CH341029A - Installation à turbine à gaz - Google Patents
Installation à turbine à gazInfo
- Publication number
- CH341029A CH341029A CH341029DA CH341029A CH 341029 A CH341029 A CH 341029A CH 341029D A CH341029D A CH 341029DA CH 341029 A CH341029 A CH 341029A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- turbine plant
- plant
- gas
- turbine
- Prior art date
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
- F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
-
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
- Breeding Of Plants And Reproduction By Means Of Culturing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB32312/53A GB789203A (en) | 1953-11-20 | 1953-11-20 | Improvements in or relating to combustion turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH341029A true CH341029A (fr) | 1959-09-15 |
Family
ID=10336640
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH341029D CH341029A (fr) | 1953-11-20 | 1954-11-12 | Installation à turbine à gaz |
Country Status (7)
Country | Link |
---|---|
US (1) | US2912221A (xx) |
BE (1) | BE533517A (xx) |
CH (1) | CH341029A (xx) |
DE (1) | DE1023275B (xx) |
FR (1) | FR1114538A (xx) |
GB (1) | GB789203A (xx) |
NL (2) | NL192509A (xx) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1258165B (de) * | 1964-07-22 | 1968-01-04 | Litton Industries Inc | Beschleunigungsmesser mit in einer Fluessigkeit schwebendem Pendel |
US3647313A (en) * | 1970-06-01 | 1972-03-07 | Gen Electric | Gas turbine engines with compressor rotor cooling |
FR2484574A1 (fr) * | 1980-06-13 | 1981-12-18 | Snecma | Palier inter-arbres de turbomachine multi-corps a amortissement par pellicule d'huile |
FR2851288B1 (fr) * | 2003-02-14 | 2006-07-28 | Snecma Moteurs | Dispositif de refroidissement de disques de turbines |
US7942635B1 (en) * | 2007-08-02 | 2011-05-17 | Florida Turbine Technologies, Inc. | Twin spool rotor assembly for a small gas turbine engine |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE737397C (de) * | 1934-04-01 | 1943-07-12 | Michael Martinka Dipl Ing | Kuehlungseinrichtung fuer Turbinenlaufraeder |
DE767312C (de) * | 1939-10-17 | 1952-05-02 | Daimler Benz Ag | Kuehlung von Abgasturbinen |
BE478671A (xx) * | 1939-12-19 | 1948-01-31 | ||
NL68201C (xx) * | 1939-12-19 | |||
FR919016A (fr) * | 1944-12-18 | 1947-02-25 | Oerlikon Maschf | Turbo-machine refroidie |
CH268947A (de) * | 1945-06-08 | 1950-06-15 | Power Jets Res & Dev Ltd | Mehrstufenturbine. |
US2657901A (en) * | 1945-06-08 | 1953-11-03 | Power Jets Res & Dev Ltd | Construction of turbine rotors |
BE481135A (xx) * | 1947-03-11 | |||
US2620157A (en) * | 1947-05-06 | 1952-12-02 | Rolls Royce | Gas-turbine engine |
US2672013A (en) * | 1950-06-30 | 1954-03-16 | Curtiss Wright Corp | Gas turbine cooling system |
-
0
- BE BE533517D patent/BE533517A/xx unknown
- NL NL99245D patent/NL99245C/xx active
- NL NL192509D patent/NL192509A/xx unknown
-
1953
- 1953-11-20 GB GB32312/53A patent/GB789203A/en not_active Expired
-
1954
- 1954-11-06 DE DEN9702A patent/DE1023275B/de active Pending
- 1954-11-08 US US467576A patent/US2912221A/en not_active Expired - Lifetime
- 1954-11-10 FR FR1114538D patent/FR1114538A/fr not_active Expired
- 1954-11-12 CH CH341029D patent/CH341029A/fr unknown
Also Published As
Publication number | Publication date |
---|---|
US2912221A (en) | 1959-11-10 |
GB789203A (en) | 1958-01-15 |
BE533517A (xx) | |
NL99245C (xx) | |
FR1114538A (fr) | 1956-04-13 |
DE1023275B (de) | 1958-01-23 |
NL192509A (xx) |
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