CH369250A - Axial turbo compressor - Google Patents
Axial turbo compressorInfo
- Publication number
- CH369250A CH369250A CH7444859A CH7444859A CH369250A CH 369250 A CH369250 A CH 369250A CH 7444859 A CH7444859 A CH 7444859A CH 7444859 A CH7444859 A CH 7444859A CH 369250 A CH369250 A CH 369250A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbo compressor
- axial turbo
- axial
- compressor
- turbo
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
- F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
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 |
---|---|---|---|
US74220558A | 1958-06-16 | 1958-06-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH369250A true CH369250A (en) | 1963-05-15 |
Family
ID=24983890
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH7444859A CH369250A (en) | 1958-06-16 | 1959-06-15 | Axial turbo compressor |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH369250A (en) |
FR (1) | FR1227668A (en) |
GB (1) | GB856599A (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3269702A (en) * | 1964-01-13 | 1966-08-30 | United Aircraft Corp | Nozzle vane assembly |
US3798899A (en) * | 1971-12-29 | 1974-03-26 | Power Technology Corp | Gas turbine engine |
GB1335145A (en) * | 1972-01-12 | 1973-10-24 | Rolls Royce | Turbine casing for a gas turbine engine |
GB2043798B (en) * | 1979-03-14 | 1983-01-12 | Rolls Royce | Gas turbine stator vane assembly |
DE3315914A1 (en) * | 1983-05-02 | 1984-11-08 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | GAS TURBINE ENGINE WITH DEVICES FOR VANIZING GAPS |
GB9306719D0 (en) * | 1993-03-31 | 1993-06-02 | Rolls Royce Plc | A turbine assembly for a gas turbine engine |
FR2817285B1 (en) * | 2000-11-30 | 2003-06-13 | Snecma Moteurs | STATOR INTERNAL OIL |
FR2829525B1 (en) * | 2001-09-13 | 2004-03-12 | Snecma Moteurs | ASSEMBLY OF SECTORS OF A TURBINE DISTRIBUTOR TO A CRANKCASE |
FR2835563B1 (en) * | 2002-02-07 | 2004-04-02 | Snecma Moteurs | ARRANGEMENT FOR HANGING SECTORS IN A CIRCLE OF A CIRCLE OF A BLADE-BEARING DISTRIBUTOR |
DE10214569A1 (en) * | 2002-04-02 | 2003-10-16 | Rolls Royce Deutschland | Stator blade segment attachment for a gas turbine |
FR2852053B1 (en) * | 2003-03-06 | 2007-12-28 | Snecma Moteurs | HIGH PRESSURE TURBINE FOR TURBOMACHINE |
GB2425155B (en) * | 2005-04-13 | 2007-09-19 | Rolls Royce Plc | A mounting arrangement |
FR2887939B1 (en) | 2005-06-29 | 2016-09-30 | Soc Nat D'etude Et De Construction De Moteurs D'aviation Snecma | TURBOMACHINE MULTI-STAGE COMPRESSOR |
US10428832B2 (en) * | 2012-08-06 | 2019-10-01 | United Technologies Corporation | Stator anti-rotation lug |
DE102022124843A1 (en) | 2022-09-27 | 2024-03-28 | Audi Aktiengesellschaft | Connection device and electrical machine comprising it |
-
1959
- 1959-05-04 GB GB1512159A patent/GB856599A/en not_active Expired
- 1959-06-15 CH CH7444859A patent/CH369250A/en unknown
- 1959-06-16 FR FR797640A patent/FR1227668A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR1227668A (en) | 1960-08-22 |
GB856599A (en) | 1960-12-21 |
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