachinery Kaltspaltjustage | |
DE19913658A1 (en) | Mixer | |
DE2119113A1 (en) | Self-adjusting sealing arrangement | |
DE2925415A1 (en) | METHOD AND DEVICE FOR REDUCING ECCENTRICITY IN A TURBO MACHINE | |
DE2255853B1 (en) | Device for the guide vane adjustment | |
DE202014106044U1 (en) | Thin fan with axial air opening | |
EP0745756B1 (en) | Fixture and method for the assembly of runner blades | |
DE102020108248B3 (en) | Device for assembling and disassembling a bearing segment of a bearing arrangement for a rotor of a wind turbine | |
DE19719770A1 (en) | Turbine machine | |
EP3775534A1 (en) | Rotor hub of a wind turbine, and method for assembling such a rotor hub | |
EP3390784B1 (en) | Continuous flow machine having multiple guide vane stages and method for partially disassembling a continuous flow machine of this type | |
DE102017119633B4 (en) | power generator | |
EP1022439A1 (en) | Steam or gas turbine casing | |
CH619507A5 (en) | ||
DE102013013571B4 (en) | Exhaust gas turbocharger | |
DE102018120806A1 (en) | Bearing arrangement of a rotor of a wind turbine | |
DE539109C (en) | Device for converting ventilated electrical machines with an outer housing divided in the axial direction from an open, ventilated machine to a closed, jacket-cooled machine | |
DE102017113627A1 (en) | Stator for a resolver, resolver and its use | |
DE60215327T2 (en) | TURBINE OR COMPRESSOR DEVICE AND METHOD FOR ASSEMBLING THE DEVICE | |
DE102006012363A1 (en) | Rotary flow machine e.g. turbine, for power station plant, has inner housing supported at two diametrically opposite lying sides at outer housing along zero level, where longitudinal center line of inner housing extends in zero level | |
EP0942514B1 (en) | Electric motor with annular flange |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
OM8 | Search report available as to paragraph 43 lit. 1 sentence 1 patent law | ||
8127 | New person/name/address of the applicant |
Owner name: ABB ALSTOM POWER (SCHWEIZ) AG, BADEN, AARGAU, CH |
|
8139 | Disposal/non-payment of the annual fee |