FR2528494B1 - Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elements - Google Patents
Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elementsInfo
- Publication number
- FR2528494B1 FR2528494B1 FR8309424A FR8309424A FR2528494B1 FR 2528494 B1 FR2528494 B1 FR 2528494B1 FR 8309424 A FR8309424 A FR 8309424A FR 8309424 A FR8309424 A FR 8309424A FR 2528494 B1 FR2528494 B1 FR 2528494B1
- Authority
- FR
- France
- Prior art keywords
- assembly
- elements
- load distribution
- distribution element
- turbine
- 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
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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08216915A GB2121885B (en) | 1982-06-10 | 1982-06-10 | Load distribution member for a gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2528494A1 FR2528494A1 (fr) | 1983-12-16 |
FR2528494B1 true FR2528494B1 (fr) | 1986-12-19 |
Family
ID=10530951
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8309424A Expired FR2528494B1 (fr) | 1982-06-10 | 1983-06-07 | Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elements |
Country Status (5)
Country | Link |
---|---|
US (1) | US4521159A (fr) |
JP (1) | JPS593102A (fr) |
DE (1) | DE3320190C2 (fr) |
FR (1) | FR2528494B1 (fr) |
GB (1) | GB2121885B (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5181826A (en) * | 1990-11-23 | 1993-01-26 | General Electric Company | Attenuating shroud support |
DE10211684A1 (de) * | 2002-03-15 | 2003-10-16 | Johnson Contr Interiors Gmbh | Dichtungselement |
US8511982B2 (en) * | 2008-11-24 | 2013-08-20 | Alstom Technology Ltd. | Compressor vane diaphragm |
GB201013004D0 (en) * | 2010-08-03 | 2010-09-15 | Rolls Royce Plc | A seal assembly |
GB201013003D0 (en) | 2010-08-03 | 2010-09-15 | Rolls Royce Plc | A seal assembly |
ES2828719T3 (es) * | 2017-11-09 | 2021-05-27 | MTU Aero Engines AG | Disposición de sellado para una turbomáquina, método para la fabricación de una disposición de sellado y turbomáquina |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB190926712A (en) * | 1909-02-04 | 1910-11-17 | Brown Boveri & Company Ag | Steam or Gas Turbine. |
GB701101A (en) * | 1950-06-29 | 1953-12-16 | Rolls Royce | Improvements in or relating to gas-turbine engines |
BE530262A (fr) * | 1953-07-11 | |||
US3056579A (en) * | 1959-04-13 | 1962-10-02 | Gen Electric | Rotor construction |
US3314648A (en) * | 1961-12-19 | 1967-04-18 | Gen Electric | Stator vane assembly |
GB987016A (en) * | 1962-08-22 | 1965-03-24 | Ass Elect Ind | Improvements in turbine rotors |
GB969579A (en) * | 1962-11-09 | 1964-09-09 | Rolls Royce | Gas turbine engine |
GB944976A (en) * | 1962-11-12 | 1963-12-18 | Rolls Royce | Supporting bearings on shafts |
US3422902A (en) * | 1966-02-21 | 1969-01-21 | Herschede Hall Clock Co The | Well pack-off unit |
GB1221229A (en) * | 1967-12-11 | 1971-02-03 | Garrett Corp | Labyrinth seal |
FR1593039A (fr) * | 1968-09-27 | 1970-05-25 | ||
US3733146A (en) * | 1971-04-07 | 1973-05-15 | United Aircraft Corp | Gas seal rotatable support structure |
-
1982
- 1982-06-10 GB GB08216915A patent/GB2121885B/en not_active Expired
-
1983
- 1983-05-20 US US06/496,669 patent/US4521159A/en not_active Expired - Fee Related
- 1983-06-03 DE DE3320190A patent/DE3320190C2/de not_active Expired
- 1983-06-07 FR FR8309424A patent/FR2528494B1/fr not_active Expired
- 1983-06-08 JP JP58102514A patent/JPS593102A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
US4521159A (en) | 1985-06-04 |
JPS642773B2 (fr) | 1989-01-18 |
DE3320190C2 (de) | 1985-03-14 |
FR2528494A1 (fr) | 1983-12-16 |
GB2121885B (en) | 1985-07-31 |
DE3320190A1 (de) | 1983-12-15 |
JPS593102A (ja) | 1984-01-09 |
GB2121885A (en) | 1984-01-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |