CH315424A - Rangée circulaire d'aubes fixes d'une turbo-machine à écoulement axial - Google Patents
Rangée circulaire d'aubes fixes d'une turbo-machine à écoulement axialInfo
- Publication number
- CH315424A CH315424A CH315424DA CH315424A CH 315424 A CH315424 A CH 315424A CH 315424D A CH315424D A CH 315424DA CH 315424 A CH315424 A CH 315424A
- Authority
- CH
- Switzerland
- Prior art keywords
- machine
- axial flow
- circular row
- fixed vanes
- flow 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
-
- 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
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 |
---|---|---|---|
GB17415/52A GB736800A (en) | 1952-07-10 | 1952-07-10 | Improvements in or relating to stationary blade rings of axial flow turbines or compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
CH315424A true CH315424A (fr) | 1956-08-15 |
Family
ID=10094790
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH315424D CH315424A (fr) | 1952-07-10 | 1953-12-22 | Rangée circulaire d'aubes fixes d'une turbo-machine à écoulement axial |
Country Status (4)
Country | Link |
---|---|
US (1) | US2807433A (fr) |
CH (1) | CH315424A (fr) |
FR (1) | FR1095079A (fr) |
GB (1) | GB736800A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2556410A1 (fr) * | 1983-12-07 | 1985-06-14 | Snecma | Dispositif de centrage de l'anneau interieur d'un stator a ailettes a calage variable |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1095453B (de) * | 1955-07-18 | 1960-12-22 | Rolls Royce | Mehrstufige Axialstroemungsmaschine |
US2894719A (en) * | 1956-02-21 | 1959-07-14 | Douglas V Foster | Improved strut supported turbine blade |
DE1076877B (de) * | 1956-05-10 | 1960-03-03 | Rolls Royce | Leitrad fuer Axialstroemungsmaschinen |
DE1218800B (de) * | 1961-04-25 | 1966-06-08 | M A N Turbo Ges Mit Beschraenk | Gasturbine, insbesondere Kleingasturbine |
US4163629A (en) * | 1977-12-23 | 1979-08-07 | The United States Of America As Represented By The Secretary Of The Air Force | Turbine vane construction |
US4526512A (en) * | 1983-03-28 | 1985-07-02 | General Electric Co. | Cooling flow control device for turbine blades |
FR2607188B1 (fr) * | 1986-11-26 | 1991-02-08 | Snecma | Carter d'entree de turbomachine a bras rayonnants |
US4793770A (en) * | 1987-08-06 | 1988-12-27 | General Electric Company | Gas turbine engine frame assembly |
US5212940A (en) * | 1991-04-16 | 1993-05-25 | General Electric Company | Tip clearance control apparatus and method |
US5236303A (en) * | 1991-09-27 | 1993-08-17 | General Electric Company | Gas turbine engine structural frame with multi-clevis ring attachment of struts to outer casing |
US5180282A (en) * | 1991-09-27 | 1993-01-19 | General Electric Company | Gas turbine engine structural frame with multi-yoke attachment of struts to outer casing |
US6000906A (en) * | 1997-09-12 | 1999-12-14 | Alliedsignal Inc. | Ceramic airfoil |
GB2402717B (en) * | 2003-06-10 | 2006-05-10 | Rolls Royce Plc | A vane assembly for a gas turbine engine |
FR2940359B1 (fr) * | 2008-12-18 | 2014-11-28 | Snecma | Carter d'echappement pour turbomachine, comportant une ferrure d'accrochage dissociee de la virole exterieure. |
US8864445B2 (en) * | 2012-01-09 | 2014-10-21 | General Electric Company | Turbine nozzle assembly methods |
US10724380B2 (en) * | 2017-08-07 | 2020-07-28 | General Electric Company | CMC blade with internal support |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2622843A (en) * | 1947-12-17 | 1952-12-23 | Packard Motor Car Co | Turbine construction for turbojet engines |
-
1952
- 1952-07-10 GB GB17415/52A patent/GB736800A/en not_active Expired
-
1953
- 1953-12-11 US US397751A patent/US2807433A/en not_active Expired - Lifetime
- 1953-12-22 CH CH315424D patent/CH315424A/fr unknown
-
1954
- 1954-01-15 FR FR1095079D patent/FR1095079A/fr not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2556410A1 (fr) * | 1983-12-07 | 1985-06-14 | Snecma | Dispositif de centrage de l'anneau interieur d'un stator a ailettes a calage variable |
EP0146449A1 (fr) * | 1983-12-07 | 1985-06-26 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Dispositif de centrage de l'anneau intérieur d'un stator à ailettes à calage variable |
US4604030A (en) * | 1983-12-07 | 1986-08-05 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. | Compressor with variable incidence stator vanes |
Also Published As
Publication number | Publication date |
---|---|
US2807433A (en) | 1957-09-24 |
FR1095079A (fr) | 1955-05-26 |
GB736800A (en) | 1955-09-14 |
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