IT1153370B - Elemento a profilo aerodinamico per palette di turbina a combustione, raffreddato tra il longherone e l'involucro, utilizzante cavita' multiple del longherone - Google Patents
Elemento a profilo aerodinamico per palette di turbina a combustione, raffreddato tra il longherone e l'involucro, utilizzante cavita' multiple del longheroneInfo
- Publication number
- IT1153370B IT1153370B IT24620/82A IT2462082A IT1153370B IT 1153370 B IT1153370 B IT 1153370B IT 24620/82 A IT24620/82 A IT 24620/82A IT 2462082 A IT2462082 A IT 2462082A IT 1153370 B IT1153370 B IT 1153370B
- Authority
- IT
- Italy
- Prior art keywords
- longherone
- envelope
- cooled
- turbine blades
- profile element
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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 (3)
| Publication Number | Publication Date |
|---|---|
| IT8224620A0 IT8224620A0 (it) | 1982-12-06 |
| IT8224620A1 IT8224620A1 (it) | 1984-06-06 |
| IT1153370B true IT1153370B (it) | 1987-01-14 |
Family
ID=23282872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT24620/82A IT1153370B (it) | 1981-12-09 | 1982-12-06 | Elemento a profilo aerodinamico per palette di turbina a combustione, raffreddato tra il longherone e l'involucro, utilizzante cavita' multiple del longherone |
Country Status (6)
| Country | Link |
|---|---|
| JP (2) | JPS58106102A (OSRAM) |
| AR (1) | AR228927A1 (OSRAM) |
| BE (1) | BE895285A (OSRAM) |
| GB (1) | GB2111604A (OSRAM) |
| IT (1) | IT1153370B (OSRAM) |
| MX (1) | MX157531A (OSRAM) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3419674A1 (de) * | 1983-05-26 | 1984-11-29 | Rolls-Royce Ltd., London | Verfahren zum aufbringen eines ueberzugs auf ein bauteil |
| EP0973998B1 (de) * | 1997-04-07 | 2001-09-19 | Siemens Aktiengesellschaft | Verfahren zur kühlung einer turbinenschaufel |
| DE19939179B4 (de) | 1999-08-20 | 2007-08-02 | Alstom | Kühlbare Schaufel für eine Gasturbine |
| EP1457641A1 (de) * | 2003-03-11 | 2004-09-15 | Siemens Aktiengesellschaft | Verfahren zum Kühlen eines heissgasführenden Bauteils und ein zu kühlendes Bauteil |
| RU2263791C1 (ru) * | 2004-03-19 | 2005-11-10 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") | Охлаждаемая рабочая лопатка турбины |
| 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/it active
- 1982-12-07 GB GB08234832A patent/GB2111604A/en not_active Withdrawn
- 1982-12-08 MX MX195506A patent/MX157531A/es unknown
- 1982-12-08 BE BE0/209682A patent/BE895285A/fr not_active IP Right Cessation
- 1982-12-09 JP JP57214732A patent/JPS58106102A/ja active Pending
- 1982-12-09 AR AR291543A patent/AR228927A1/es active
-
1986
- 1986-08-12 JP JP1986122995U patent/JPH0110401Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| MX157531A (es) | 1988-11-28 |
| BE895285A (fr) | 1983-06-08 |
| JPS58106102A (ja) | 1983-06-24 |
| IT8224620A1 (it) | 1984-06-06 |
| JPS6278302U (OSRAM) | 1987-05-19 |
| IT8224620A0 (it) | 1982-12-06 |
| JPH0110401Y2 (OSRAM) | 1989-03-24 |
| AR228927A1 (es) | 1983-04-29 |
| GB2111604A (en) | 1983-07-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19961230 |