GB738213A - Construction of turbine stator blades - Google Patents
Construction of turbine stator bladesInfo
- Publication number
- GB738213A GB738213A GB15155/53A GB1515553A GB738213A GB 738213 A GB738213 A GB 738213A GB 15155/53 A GB15155/53 A GB 15155/53A GB 1515553 A GB1515553 A GB 1515553A GB 738213 A GB738213 A GB 738213A
- Authority
- GB
- United Kingdom
- Prior art keywords
- core
- stator
- ribs
- bolt
- channels
- 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
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
- Motor Or Generator Cooling System (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE529252D BE529252A (pt) | 1953-06-01 | ||
GB15155/53A GB738213A (en) | 1953-06-01 | 1953-06-01 | Construction of turbine stator blades |
US428736A US2833514A (en) | 1953-06-01 | 1954-05-10 | Construction of turbine stator blades |
DEA20380A DE952222C (de) | 1953-06-01 | 1954-05-22 | Statorschaufel fuer Gasturbinen |
FR1101346D FR1101346A (fr) | 1953-06-01 | 1954-05-25 | Perfectionnements aux ailettes de stators de turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15155/53A GB738213A (en) | 1953-06-01 | 1953-06-01 | Construction of turbine stator blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB738213A true GB738213A (en) | 1955-10-12 |
Family
ID=10054006
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15155/53A Expired GB738213A (en) | 1953-06-01 | 1953-06-01 | Construction of turbine stator blades |
Country Status (5)
Country | Link |
---|---|
US (1) | US2833514A (pt) |
BE (1) | BE529252A (pt) |
DE (1) | DE952222C (pt) |
FR (1) | FR1101346A (pt) |
GB (1) | GB738213A (pt) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2894719A (en) * | 1956-02-21 | 1959-07-14 | Douglas V Foster | Improved strut supported turbine blade |
DE1097212B (de) * | 1956-10-22 | 1961-01-12 | Her Majesty The Queen In The R | Mit Kuehlkanaelen versehene Schaufel, insbesondere fuer Gasturbinen |
DE1104265B (de) * | 1959-04-02 | 1961-04-06 | Her Majesty The Queen | Laufrad fuer Gasturbinen mit luftgekuehlten Laufschaufeln |
DE1297938B (de) * | 1964-12-07 | 1969-06-19 | United Aircraft Corp | Leitschaufel mit Waermeschild, insbesondere fuer Gasturbinen |
US3468513A (en) * | 1966-06-11 | 1969-09-23 | Daimler Benz Ag | Cooled rotor blade |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1021644B (de) * | 1955-05-18 | 1957-12-27 | Messerschmitt Ag | Laufschaufel fuer Gasturbinen mit Oberflaechenkuehlung |
NL99435C (pt) * | 1957-08-22 | |||
DE1167117B (de) * | 1960-04-12 | 1964-04-02 | Siemens Ag | Gasturbinenschaufelanordnung fuer Innenkuehlung |
DE1185415B (de) * | 1962-02-03 | 1965-01-14 | Gasturbinenbau Und Energiemasc | Einrichtung zum Kuehlen von Turbinenscheiben einer Gasturbine |
GB1018747A (en) * | 1964-11-13 | 1966-02-02 | Rolls Royce | Aerofoil shaped blade for fluid flow machines |
US3367628A (en) * | 1966-10-31 | 1968-02-06 | United Aircraft Corp | Movable vane unit |
US3471126A (en) * | 1966-10-31 | 1969-10-07 | United Aircraft Corp | Movable vane unit |
GB1605310A (en) * | 1975-05-30 | 1989-02-01 | Rolls Royce | Nozzle guide vane structure |
FR2491549B1 (fr) * | 1980-10-08 | 1985-07-05 | Snecma | Dispositif de refroidissement d'une turbine a gaz, par prelevement d'air au niveau du compresseur |
US5413463A (en) * | 1991-12-30 | 1995-05-09 | General Electric Company | Turbulated cooling passages in gas turbine buckets |
US6997679B2 (en) * | 2003-12-12 | 2006-02-14 | General Electric Company | Airfoil cooling holes |
FR2984428B1 (fr) * | 2011-12-19 | 2018-12-07 | Safran Aircraft Engines | Redresseur de compresseur pour turbomachine. |
JP6934350B2 (ja) * | 2017-08-03 | 2021-09-15 | 三菱パワー株式会社 | ガスタービン |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA491905A (en) * | 1953-04-07 | Rolls-Royce Limited | Gas-turbine engines and nozzle-guide vane assemblies therefor | |
CA491904A (en) * | 1953-04-07 | Rolls-Royce Limited | Gas-turbine engines and nozzle-guide vane assemblies therefor | |
DE872695C (de) * | 1941-03-28 | 1953-04-27 | Versuchsanstalt Fuer Luftfahrt | Hohlschaufel, insbesondere fuer Gas- oder Abgasturbinen |
GB602530A (en) * | 1945-10-16 | 1948-05-28 | Bristol Aeroplane Co Ltd | Improvements in or relating to gas turbines |
GB619107A (en) * | 1946-11-21 | 1949-03-03 | Brush Electrical Eng | Improvements in and relating to turbine blading |
FR949459A (fr) * | 1947-07-09 | 1949-08-31 | Aubes pour rotors | |
GB666537A (en) * | 1949-08-27 | 1952-02-13 | Armstrong Siddeley Motors Ltd | Mounting of the stator blades of a gaseous fluid turbine |
BE498667A (pt) * | 1949-08-27 |
-
0
- BE BE529252D patent/BE529252A/xx unknown
-
1953
- 1953-06-01 GB GB15155/53A patent/GB738213A/en not_active Expired
-
1954
- 1954-05-10 US US428736A patent/US2833514A/en not_active Expired - Lifetime
- 1954-05-22 DE DEA20380A patent/DE952222C/de not_active Expired
- 1954-05-25 FR FR1101346D patent/FR1101346A/fr not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2894719A (en) * | 1956-02-21 | 1959-07-14 | Douglas V Foster | Improved strut supported turbine blade |
DE1097212B (de) * | 1956-10-22 | 1961-01-12 | Her Majesty The Queen In The R | Mit Kuehlkanaelen versehene Schaufel, insbesondere fuer Gasturbinen |
DE1104265B (de) * | 1959-04-02 | 1961-04-06 | Her Majesty The Queen | Laufrad fuer Gasturbinen mit luftgekuehlten Laufschaufeln |
DE1297938B (de) * | 1964-12-07 | 1969-06-19 | United Aircraft Corp | Leitschaufel mit Waermeschild, insbesondere fuer Gasturbinen |
US3468513A (en) * | 1966-06-11 | 1969-09-23 | Daimler Benz Ag | Cooled rotor blade |
Also Published As
Publication number | Publication date |
---|---|
BE529252A (pt) | |
DE952222C (de) | 1956-11-15 |
US2833514A (en) | 1958-05-06 |
FR1101346A (fr) | 1955-10-05 |
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