CH209009A - Machine part with cooling device against harmful heating, in particular turbine blade and method for its production. - Google Patents
Machine part with cooling device against harmful heating, in particular turbine blade and method for its production.Info
- Publication number
- CH209009A CH209009A CH209009DA CH209009A CH 209009 A CH209009 A CH 209009A CH 209009D A CH209009D A CH 209009DA CH 209009 A CH209009 A CH 209009A
- Authority
- CH
- Switzerland
- Prior art keywords
- production
- cooling device
- turbine blade
- machine part
- device against
- 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
- F01D5/186—Film cooling
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
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 |
---|---|---|---|
DE209009X | 1938-02-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH209009A true CH209009A (en) | 1940-03-15 |
Family
ID=5794542
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH209009D CH209009A (en) | 1938-02-08 | 1939-01-26 | Machine part with cooling device against harmful heating, in particular turbine blade and method for its production. |
Country Status (5)
Country | Link |
---|---|
US (1) | US2220420A (en) |
BE (1) | BE432599A (en) |
CH (1) | CH209009A (en) |
FR (1) | FR849880A (en) |
GB (1) | GB524794A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767546C (en) * | 1938-09-12 | 1952-11-04 | Bmw Flugmotorenbau G M B H | Internally cooled turbine blade |
DE1024754B (en) * | 1956-02-11 | 1958-02-20 | Maschf Augsburg Nuernberg Ag | Cooled blade for hot operated turbines or compressors |
DE969599C (en) * | 1943-05-27 | 1958-06-19 | Holzwarth Gasturbinen G M B H | Cooled nozzle body for centrifugal machines, especially exhaust gas turbines |
DE1092255B (en) * | 1957-05-28 | 1960-11-03 | Snecma | Method for cooling machine parts, in particular hollow gas turbine blades |
Families Citing this family (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2563269A (en) * | 1943-05-22 | 1951-08-07 | Lockheed Aircraft Corp | Gas turbine |
FR963824A (en) * | 1943-11-19 | 1950-07-21 | ||
US2489683A (en) * | 1943-11-19 | 1949-11-29 | Edward A Stalker | Turbine |
BE462182A (en) * | 1944-12-22 | 1900-01-01 | ||
US2463340A (en) * | 1945-02-22 | 1949-03-01 | Wiberg Oscar Anton | Axial flow turbine blade structure |
US2506581A (en) * | 1945-06-30 | 1950-05-09 | Jr Albon C Cowles | Means for cooling gas turbine blades |
US2585871A (en) * | 1945-10-22 | 1952-02-12 | Edward A Stalker | Turbine blade construction with provision for cooling |
US2613910A (en) * | 1947-01-24 | 1952-10-14 | Edward A Stalker | Slotted turbine blade |
US2641439A (en) * | 1947-10-01 | 1953-06-09 | Chrysler Corp | Cooled turbine or compressor blade |
US2750147A (en) * | 1947-10-28 | 1956-06-12 | Power Jets Res & Dev Ltd | Blading for turbines and like machines |
US2613911A (en) * | 1947-11-06 | 1952-10-14 | Stalker Dev Company | Fluid turning blade |
US2641440A (en) * | 1947-11-18 | 1953-06-09 | Chrysler Corp | Turbine blade with cooling means and carrier therefor |
IT454293A (en) * | 1948-04-22 | |||
US2687278A (en) * | 1948-05-26 | 1954-08-24 | Chrysler Corp | Article with passages |
US2700530A (en) * | 1948-08-27 | 1955-01-25 | Chrysler Corp | High temperature elastic fluid apparatus |
US2625366A (en) * | 1948-11-18 | 1953-01-13 | Packard Motor Car Co | Turbine rotor construction |
US2858100A (en) * | 1952-02-01 | 1958-10-28 | Stalker Dev Company | Blade structure for turbines and the like |
US2807434A (en) * | 1952-04-22 | 1957-09-24 | Gen Motors Corp | Turbine rotor assembly |
US2873944A (en) * | 1952-09-10 | 1959-02-17 | Gen Motors Corp | Turbine blade cooling |
US2780435A (en) * | 1953-01-12 | 1957-02-05 | Jackson Thomas Woodrow | Turbine blade cooling structure |
DE1000733C2 (en) * | 1953-10-21 | 1957-06-19 | Wilhelm Ludowici Dr Ing | Car-shaped kiln for pottery |
US3112557A (en) * | 1958-02-10 | 1963-12-03 | Rolls Royce | Turbine and compressor blades |
US3319593A (en) * | 1962-12-24 | 1967-05-16 | Papst Hermann | Boundary layer control |
US4026659A (en) * | 1975-10-16 | 1977-05-31 | Avco Corporation | Cooled composite vanes for turbine nozzles |
US4672727A (en) * | 1985-12-23 | 1987-06-16 | United Technologies Corporation | Method of fabricating film cooling slot in a hollow airfoil |
US4726735A (en) * | 1985-12-23 | 1988-02-23 | United Technologies Corporation | Film cooling slot with metered flow |
US4770608A (en) * | 1985-12-23 | 1988-09-13 | United Technologies Corporation | Film cooled vanes and turbines |
US4738588A (en) * | 1985-12-23 | 1988-04-19 | Field Robert E | Film cooling passages with step diffuser |
US4653983A (en) * | 1985-12-23 | 1987-03-31 | United Technologies Corporation | Cross-flow film cooling passages |
US4705455A (en) * | 1985-12-23 | 1987-11-10 | United Technologies Corporation | Convergent-divergent film coolant passage |
US4684323A (en) * | 1985-12-23 | 1987-08-04 | United Technologies Corporation | Film cooling passages with curved corners |
US4664597A (en) * | 1985-12-23 | 1987-05-12 | United Technologies Corporation | Coolant passages with full coverage film cooling slot |
US4669957A (en) * | 1985-12-23 | 1987-06-02 | United Technologies Corporation | Film coolant passage with swirl diffuser |
US4676719A (en) * | 1985-12-23 | 1987-06-30 | United Technologies Corporation | Film coolant passages for cast hollow airfoils |
GB2202907A (en) * | 1987-03-26 | 1988-10-05 | Secr Defence | Cooled aerofoil components |
US4859147A (en) * | 1988-01-25 | 1989-08-22 | United Technologies Corporation | Cooled gas turbine blade |
US5097660A (en) * | 1988-12-28 | 1992-03-24 | Sundstrand Corporation | Coanda effect turbine nozzle vane cooling |
GB9821639D0 (en) | 1998-10-06 | 1998-11-25 | Rolls Royce Plc | Coolant passages for gas turbine components |
US6589600B1 (en) * | 1999-06-30 | 2003-07-08 | General Electric Company | Turbine engine component having enhanced heat transfer characteristics and method for forming same |
US7357351B2 (en) * | 2002-07-18 | 2008-04-15 | Eric T. Schmidt | Linear shock wave absorber |
US7798765B2 (en) * | 2007-04-12 | 2010-09-21 | United Technologies Corporation | Out-flow margin protection for a gas turbine engine |
US8246297B2 (en) | 2008-07-21 | 2012-08-21 | Pratt & Whitney Canada Corp. | Shroud segment cooling configuration |
US11286783B2 (en) * | 2020-04-27 | 2022-03-29 | Raytheon Technologies Corporation | Airfoil with CMC liner and multi-piece monolithic ceramic shell |
-
0
- BE BE432599D patent/BE432599A/xx unknown
-
1939
- 1939-01-26 CH CH209009D patent/CH209009A/en unknown
- 1939-02-06 FR FR849880D patent/FR849880A/en not_active Expired
- 1939-02-08 GB GB4133/39A patent/GB524794A/en not_active Expired
- 1939-02-09 US US255536A patent/US2220420A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767546C (en) * | 1938-09-12 | 1952-11-04 | Bmw Flugmotorenbau G M B H | Internally cooled turbine blade |
DE969599C (en) * | 1943-05-27 | 1958-06-19 | Holzwarth Gasturbinen G M B H | Cooled nozzle body for centrifugal machines, especially exhaust gas turbines |
DE1024754B (en) * | 1956-02-11 | 1958-02-20 | Maschf Augsburg Nuernberg Ag | Cooled blade for hot operated turbines or compressors |
DE1092255B (en) * | 1957-05-28 | 1960-11-03 | Snecma | Method for cooling machine parts, in particular hollow gas turbine blades |
Also Published As
Publication number | Publication date |
---|---|
FR849880A (en) | 1939-12-04 |
BE432599A (en) | |
GB524794A (en) | 1940-08-14 |
US2220420A (en) | 1940-11-05 |
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