FR1003299A - Perfectionnement aux turbines à gaz et autres turbo-machines axiales - Google Patents
Perfectionnement aux turbines à gaz et autres turbo-machines axialesInfo
- Publication number
- FR1003299A FR1003299A FR1003299DA FR1003299A FR 1003299 A FR1003299 A FR 1003299A FR 1003299D A FR1003299D A FR 1003299DA FR 1003299 A FR1003299 A FR 1003299A
- Authority
- FR
- France
- Prior art keywords
- machines
- gas turbines
- further training
- axial turbo
- turbo
- 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
-
- 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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1003299T | 1949-12-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1003299A true FR1003299A (fr) | 1952-03-17 |
Family
ID=9562875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1003299D Expired FR1003299A (fr) | 1949-12-13 | 1949-12-13 | Perfectionnement aux turbines à gaz et autres turbo-machines axiales |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1003299A (fr) |
GB (1) | GB689270A (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE954835C (de) * | 1954-02-04 | 1956-12-20 | Canadian Patents Dev | Gehaeusering fuer Kreiselradmaschinen, insbesondere fuer Gasturbinen |
DE960328C (de) * | 1952-09-27 | 1957-03-21 | Tech Studien Ag | Abdichteinrrichtung an einem Gehaeuse fuer Gas- oder Dampfturbinen |
DE1259142B (de) * | 1962-02-14 | 1968-01-18 | Licentia Gmbh | Ringflansch des rohrfoermigen Innen- oder Aussengehaeuses einer Axialgas- oder -dampfturbine |
DE4230235A1 (de) * | 1992-09-10 | 1994-03-17 | Asea Brown Boveri | Axialdurchströmte Gasturbine |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2738921A (en) * | 1950-11-22 | 1956-03-20 | United Aircraft Corp | Boundary layer control apparatus for compressors |
US2917276A (en) * | 1955-02-28 | 1959-12-15 | Orenda Engines Ltd | Segmented stator ring assembly |
US2962256A (en) * | 1956-03-28 | 1960-11-29 | Napier & Son Ltd | Turbine blade shroud rings |
US3000552A (en) * | 1957-05-28 | 1961-09-19 | Gen Motors Corp | Compressor vane mounting |
US3066911A (en) * | 1959-05-12 | 1962-12-04 | Thompson Ramo Wooldridge Inc | Nozzle and turbine wheel shroud support |
US3043564A (en) * | 1960-03-14 | 1962-07-10 | United Aircraft Corp | Stator construction |
US3142475A (en) * | 1962-12-28 | 1964-07-28 | Gen Electric | Stator assembly |
US4131388A (en) * | 1977-05-26 | 1978-12-26 | United Technologies Corporation | Outer air seal |
FR2577281B1 (fr) * | 1985-02-13 | 1987-03-20 | Snecma | Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter |
GB2206651B (en) * | 1987-07-01 | 1991-05-08 | Rolls Royce Plc | Turbine blade shroud structure |
EP0591565B1 (fr) * | 1992-10-05 | 1996-01-24 | Asea Brown Boveri Ag | Fixation d'aube statorique pour turbomachine à écoulement axial |
IT1318103B1 (it) | 2000-07-03 | 2003-07-23 | Nuovo Pignone Spa | Sistema di connessione tra un ugello di bassa pressione ed untransition duct in una turbina a gas |
EP2236761A1 (fr) * | 2009-04-02 | 2010-10-06 | Siemens Aktiengesellschaft | Support d'aube directrice |
-
1949
- 1949-12-13 FR FR1003299D patent/FR1003299A/fr not_active Expired
-
1950
- 1950-12-11 GB GB30273/50A patent/GB689270A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE960328C (de) * | 1952-09-27 | 1957-03-21 | Tech Studien Ag | Abdichteinrrichtung an einem Gehaeuse fuer Gas- oder Dampfturbinen |
DE954835C (de) * | 1954-02-04 | 1956-12-20 | Canadian Patents Dev | Gehaeusering fuer Kreiselradmaschinen, insbesondere fuer Gasturbinen |
DE1259142B (de) * | 1962-02-14 | 1968-01-18 | Licentia Gmbh | Ringflansch des rohrfoermigen Innen- oder Aussengehaeuses einer Axialgas- oder -dampfturbine |
DE4230235A1 (de) * | 1992-09-10 | 1994-03-17 | Asea Brown Boveri | Axialdurchströmte Gasturbine |
Also Published As
Publication number | Publication date |
---|---|
GB689270A (en) | 1953-03-25 |
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