BE551145A - - Google Patents

Info

Publication number: BE551145A
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.)

1955-09-26

Publication of BE551145A publication Critical patent/BE551145A/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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
- 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
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates

Landscapes

Engineering & Computer Science (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Turbine Rotor Nozzle Sealing (AREA)

BE551145D 1955-09-26 BE551145A (xx)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB3010696X		1955-09-26

Publications (1)

Publication Number	Publication Date
BE551145A true BE551145A (xx)

Family

ID=10919700

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BE551145D BE551145A (xx)	1955-09-26

Country Status (3)

Country	Link
US (1)	US3010696A (xx)
BE (1)	BE551145A (xx)
FR (1)	FR1158880A (xx)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
NL295165A (xx) *	1962-07-11
US3295825A (en) *	1965-03-10	1967-01-03	Gen Motors Corp	Multi-stage turbine rotor
US3471127A (en) *	1966-12-08	1969-10-07	Gen Motors Corp	Turbomachine rotor
US3446480A (en) *	1966-12-19	1969-05-27	Gen Motors Corp	Turbine rotor
US3490852A (en) *	1967-12-21	1970-01-20	Gen Electric	Gas turbine rotor bucket cooling and sealing arrangement
GB1479332A (en) *	1974-11-06	1977-07-13	Rolls Royce	Means for retaining blades to a disc or like structure
FR2524932A1 (fr) *	1982-04-08	1983-10-14	Snecma	Dispositif de retenue axiale de pieds d'aube dans un disque de turbomachine
JPS62118033A (ja) *	1985-11-04	1987-05-29	ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン	タ−ビンのデイスクとサイドプレ−トの組合体
GB8705216D0 (en) *	1987-03-06	1987-04-08	Rolls Royce Plc	Rotor assembly
US5030060A (en) *	1988-10-20	1991-07-09	The United States Of America As Represented By The Secretary Of The Air Force	Method and apparatus for cooling high temperature ceramic turbine blade portions
FR2663997B1 (fr) *	1990-06-27	1993-12-24	Snecma	Dispositif de fixation d'une couronne de revolution sur un disque de turbomachine.
EP2146051B1 (en) *	2008-07-17	2011-09-07	Ansaldo Energia S.P.A.	Rotor assembly for a gas turbine, gas turbine including said rotor assembly and method for cooling said rotor assembly
EP2236759A1 (de) *	2009-03-27	2010-10-06	Siemens Aktiengesellschaft	Laufschaufelsystem
FR2955889B1 (fr) *	2010-01-29	2012-11-16	Snecma	Moyen de blocage d'un flasque d'etancheite sur un disque de turbine
FR2982635B1 (fr) *	2011-11-15	2013-11-15	Snecma	Roue a aubes pour une turbomachine
EP2860351A1 (de) *	2013-10-10	2015-04-15	Siemens Aktiengesellschaft	Anordnung zum Sichern einer Funktionsstellung einer an einer Läuferscheibe angeordneten Deckplatte relativ zu einer an der Läuferscheibe angeordneten Laufschaufel
EP3141698A1 (en) *	2015-09-10	2017-03-15	Siemens Aktiengesellschaft	Arrangement for a gas turbine
JP6817329B2 (ja) *	2016-12-13	2021-01-20	三菱パワー株式会社	ガスタービンの分解組立方法、シール板組立体及びガスタービンロータ
MX2019006636A (es) *	2016-12-13	2019-08-01	Mitsubishi Hitachi Power Sys	Metodo para desmontar/montar turbina de gas, montaje de placa selladora y rotor de turbina de gas.
CN110073080B (zh)	2016-12-13	2021-10-19	三菱动力株式会社	燃气轮机的分解组装方法、燃气轮机转子以及燃气轮机
CA3000376A1 (en) *	2017-05-23	2018-11-23	Rolls-Royce Corporation	Turbine shroud assembly having ceramic matrix composite track segments with metallic attachment features

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
IT454293A (xx) *	1948-04-22
GB687507A (en) *	1949-06-28	1953-02-18	Cem Comp Electro Mec	Improvements in turbine and compressor blades
US2568726A (en) *	1949-08-03	1951-09-25	Franz Anselm	Air-cooled turbine blade
GB701263A (en) *	1950-08-03	1953-12-23	Rolls Royce	Improvements in or relating to turbo-machines
GB742477A (en) *	1952-10-31	1955-12-30	Rolls Royce	Improvements in or relating to bladed stator or rotor constructions for fluid machines such as axial-flow turbines or compressors
BE530262A (xx) *	1953-07-11
US2828940A (en) *	1953-12-30	1958-04-01	United Aircraft Corp	Cooled turbine blade

0
- BE BE551145D patent/BE551145A/xx unknown
1956
- 1956-09-10 US US608897A patent/US3010696A/en not_active Expired - Lifetime
- 1956-09-25 FR FR1158880D patent/FR1158880A/fr not_active Expired

Also Published As

Publication number	Publication date
US3010696A (en)	1961-11-28
FR1158880A (fr)	1958-06-20

Publication	Publication Date	Title
AT198143B (xx)	1958-06-10
AT194324B (xx)	1958-01-10
AT198671B (xx)	1958-07-25
AT195882B (xx)	1958-02-25
AT195787B (xx)	1958-02-25
AT195202B (xx)	1958-01-25
AT198478B (xx)	1958-07-10
AT193805B (xx)	1957-12-10
AT194860B (xx)	1958-01-25
AT196153B (xx)	1958-02-25
AT196487B (xx)	1958-03-25
AT195161B (xx)	1958-01-25
AT194962B (xx)	1958-01-25
AT195329B (xx)	1958-01-25
AT195450B (xx)	1958-02-10
AT195570B (xx)	1958-02-10
AT195613B (xx)	1958-02-25
AT195620B (xx)	1958-02-25
AT195663B (xx)	1958-02-25
AT195705B (xx)	1958-02-25
AT194664B (xx)	1958-01-10
AT195857B (xx)	1958-02-25
AT195858B (xx)	1958-02-25
AT194311B (xx)	1958-01-10
AT197200B (xx)	1958-04-10