DE69402730D1 - Sicherungsmethode für einen Turbinenfutter - Google Patents
Sicherungsmethode für einen TurbinenfutterInfo
- Publication number
- DE69402730D1 DE69402730D1 DE69402730T DE69402730T DE69402730D1 DE 69402730 D1 DE69402730 D1 DE 69402730D1 DE 69402730 T DE69402730 T DE 69402730T DE 69402730 T DE69402730 T DE 69402730T DE 69402730 D1 DE69402730 D1 DE 69402730D1
- Authority
- DE
- Germany
- Prior art keywords
- securing method
- turbine chuck
- chuck
- turbine
- securing
- 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.)
- Expired - Lifetime
Links
Classifications
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
-
- 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
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/006,445 US5320486A (en) | 1993-01-21 | 1993-01-21 | Apparatus for positioning compressor liner segments |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69402730D1 true DE69402730D1 (de) | 1997-05-28 |
DE69402730T2 DE69402730T2 (de) | 1997-11-27 |
Family
ID=21720926
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69402730T Expired - Lifetime DE69402730T2 (de) | 1993-01-21 | 1994-01-14 | Sicherungsmethode für einen Turbinenfutter |
Country Status (4)
Country | Link |
---|---|
US (1) | US5320486A (de) |
EP (1) | EP0608080B1 (de) |
JP (1) | JPH0713471B2 (de) |
DE (1) | DE69402730T2 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2743603B1 (fr) * | 1996-01-11 | 1998-02-13 | Snecma | Dispositif de jonction de segments d'un distributeur circulaire a un carter de turbomachine |
US5971703A (en) * | 1997-12-05 | 1999-10-26 | Pratt & Whitney Canada Inc. | Seal assembly for a gas turbine engine |
FR2800797B1 (fr) | 1999-11-10 | 2001-12-07 | Snecma | Assemblage d'un anneau bordant une turbine a la structure de turbine |
FR2817285B1 (fr) * | 2000-11-30 | 2003-06-13 | Snecma Moteurs | Virole interne de stator |
US7114920B2 (en) * | 2004-06-25 | 2006-10-03 | Pratt & Whitney Canada Corp. | Shroud and vane segments having edge notches |
US20090110546A1 (en) * | 2007-10-29 | 2009-04-30 | United Technologies Corp. | Feather Seals and Gas Turbine Engine Systems Involving Such Seals |
GB2478144A (en) * | 2010-02-26 | 2011-08-31 | Rolls Royce Plc | Panelled assembly, eg for a gas turbine engine ducted fan casing |
US20110243725A1 (en) * | 2010-03-31 | 2011-10-06 | General Electric Company | Turbine shroud mounting apparatus with anti-rotation feature |
GB2494137B (en) | 2011-08-31 | 2016-02-17 | Rolls Royce Plc | A rotor casing liner comprising multiple sections |
FR2980235B1 (fr) * | 2011-09-20 | 2015-04-17 | Snecma | Anneau pour une turbine de turbomachine |
US9127568B2 (en) * | 2012-01-04 | 2015-09-08 | General Electric Company | Turbine casing |
US9200531B2 (en) | 2012-01-31 | 2015-12-01 | United Technologies Corporation | Fan case rub system, components, and their manufacture |
US9249681B2 (en) | 2012-01-31 | 2016-02-02 | United Technologies Corporation | Fan case rub system |
US9194299B2 (en) | 2012-12-21 | 2015-11-24 | United Technologies Corporation | Anti-torsion assembly |
US10669936B2 (en) | 2013-03-13 | 2020-06-02 | Raytheon Technologies Corporation | Thermally conforming acoustic liner cartridge for a gas turbine engine |
EP3008309B1 (de) | 2013-06-14 | 2018-04-25 | United Technologies Corporation | Flusssteuerungsvorrichtung für einen gasturbinenmotor |
US9759079B2 (en) | 2015-05-28 | 2017-09-12 | Rolls-Royce Corporation | Split line flow path seals |
US10697314B2 (en) | 2016-10-14 | 2020-06-30 | Rolls-Royce Corporation | Turbine shroud with I-beam construction |
US10557365B2 (en) | 2017-10-05 | 2020-02-11 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having reaction load distribution features |
US10718226B2 (en) | 2017-11-21 | 2020-07-21 | Rolls-Royce Corporation | Ceramic matrix composite component assembly and seal |
US10697315B2 (en) | 2018-03-27 | 2020-06-30 | Rolls-Royce North American Technologies Inc. | Full hoop blade track with keystoning segments |
US11028722B2 (en) | 2018-05-30 | 2021-06-08 | Rolls-Royce North American Technologies Inc. | Ceramic matrix composite blade track assembly with tip clearance control |
US11149563B2 (en) | 2019-10-04 | 2021-10-19 | Rolls-Royce Corporation | Ceramic matrix composite blade track with mounting system having axial reaction load distribution features |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA629283A (en) * | 1961-10-17 | P. Miller Joseph | Turbomachine stator assembly | |
GB225245A (en) * | 1923-11-23 | 1924-12-24 | British Thomson Houston Co Ltd | Improvements in and relating to elastic fluid turbines |
GB316411A (en) * | 1928-07-05 | 1929-08-01 | Karl Baumann | Improvements relating to elastic fluid turbines |
US2834537A (en) * | 1954-01-18 | 1958-05-13 | Ryan Aeronautical Co | Compressor stator structure |
GB786689A (en) * | 1955-11-09 | 1957-11-20 | Gen Motors Corp | Improvements relating to elastic-fluid turbines |
US2915280A (en) * | 1957-04-18 | 1959-12-01 | Gen Electric | Nozzle and seal assembly |
NL269161A (de) * | 1960-09-28 | |||
US3056583A (en) * | 1960-11-10 | 1962-10-02 | Gen Electric | Retaining means for turbine shrouds and nozzle diaphragms of turbine engines |
US3892497A (en) * | 1974-05-14 | 1975-07-01 | Westinghouse Electric Corp | Axial flow turbine stationary blade and blade ring locking arrangement |
GB2019954B (en) * | 1978-04-04 | 1982-08-04 | Rolls Royce | Turbomachine housing |
GB2076071B (en) * | 1980-05-16 | 1983-11-02 | United Technologies Corp | Flow directing assembly for a gas turbine engine |
US4573866A (en) * | 1983-05-02 | 1986-03-04 | United Technologies Corporation | Sealed shroud for rotating body |
DE3333436C1 (de) * | 1983-09-16 | 1985-02-14 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur Axial- und Umfangssicherung von statischen Gehaeusebauteilen fuer Stroemungsmaschinen |
FR2597921A1 (fr) * | 1986-04-24 | 1987-10-30 | Snecma | Anneau de turbine sectorise |
US4866942A (en) * | 1987-10-13 | 1989-09-19 | The United States Of America As Represented By The Secretary Of The Air Force | Augmentor curtain liner for equalizing pressure therein |
US4854122A (en) * | 1988-01-28 | 1989-08-08 | The United States Of America As Represented By The Secretary Of The Air Force | Augmentor curtain liner assembly for sharing tensile loading |
US4944151A (en) * | 1988-09-26 | 1990-07-31 | Avco Corporation | Segmented combustor panel |
GB2239678B (en) * | 1989-12-08 | 1993-03-03 | Rolls Royce Plc | Gas turbine engine blade shroud assembly |
US5076049A (en) * | 1990-04-02 | 1991-12-31 | General Electric Company | Pretensioned frame |
US5088888A (en) * | 1990-12-03 | 1992-02-18 | General Electric Company | Shroud seal |
US5080557A (en) * | 1991-01-14 | 1992-01-14 | General Motors Corporation | Turbine blade shroud assembly |
US5141395A (en) * | 1991-09-05 | 1992-08-25 | General Electric Company | Flow activated flowpath liner seal |
US5201846A (en) * | 1991-11-29 | 1993-04-13 | General Electric Company | Low-pressure turbine heat shield |
-
1993
- 1993-01-21 US US08/006,445 patent/US5320486A/en not_active Expired - Lifetime
-
1994
- 1994-01-14 EP EP94300271A patent/EP0608080B1/de not_active Expired - Lifetime
- 1994-01-14 DE DE69402730T patent/DE69402730T2/de not_active Expired - Lifetime
- 1994-01-20 JP JP6004309A patent/JPH0713471B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0608080B1 (de) | 1997-04-23 |
DE69402730T2 (de) | 1997-11-27 |
JPH06280613A (ja) | 1994-10-04 |
EP0608080A1 (de) | 1994-07-27 |
US5320486A (en) | 1994-06-14 |
JPH0713471B2 (ja) | 1995-02-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN |