BE529252A - - Google Patents

Info

Publication number
BE529252A
BE529252A BE529252DA BE529252A BE 529252 A BE529252 A BE 529252A BE 529252D A BE529252D A BE 529252DA BE 529252 A BE529252 A BE 529252A
Authority
BE
Belgium
Application number
Priority date (The priority date 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 date listed.)
Publication of BE529252A publication Critical patent/BE529252A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; 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)
BE529252D 1953-06-01 BE529252A (US06262066-20010717-C00359.png)

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
BE529252A true BE529252A (US06262066-20010717-C00359.png)

Family

ID=10054006

Family Applications (1)

Application Number Title Priority Date Filing Date
BE529252D BE529252A (US06262066-20010717-C00359.png) 1953-06-01

Country Status (5)

Country Link
US (1) US2833514A (US06262066-20010717-C00359.png)
BE (1) BE529252A (US06262066-20010717-C00359.png)
DE (1) DE952222C (US06262066-20010717-C00359.png)
FR (1) FR1101346A (US06262066-20010717-C00359.png)
GB (1) GB738213A (US06262066-20010717-C00359.png)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1021644B (de) * 1955-05-18 1957-12-27 Messerschmitt Ag Laufschaufel fuer Gasturbinen mit Oberflaechenkuehlung
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
NL230456A (US06262066-20010717-C00359.png) * 1957-08-22
DE1104265B (de) * 1959-04-02 1961-04-06 Her Majesty The Queen Laufrad fuer Gasturbinen mit luftgekuehlten Laufschaufeln
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
US3269700A (en) * 1964-12-07 1966-08-30 United Aircraft Corp Heat shield for turbine strut
DE1476755B2 (de) * 1966-06-11 1974-01-17 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Gekühlte Laufschaufel
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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA491904A (en) * 1953-04-07 Rolls-Royce Limited Gas-turbine engines and nozzle-guide vane assemblies therefor
CA491905A (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
BE498667A (US06262066-20010717-C00359.png) * 1949-08-27
GB666537A (en) * 1949-08-27 1952-02-13 Armstrong Siddeley Motors Ltd Mounting of the stator blades of a gaseous fluid turbine

Also Published As

Publication number Publication date
GB738213A (en) 1955-10-12
US2833514A (en) 1958-05-06
DE952222C (de) 1956-11-15
FR1101346A (fr) 1955-10-05

Similar Documents

Publication Publication Date Title
IT547049A (US06262066-20010717-C00359.png)
IT519690A (US06262066-20010717-C00359.png)
AT193854B (US06262066-20010717-C00359.png)
JPS325215B1 (US06262066-20010717-C00359.png)
AT191364A (US06262066-20010717-C00359.png)
AT190646B (US06262066-20010717-C00359.png)
AT193331B (US06262066-20010717-C00359.png)
FR1074937A (US06262066-20010717-C00359.png)
AT192380B (US06262066-20010717-C00359.png)
AT189958B (US06262066-20010717-C00359.png)
AT191140B (US06262066-20010717-C00359.png)
AT191026B (US06262066-20010717-C00359.png)
JPS317972B1 (US06262066-20010717-C00359.png)
AT199365B (US06262066-20010717-C00359.png)
FR57621E (US06262066-20010717-C00359.png)
AT191238B (US06262066-20010717-C00359.png)
AT194824B (US06262066-20010717-C00359.png)
AT213751B (US06262066-20010717-C00359.png)
AT205166B (US06262066-20010717-C00359.png)
FR1038965A (US06262066-20010717-C00359.png)
AT195162B (US06262066-20010717-C00359.png)
FR1032506A (US06262066-20010717-C00359.png)
DE1004306C2 (US06262066-20010717-C00359.png)
AT194074B (US06262066-20010717-C00359.png)
AT196785B (US06262066-20010717-C00359.png)