CH535373A - Aube à refroidissement interne - Google Patents
Aube à refroidissement interneInfo
- Publication number
- CH535373A CH535373A CH1056671A CH1056671A CH535373A CH 535373 A CH535373 A CH 535373A CH 1056671 A CH1056671 A CH 1056671A CH 1056671 A CH1056671 A CH 1056671A CH 535373 A CH535373 A CH 535373A
- Authority
- CH
- Switzerland
- Prior art keywords
- internally cooled
- cooled vane
- vane
- internally
- cooled
- 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
- F01D5/181—Blades having a closed internal cavity containing a cooling medium, e.g. sodium
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/25—Three-dimensional helical
-
- 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 |
|---|---|---|---|
| FR7026718A FR2098558A5 (enExample) | 1970-07-20 | 1970-07-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH535373A true CH535373A (fr) | 1973-03-31 |
Family
ID=9058931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH1056671A CH535373A (fr) | 1970-07-20 | 1971-07-19 | Aube à refroidissement interne |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3738771A (enExample) |
| CH (1) | CH535373A (enExample) |
| DE (1) | DE2131484A1 (enExample) |
| FR (1) | FR2098558A5 (enExample) |
| GB (1) | GB1306496A (enExample) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1541894A (en) * | 1976-08-12 | 1979-03-14 | Rolls Royce | Gas turbine engines |
| GB2286229B (en) * | 1977-10-04 | 1995-12-20 | Rolls Royce | Turbine aerofoil blade provided with a heat insulating coating |
| GB2252368B (en) * | 1981-03-20 | 1993-02-17 | Rolls Royce | Liquid cooled aerofoil blade |
| GB2254379B (en) * | 1981-04-28 | 1993-04-14 | Rolls Royce | Cooled aerofoil blade |
| US4775296A (en) * | 1981-12-28 | 1988-10-04 | United Technologies Corporation | Coolable airfoil for a rotary machine |
| US4514144A (en) * | 1983-06-20 | 1985-04-30 | General Electric Company | Angled turbulence promoter |
| US4854374A (en) * | 1988-02-02 | 1989-08-08 | Frank Harrison | Temperature controlling apparatus |
| US4879880A (en) * | 1989-01-17 | 1989-11-14 | Frank Harrison | Air temperature regulator |
| US5299418A (en) * | 1992-06-09 | 1994-04-05 | Jack L. Kerrebrock | Evaporatively cooled internal combustion engine |
| US5782076A (en) * | 1996-05-17 | 1998-07-21 | Westinghouse Electric Corporation | Closed loop air cooling system for combustion turbines |
| US5857836A (en) * | 1996-09-10 | 1999-01-12 | Aerodyne Research, Inc. | Evaporatively cooled rotor for a gas turbine engine |
| US5980209A (en) * | 1997-06-27 | 1999-11-09 | General Electric Co. | Turbine blade with enhanced cooling and profile optimization |
| US6019572A (en) * | 1998-08-06 | 2000-02-01 | Siemens Westinghouse Power Corporation | Gas turbine row #1 steam cooled vane |
| US6192670B1 (en) | 1999-06-15 | 2001-02-27 | Jack L. Kerrebrock | Radial flow turbine with internal evaporative blade cooling |
| US6539627B2 (en) | 2000-01-19 | 2003-04-01 | General Electric Company | Method of making turbulated cooling holes |
| IT1319140B1 (it) * | 2000-11-28 | 2003-09-23 | Nuovo Pignone Spa | Sistema di refrigerazione per ugelli statorici di turbine a gas |
| US6997679B2 (en) * | 2003-12-12 | 2006-02-14 | General Electric Company | Airfoil cooling holes |
| US7207775B2 (en) * | 2004-06-03 | 2007-04-24 | General Electric Company | Turbine bucket with optimized cooling circuit |
| US7357623B2 (en) * | 2005-05-23 | 2008-04-15 | Pratt & Whitney Canada Corp. | Angled cooling divider wall in blade attachment |
| DE102005055682A1 (de) | 2005-11-22 | 2007-05-24 | Giesecke & Devrient Gmbh | Vorrichtung für die Überprüfung der Echtheit von Banknoten |
| US9353687B1 (en) * | 2012-10-18 | 2016-05-31 | Florida Turbine Technologies, Inc. | Gas turbine engine with liquid metal cooling |
| KR101509385B1 (ko) * | 2014-01-16 | 2015-04-07 | 두산중공업 주식회사 | 스월링 냉각 채널을 구비한 터빈 블레이드 및 그 냉각 방법 |
| US10428660B2 (en) * | 2017-01-31 | 2019-10-01 | United Technologies Corporation | Hybrid airfoil cooling |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2150098A (en) * | 1936-03-27 | 1939-03-07 | Alexander J Jodeiko | Cooling means for combustion turbines |
| BE431387A (enExample) * | 1936-07-01 | |||
| GB610737A (en) * | 1946-03-19 | 1948-10-20 | Power Jets Res & Dev Ltd | Improvements relating to turbine and like blading |
| BE485284A (enExample) * | 1947-10-28 | |||
| BE496812A (enExample) * | 1949-07-06 | 1900-01-01 | ||
| DE1002570C2 (de) * | 1955-05-04 | 1957-07-18 | Marko Majcen | Gasturbinenanlage mit doppeltem Kreisprozess |
| US2888243A (en) * | 1956-10-22 | 1959-05-26 | Pollock Robert Stephen | Cooled turbine blade |
| GB985772A (en) * | 1961-01-13 | 1965-03-10 | Bristol Siddeley Engines Ltd | Improvements in blades for gas turbines |
| US3164367A (en) * | 1962-11-21 | 1965-01-05 | Gen Electric | Gas turbine blade |
-
1970
- 1970-07-20 FR FR7026718A patent/FR2098558A5/fr not_active Expired
-
1971
- 1971-06-24 DE DE19712131484 patent/DE2131484A1/de active Pending
- 1971-07-15 GB GB3323971A patent/GB1306496A/en not_active Expired
- 1971-07-15 US US00162849A patent/US3738771A/en not_active Expired - Lifetime
- 1971-07-19 CH CH1056671A patent/CH535373A/fr not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| US3738771A (en) | 1973-06-12 |
| GB1306496A (en) | 1973-02-14 |
| FR2098558A5 (enExample) | 1972-03-10 |
| DE2131484A1 (de) | 1972-01-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PL | Patent ceased |