BE529252A - - Google Patents

Info

Publication number: BE529252A
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.)

1953-06-01

Publication of BE529252A publication Critical patent/BE529252A/xx

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)

BE529252D 1953-06-01 BE529252A (en)

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 (en)

Family

ID=10054006

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BE529252D BE529252A (en)	1953-06-01

Country Status (5)

Country	Link
US (1)	US2833514A (en)
BE (1)	BE529252A (en)
DE (1)	DE952222C (en)
FR (1)	FR1101346A (en)
GB (1)	GB738213A (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE1021644B (en) *	1955-05-18	1957-12-27	Messerschmitt Ag	Blade for gas turbines with surface cooling
US2894719A (en) *	1956-02-21	1959-07-14	Douglas V Foster	Improved strut supported turbine blade
DE1097212B (en) *	1956-10-22	1961-01-12	Her Majesty The Queen In The R	Blade provided with cooling ducts, especially for gas turbines
BE570533A (en) *	1957-08-22
DE1104265B (en) *	1959-04-02	1961-04-06	Her Majesty The Queen	Impeller for gas turbines with air-cooled blades
DE1167117B (en) *	1960-04-12	1964-04-02	Siemens Ag	Gas turbine blade arrangement for internal cooling
DE1185415B (en) *	1962-02-03	1965-01-14	Gasturbinenbau Und Energiemasc	Device for cooling turbine disks of a gas turbine
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 (en) *	1966-06-11	1974-01-17	Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen	Cooled blade
US3471126A (en) *	1966-10-31	1969-10-07	United Aircraft Corp	Movable vane unit
US3367628A (en) *	1966-10-31	1968-02-06	United Aircraft Corp	Movable vane unit
GB1605310A (en) *	1975-05-30	1989-02-01	Rolls Royce	Nozzle guide vane structure
FR2491549B1 (en) *	1980-10-08	1985-07-05	Snecma	DEVICE FOR COOLING A GAS TURBINE, BY TAKING AIR FROM THE COMPRESSOR
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 (en) *	2011-12-19	2018-12-07	Safran Aircraft Engines	COMPRESSOR RECTIFIER FOR TURBOMACHINE.
JP6934350B2 (en) *	2017-08-03	2021-09-15	三菱パワー株式会社	gas turbine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
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 (en) *	1941-03-28	1953-04-27	Versuchsanstalt Fuer Luftfahrt	Hollow blade, especially for gas or exhaust gas turbines
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 (en) *	1947-07-09	1949-08-31		Blades for rotors
BE498667A (en) *	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

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/en not_active Expired
- 1954-05-25 FR FR1101346D patent/FR1101346A/en not_active Expired

Also Published As

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

Publication	Publication Date	Title
AT193854B (en)	1957-12-10
AT191364A (en)	1957-08-26
AT190646B (en)	1957-07-10
BE517130A (en)	1953-02-14
AT193331B (en)	1957-11-25
AT189958B (en)	1957-05-25
AT191140B (en)	1957-08-10
AT192380B (en)	1957-10-10
AT191026B (en)	1957-07-25
AT199365B (en)	1958-08-25
AT191238B (en)	1957-08-10
AT213751B (en)	1961-02-27
AT205166B (en)	1959-09-10
AT194074B (en)	1957-12-27
AT194824B (en)	1958-01-25
AT194372B (en)	1958-01-10
AT195162B (en)	1958-01-25
AT195400B (en)	1958-01-25
AT196785B (en)	1958-03-25
AT197771B (en)	1958-05-27
AT199317B (en)	1958-08-25
BE517254A (en)
BE326981A (en)
BE51713A (en)
BE488396A (en)