GB737167A - Improvements in hollow blades for fluid-flow operated machines - Google Patents
Improvements in hollow blades for fluid-flow operated machinesInfo
- Publication number
- GB737167A GB737167A GB14531/51A GB1453151A GB737167A GB 737167 A GB737167 A GB 737167A GB 14531/51 A GB14531/51 A GB 14531/51A GB 1453151 A GB1453151 A GB 1453151A GB 737167 A GB737167 A GB 737167A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- slot
- guide
- hollow
- cooling fluid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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
-
- 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
-
- 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 (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR511A FR1262551A (fr) | 1949-11-22 | 1949-11-22 | Aube creuse pour machines à écoulement de fluide |
US224325A US2801072A (en) | 1949-11-22 | 1951-05-03 | Hollow blade for fluid flow operated machine |
CH325966T | 1951-06-12 | ||
GB14530/51A GB737166A (en) | 1949-11-22 | 1951-06-19 | Improvements in or relating to fluid-cooled hollow turbine or like blades |
DEO1673A DE938280C (de) | 1949-11-22 | 1951-06-24 | Hohlschaufel fuer Stroemungsmaschinen |
DEO1674A DE938691C (de) | 1949-11-22 | 1951-06-24 | Aufbau und Befestigung von Einsaetzen fuer die Kuehlmittelfuehrung innengekuehlter Hohlschaufeln fuer Stroemungsmaschinen |
BE504383T | 1951-06-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB737167A true GB737167A (en) | 1955-09-21 |
Family
ID=10042863
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14530/51A Expired GB737166A (en) | 1949-11-22 | 1951-06-19 | Improvements in or relating to fluid-cooled hollow turbine or like blades |
GB14531/51A Expired GB737167A (en) | 1949-11-22 | 1951-06-19 | Improvements in hollow blades for fluid-flow operated machines |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14530/51A Expired GB737166A (en) | 1949-11-22 | 1951-06-19 | Improvements in or relating to fluid-cooled hollow turbine or like blades |
Country Status (6)
Country | Link |
---|---|
US (1) | US2801072A (de) |
BE (1) | BE504383A (de) |
CH (1) | CH325966A (de) |
DE (2) | DE938691C (de) |
FR (1) | FR1262551A (de) |
GB (2) | GB737166A (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2121483A (en) * | 1982-06-08 | 1983-12-21 | Rolls Royce | Cooled turbine blade for a gas turbine engine |
US4582467A (en) * | 1983-12-22 | 1986-04-15 | United Technologies Corporation | Two stage rotor assembly with improved coolant flow |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3087484B1 (fr) * | 2018-10-18 | 2021-01-15 | Safran Aircraft Engines | Aube de turbomachine |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE494165C (de) * | 1927-11-17 | 1930-03-19 | Charles Algernon Parsons | Verfahren zur Herstellung von Turbinenschaufeln mit Fuss- und Schaftteil durch Walzen aus einem Rohwerkstueck |
US2013622A (en) * | 1932-03-24 | 1935-09-03 | Parsons C A & Co Ltd | Method of making turbine blades |
DE604732C (de) * | 1932-03-24 | 1934-10-29 | Parsons C A & Co Ltd | Verfahren zur Herstellung von hohlen, nahtlosen Turbinenschaufeln |
DE625799C (de) * | 1934-04-25 | 1936-02-15 | Parsons C A & Co Ltd | Verfahren zur Herstellung hohler Turbinenschaufeln durch Ausstrecken eines gefuellten Hohlwerkstuecks von einer zur Laenge der fertigen Schaufel relativ geringen Laenge |
FR880656A (fr) * | 1940-09-20 | 1943-04-01 | Bmw Flugmotorenbau Gmbh | Rotor pour turbines à gaz d'échappement |
CH237453A (de) * | 1942-02-04 | 1945-04-30 | Bmw Flugmotorenbau Ges Mbh | Innengekühlte Turbinenschaufel. |
US2563269A (en) * | 1943-05-22 | 1951-08-07 | Lockheed Aircraft Corp | Gas turbine |
GB584580A (en) * | 1943-12-28 | 1947-01-17 | Masch Fabrick Oerlikon | Improvements in or relating to turbine blades |
FR949459A (fr) * | 1947-07-09 | 1949-08-31 | Aubes pour rotors | |
IT454293A (de) * | 1948-04-22 | |||
FR981599A (fr) * | 1948-12-31 | 1951-05-28 | Dispositif amortisseur de vibrations | |
US2648520A (en) * | 1949-08-02 | 1953-08-11 | Heinz E Schmitt | Air-cooled turbine blade |
-
1949
- 1949-11-22 FR FR511A patent/FR1262551A/fr not_active Expired
-
1951
- 1951-05-03 US US224325A patent/US2801072A/en not_active Expired - Lifetime
- 1951-06-12 CH CH325966D patent/CH325966A/fr unknown
- 1951-06-19 GB GB14530/51A patent/GB737166A/en not_active Expired
- 1951-06-19 GB GB14531/51A patent/GB737167A/en not_active Expired
- 1951-06-24 DE DEO1674A patent/DE938691C/de not_active Expired
- 1951-06-24 DE DEO1673A patent/DE938280C/de not_active Expired
- 1951-06-30 BE BE504383D patent/BE504383A/xx unknown
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2121483A (en) * | 1982-06-08 | 1983-12-21 | Rolls Royce | Cooled turbine blade for a gas turbine engine |
US4582467A (en) * | 1983-12-22 | 1986-04-15 | United Technologies Corporation | Two stage rotor assembly with improved coolant flow |
Also Published As
Publication number | Publication date |
---|---|
FR1262551A (fr) | 1961-06-05 |
US2801072A (en) | 1957-07-30 |
GB737166A (en) | 1955-09-21 |
BE504383A (de) | 1951-12-31 |
DE938280C (de) | 1956-01-26 |
DE938691C (de) | 1956-02-02 |
CH325966A (fr) | 1957-11-30 |
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