SE411782B - For kraftiga termiska pakenningar utsatt, kyld komponent serskilt turbinskovel samt sett for tillverkning av densamma - Google Patents
For kraftiga termiska pakenningar utsatt, kyld komponent serskilt turbinskovel samt sett for tillverkning av densammaInfo
- Publication number
- SE411782B SE411782B SE7600845A SE7600845A SE411782B SE 411782 B SE411782 B SE 411782B SE 7600845 A SE7600845 A SE 7600845A SE 7600845 A SE7600845 A SE 7600845A SE 411782 B SE411782 B SE 411782B
- Authority
- SE
- Sweden
- Prior art keywords
- turbin
- manufacturing
- cover
- component specific
- thermal packaging
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000004806 packaging method and process Methods 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
- F01D5/182—Transpiration cooling
- F01D5/183—Blade walls being porous
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2503285A DE2503285C2 (de) | 1975-01-28 | 1975-01-28 | Verfahren zur Herstellung eines einstückigen thermisch hochbeanspruchten gekühlten Bauteils, insbesondere einer Schaufel für Turbinentriebwerke |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| SE7600845L SE7600845L (sv) | 1976-07-29 |
| SE411782B true SE411782B (sv) | 1980-02-04 |
Family
ID=5937437
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SE7600845A SE411782B (sv) | 1975-01-28 | 1976-01-27 | For kraftiga termiska pakenningar utsatt, kyld komponent serskilt turbinskovel samt sett for tillverkning av densamma |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4067662A (it) |
| DE (1) | DE2503285C2 (it) |
| FR (1) | FR2299499A1 (it) |
| GB (1) | GB1507001A (it) |
| IT (1) | IT1053445B (it) |
| SE (1) | SE411782B (it) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4133368A (en) * | 1977-08-01 | 1979-01-09 | United Technologies Corporation | Single crystal casting mold and method for making same |
| US4376004A (en) * | 1979-01-16 | 1983-03-08 | Westinghouse Electric Corp. | Method of manufacturing a transpiration cooled ceramic blade for a gas turbine |
| US4311433A (en) * | 1979-01-16 | 1982-01-19 | Westinghouse Electric Corp. | Transpiration cooled ceramic blade for a gas turbine |
| US4247259A (en) * | 1979-04-18 | 1981-01-27 | Avco Corporation | Composite ceramic/metallic turbine blade and method of making same |
| US4487550A (en) * | 1983-01-27 | 1984-12-11 | The United States Of America As Represented By The Secretary Of The Air Force | Cooled turbine blade tip closure |
| DE3327218A1 (de) * | 1983-07-28 | 1985-02-07 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Thermisch hochbeanspruchtes, gekuehltes bauteil, insbesondere turbinenschaufel |
| DE3339505A1 (de) * | 1983-10-31 | 1985-05-09 | Bernd 6352 Ober-Mörlen Jung | Gasturbine mit einem vorgeschalteten turbokompressor |
| US4491421A (en) * | 1983-11-21 | 1985-01-01 | De Dietrich (Usa), Inc. | Impeller assembly and shaft having interference fit |
| US4508455A (en) * | 1983-11-21 | 1985-04-02 | De Dietrich (Usa), Inc. | Agitator including impeller assembly and shaft having interference fit |
| US4589823A (en) * | 1984-04-27 | 1986-05-20 | General Electric Company | Rotor blade tip |
| US5690473A (en) * | 1992-08-25 | 1997-11-25 | General Electric Company | Turbine blade having transpiration strip cooling and method of manufacture |
| DE19611115B4 (de) * | 1996-03-21 | 2007-03-08 | Adam Opel Ag | Gehäuse für ein hydraulisch unterstütztes Zahnstangenlenkgetriebe |
| US6350404B1 (en) | 2000-06-13 | 2002-02-26 | Honeywell International, Inc. | Method for producing a ceramic part with an internal structure |
| EP1186748A1 (de) * | 2000-09-05 | 2002-03-13 | Siemens Aktiengesellschaft | Laufschaufel für eine Strömungsmaschine sowie Strömungsmaschine |
| US6375425B1 (en) | 2000-11-06 | 2002-04-23 | General Electric Company | Transpiration cooling in thermal barrier coating |
| US6544003B1 (en) * | 2000-11-08 | 2003-04-08 | General Electric Co. | Gas turbine blisk with ceramic foam blades and its preparation |
| GB0700499D0 (en) | 2007-01-11 | 2007-02-21 | Rolls Royce Plc | Aerofoil configuration |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB731161A (en) * | 1952-02-11 | 1955-06-01 | Parsons & Marine Eng Turbine | Improvements in or relating to the sweat-cooling of components, e.g., for gas turbines |
| US2851216A (en) * | 1954-01-13 | 1958-09-09 | Schwarzkopf Dev Co | Device adapted for respiration cooling and process of making same |
| US3011761A (en) * | 1954-11-25 | 1961-12-05 | Power Jets Res & Dev Ltd | Turbine blades |
| US2857657A (en) * | 1956-01-16 | 1958-10-28 | California Inst Res Found | Method of constructing a porous wall |
| US2946681A (en) * | 1957-01-31 | 1960-07-26 | Federal Mogul Bower Bearings | Method of providing a body with a porous metal shell |
| US3067982A (en) * | 1958-08-25 | 1962-12-11 | California Inst Res Found | Porous wall turbine blades and method of manufacture |
| US3114961A (en) * | 1959-03-20 | 1963-12-24 | Power Jets Res & Dev Ltd | Treatment of porous bodies |
| US3529902A (en) * | 1968-05-22 | 1970-09-22 | Gen Motors Corp | Turbine vane |
| US3656863A (en) * | 1970-07-27 | 1972-04-18 | Curtiss Wright Corp | Transpiration cooled turbine rotor blade |
| US3706508A (en) * | 1971-04-16 | 1972-12-19 | Sean Lingwood | Transpiration cooled turbine blade with metered coolant flow |
| DE2301105C2 (de) * | 1973-01-10 | 1984-07-05 | Sherwood Refractories Inc., Cleveland, Ohio | Präzisionsgußform und Verfahren zu deren Herstellung |
-
1975
- 1975-01-28 DE DE2503285A patent/DE2503285C2/de not_active Expired
-
1976
- 1976-01-21 US US05/651,147 patent/US4067662A/en not_active Expired - Lifetime
- 1976-01-26 IT IT47792/76A patent/IT1053445B/it active
- 1976-01-27 SE SE7600845A patent/SE411782B/xx unknown
- 1976-01-27 GB GB3129/76A patent/GB1507001A/en not_active Expired
- 1976-01-27 FR FR7602113A patent/FR2299499A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US4067662A (en) | 1978-01-10 |
| FR2299499B3 (it) | 1979-06-29 |
| IT1053445B (it) | 1981-08-31 |
| GB1507001A (en) | 1978-04-12 |
| DE2503285C2 (de) | 1984-08-30 |
| SE7600845L (sv) | 1976-07-29 |
| FR2299499A1 (fr) | 1976-08-27 |
| DE2503285A1 (de) | 1976-07-29 |
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