BE895285A - IMPROVEMENTS ON GAS TURBINE BLADES - Google Patents
IMPROVEMENTS ON GAS TURBINE BLADESInfo
- Publication number
- BE895285A BE895285A BE0/209682A BE209682A BE895285A BE 895285 A BE895285 A BE 895285A BE 0/209682 A BE0/209682 A BE 0/209682A BE 209682 A BE209682 A BE 209682A BE 895285 A BE895285 A BE 895285A
- Authority
- BE
- Belgium
- Prior art keywords
- gas turbine
- turbine blades
- blades
- gas
- turbine
- 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
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Pulleys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US32888481A | 1981-12-09 | 1981-12-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE895285A true BE895285A (en) | 1983-06-08 |
Family
ID=23282872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE0/209682A BE895285A (en) | 1981-12-09 | 1982-12-08 | IMPROVEMENTS ON GAS TURBINE BLADES |
Country Status (6)
Country | Link |
---|---|
JP (2) | JPS58106102A (en) |
AR (1) | AR228927A1 (en) |
BE (1) | BE895285A (en) |
GB (1) | GB2111604A (en) |
IT (1) | IT1153370B (en) |
MX (1) | MX157531A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3419674A1 (en) * | 1983-05-26 | 1984-11-29 | Rolls-Royce Ltd., London | METHOD FOR APPLYING A COATING TO A COMPONENT |
KR20010006106A (en) * | 1997-04-07 | 2001-01-26 | 칼 하인쯔 호르닝어 | Method for cooling a turbine blade |
DE19939179B4 (en) * | 1999-08-20 | 2007-08-02 | Alstom | Coolable blade for a gas turbine |
EP1457641A1 (en) * | 2003-03-11 | 2004-09-15 | Siemens Aktiengesellschaft | Method for cooling a hot gas guiding component and component to be cooled |
US8727727B2 (en) * | 2010-12-10 | 2014-05-20 | General Electric Company | Components with cooling channels and methods of manufacture |
US9115590B2 (en) * | 2012-09-26 | 2015-08-25 | United Technologies Corporation | Gas turbine engine airfoil cooling circuit |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5672201A (en) * | 1979-11-14 | 1981-06-16 | Hitachi Ltd | Cooling structure of gas turbine blade |
-
1982
- 1982-12-06 IT IT24620/82A patent/IT1153370B/en active
- 1982-12-07 GB GB08234832A patent/GB2111604A/en not_active Withdrawn
- 1982-12-08 BE BE0/209682A patent/BE895285A/en not_active IP Right Cessation
- 1982-12-08 MX MX195506A patent/MX157531A/en unknown
- 1982-12-09 AR AR291543A patent/AR228927A1/en active
- 1982-12-09 JP JP57214732A patent/JPS58106102A/en active Pending
-
1986
- 1986-08-12 JP JP1986122995U patent/JPH0110401Y2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPH0110401Y2 (en) | 1989-03-24 |
AR228927A1 (en) | 1983-04-29 |
JPS6278302U (en) | 1987-05-19 |
IT1153370B (en) | 1987-01-14 |
MX157531A (en) | 1988-11-28 |
GB2111604A (en) | 1983-07-06 |
IT8224620A0 (en) | 1982-12-06 |
IT8224620A1 (en) | 1984-06-06 |
JPS58106102A (en) | 1983-06-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2100808B (en) | Blade root modification for a gas turbine engine | |
GB2163218B (en) | Cooled vane or blade for a gas turbine engine | |
GB2103294B (en) | Shroud assembly for a gas turbine engine | |
GB2093126B (en) | Rotor blade for a gas turbine engine | |
JPS56168040A (en) | Circular combustor for gas turbine engine | |
JPS57142422A (en) | Combustor for gas turbine engine | |
FR2337255A1 (en) | GAS TURBINE IMPROVEMENTS | |
GB2117450B (en) | Casing support for a gas turbine engine | |
GB1555587A (en) | Aerofoil blade for a gas turbine engine | |
GB2087979B (en) | Gas turbine engine blade tip seal | |
FR2413551B1 (en) | GAS TURBINE INSTALLATION | |
GB2114661B (en) | Casing structure for a gas turbine engine | |
IT8321090A0 (en) | PRE-DIFFUSER FOR GAS TURBINE ENGINES. | |
GB2076071B (en) | Flow directing assembly for a gas turbine engine | |
GB2100807B (en) | Turbine blade for gas turbine engines | |
BE895473A (en) | IMPROVEMENTS ON GAS TURBINE BLADES | |
FR2427468B1 (en) | IMPROVED COOLING DEVICE FOR GAS TURBINE BLADES | |
BR8201026A (en) | GAS TURBINE COMPRESSOR | |
DE3263299D1 (en) | Annular air-cooled abradable-blade tip-sealing shroud for a gas turbine or a compressor | |
GB1552536A (en) | Rotor blade for a gas turbine engine | |
GB2049069B (en) | Rotor assembly for a gas turbine engine | |
GB2107405B (en) | Nozzle guide vane for a gas turbine engine | |
BE895285A (en) | IMPROVEMENTS ON GAS TURBINE BLADES | |
DE2860416D1 (en) | Admission system for a gas turbine compressor | |
GB1556274A (en) | Blade carrying disc for a gas turbine engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RE | Patent lapsed |
Owner name: WESTINGHOUSE ELECTRIC CORP. Effective date: 19851231 |